NASA SP-7011 (379) September 1993

AEROSPACE MEDICINE AND BIOLOGY

A CONTINUING BIBLIOGRAPHY WITH INDEXES

<;p-7011(379)) AEROSPACE iNE INO BIOLOGY: A CONTINUING BIBLIOGRAPHY WITH INOE ES Unclas (SUPPLEMENT 379) (NASA) 106 p

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AEROSPACE MEDICINE AND BIOLOGY

A CONTINUING BIBLIOGRAPHY WITH INDEXES

National Aeronautics and Space Administration Scientific and Technical Information Program NASA Washington. DC 1993 This publication was prepared by the NASA Center for AeroSpace Information, 800 Elkridge Landing Road, Linthicum Heights. MD 21090-2934, (301) 621-0390. INTRODUCTION

This issue of Aerospace Medicine and Biology (NASA SP-7011) lists 305 reports, articles, and other documents recently announced in the NASA STl Database. The first issue of Aerospace Medicine and Biology was published in July 1964.

Accession numbers cited in this issue include: Scientific and Technical Aerospace Reports (STAR) (N-10000 Series) N93-27098 — N93-29391 International Aerospace Abstracts (IAA) (A-10000 Series) A93-37501 — A93-41655

In its subject coverage, Aerospace Medicine and Biology concentrates on the biological, physiologi- cal, psychological, and environmental effects to which humans are subjected during and following simulated or actual flight in the Earth's atmosphere or in interplanetary space. References describing similar effects on biological organisms of lower order are also included. Such related topics as sanitary problems, pharmacology, toxicology, safety and survival, life support systems, exobiology, and personnel factors receive appropriate attention. Applied research receives the most emphasis, but references to fundamental studies and theoretical principles related to experimental development also qualify for inclusion.

Each entry in the publication consists of a standard bibliographic citation accompanied in most cases by an abstract. The listing of the entries is arranged by STAR categories 51 through 55, the Life Sciences division. The citations include the original accession numbers from the respective announcement journals.

Seven indexes—subject, personal author, corporate source, foreign technology, contract number, report number, and accession number—are included.

A cumulative index for 1993 will be published in early 1994.

Information on availability of documents listed, addresses of organizations, and CASI price schedules are located at the back of this issue.

INTENTIONALU fi£&H TABLE OF CONTENTS

Category 51 Life Sciences (General) 271

Category 52 Aerospace Medicine 277 Includes physiological factors; biological effects of radiation; and effects of weightlessness on man and animals.

Category 53 Behavioral Sciences 286 Includes psychological factors; individual and group behavior; crew training and evaluation; and psychiatric research.

Category 54 Man/System Technology and Life Support 289 Includes human engineering; biotechnology; and space suits and protective clothing.

Category 55 Space Biology 322 Includes exobiology; planetary biology; and extraterrestrial life.

Subject Index A-1 Personal Author Index B-1 Corporate Source Index C-1 Foreign Technology Index D-1 Contract Number Index E-1 Report Number Index F-1 Accession Number Index G-1 Appendix APP-1

EAGfc I I/ INFENTIONALU TYPICAL REPORT CITATION AND ABSTRACT

NASA SPONSORE^Du 1uIO5 N MICROFICHE ACCESSION NUMBER -» N93-12195*# Lockheed Engineering and Sciences, Co., Houston, <— CORPORATE SOURCE TX. TITLE -» ASTRONAUT CANDIDATE STRENGTH MEASUREMENT USING THE CYBEX 2 AND THE UDO MULTI-JOINT 2 DYNAMOMETERS Final Report AUTHORS -> AMY E. CARROLL and ROBERT P. WILMINGTON May 1992 <- PUBLICATION DATE CONTRACT NUMBER -» (Contract NAS9-17900) REPORT NUMBERS -> (NASA-CR-185679; MAS 1.26:185679; LESC-30277) Avail: CASI HC «- AVAILABILITY PRICE CODE —» A03/MFA01 The Anthropometry and Biomechanics Laboratory in the man- Systems division at NASA's Johnson Space Center has as one of its responsibilities the anthropometry and strength measurement data collection of astronaut candidates. The anthropometry data is used to ensure that the astronaut candidates are within the height restrictions for space vehicle and space suit design requirments, for example. The strength data is used to help detect abnormalities or isolate injuries to muscle groups that could jeopardize the astronauts' safety. The Cybex II Dynamometer has been used for strength measurements from 1985 through 1991. The Cybex II was one of the first instruments of its kind to measure strength and similarity of muscle groups by isolating the specific joint of interest. In November 1991. a LIDO Multi-Joint II Dynamometer was purchased to upgrade the strength measurement data collection capability of the Anthropometry and Biomechanics Laboratory. The LIDO Multi-Joint II Dynamometer design offers several advantages over the Cybex II Dynamometer including a more sophis- ticated method of joint isolation and a more accurate and efficient computer based data collection system. Author

TYPICAL JOURNAL ARTICLE CITATION AND ABSTRACT

ACCESSION NUMBER -» A93-11150 TITLE -» STUDIES TOWARDS THE CRYSTALLIZATION OF THE ROD VISUAL PIGMENT RHODOPS1N AUTHORS -» W. J. DE GRIP. J. VAN OOSTRUM, and G. L. J. DE CALUWE AUTHORS' AFFILIATION -» (Nigmegen Catholic Univ., Netherlands) Journal of Crystal «- JOURNAL TITLE Growth (ISSN 0022-0248) vol. 122, no. 1-4 Aug. 1992 <- PUBLICATION DATE p. 375-384. Research supported by SRON refs CONTRACT NUMBER -» (Contract NWO-SON-328-050) Copyright Results are presented of crystallization experiments on bovine rhodopsin, which established a restricted range of conditions which reproducibly yield rhodopsin crystals. Several parameters were optimized, including the detergent, the precipitant, additives, and pH. The crystals obtained so far are too small (less than 50 microns in any direction) or of insufficient order to allow high-resolution diffraction analysis. Several approaches are proposed for improving the average size, stability, and order of the rhodopsin crystals. I. S.

vi AEROSPACE MEDICINE AND BIOLOGY A Continuing Bibliography (Suppl. 379) September 1993

51 Therapeutics (ISSN 0022-3565) vol. 264, no. 3 March 1993 p. 1071-1078. LIFE SCIENCES (GENERAL) Copyright Hind-limb unloading by tail suspension of rats was used to examine the effectiveness of aminohydroxybutane bisphosphonate (AHBuBP) and clenbuterol in preventing bone loss and muscle atrophy, respectively. Rats were randomized into six groups of six: (1) unsuspended, saline; (2) unsuspended, saline, pair fed A93-38451* National Aeronautics and Space Administration. with group 3; (3) suspended, saline; (4) suspended, 0.03 mg/kg/day Ames Research Center, Moffett Field, CA. x 2 of AHBuBP; (5) suspended, 0.3 mg/kg/day x 2 of AHBuBP; 8-OH-DPAT DOES NOT INTERFERE WITH HABITUATION TO and (6) suspended, 0.3 mg/kg/day x 2 of AHBuBP + clenbuterol MOTION-INDUCED EMESIS IN CATS (0.5 mg/kg/day i.p. x 6, then 1 mg/kg/day i.p. x G). Animals in JAMES B. LUCOT and GEORGE H. CRAMPTON (Wright State groups 3 to 6 were tail suspended for 14 days and allowed free Univ., Dayton, OH) Brain Research Bulletin (ISSN 0361-9320) mobility with their hind limbs unloaded. On days -2 and -1, before vol.26 1991 p. 919-921. refs suspension on day 0, all rats received a single s.c. injection of (Contract NCC2-229) either 2 ml/kg of normal saline (vehicle) or AHBuBP. On day 14, Copyright the rats were euthanized. It was found that pair feeding had no Experiments were performed to determine if suppression of effect other than on food consumption and body weight. AHBuBP motion-induced emesis (motion sickness) by 8-OH-DPAT altered caused a dose-dependent increase in bone density in humeri, the development or retention of habituation to the motion stimulus. tibias and femurs, even in tail-suspended rats, relative to control Cats received 8-OH-DPAT followed by provocative motion on three unsuspended animals, with no significant difference in bone consecutive treatment days. A drug-free test on the fourth day strength or stiffness between AHBuBP groups and unsuspended resulted in an incidence of emesis that was not different from animals. Author (revised) that obtained on the fourth consecutive day of drug-free motion testing. Three consecutive days of treatment with 8-OH-DPAT A93-39707 without motion had no effect on the incidence of motion sickness MATHEMATICAL MODEL FOR THE EXCHANGE OF GASES IN on the fourth day. It was concluded that suppression of motion THE LUNGS WITH SPECIAL REFERENCE TO CARBON sickness by 8-OH-DPAT does not alter the acquisition or retention MONOXIDE of habituation. Author (revised) S. SELVAKUMAR, M. SHARAN, and M. P. SINGH (Indian Inst. of Technology, New Delhi, India) Medical & Biological Engineering A93-39280 & Computing (ISSN 0140-0118) vol. 30, no. 5 Sept. 1992 p. FERROUS IRON OXIDATION BY ANOXYGENIC 525-532. PHOTOTROPHIC BACTERIA Copyright FRIEDRICH WIDDEL (Max-Planck-lnst. fuer Marine Mikrobiologie, A mathematical model has been formulated for the simultaneous Bremen, Germany), SYLVIA SCHNELL, SILKE HEISING (Konstanz exchange of gases O2, CO2, CO and N2 in the lungs. The model Univ., Germany), ARMIN EHRENREICH, BERNHARD ASSMUS takes into account the physiological parameters, such as ventilation (Max-Planck-lnst. fuer Marine Mikrobiologie, Bremen, Germany), rate, diffusing capacity of the lungs, cardiac output, total volume and BERNHARD SCHINK (Konstanz Univ., Germany) Nature of blood in the body and the interaction of gases in the blood. (ISSN 0028-0836) vol. 362, no. 6423 April 29, 1993 p. The nonlinear functions for representing O2, CO2 and CO 834-836. -refs dissociation curves have been used. The results predicted from Copyright the model are in good agreement with those based on the The reducing power of ferrous Fe is dramatically increased at ventilation/perfusion relationships. The COHb build-up in the blood, pH values above 2-3, due to the formation of ferric hydroxy and computed from the model as a function of exposure time, is in oxyhydroxy compounds. It is presently noted that it may be possible good agreement with the experimental values. The consideration for Fe (II) at around pH 7.0 to function as an electron donor for of capillary blood pO2 as a constant value, instead of an anoxygenic photosynthesis, and attention is given to purple, independent variable, is shown to introduce a maximum error of nonsulfur bacteria which can oxidize colorless Fe (II) to brown Fe 0.25 per cent in the blood COHb. The model is applied to analyze (III), and reduce C02 to cell material. It is thereby shown that the COHb levels at high altitude. Author oxygen-independent biological Fe oxidation was possible prior to the evolution of oxygenic photosynthesis. AIAA A93-39711 NEUROPHARMACOLOGY OF MOTION SICKNESS AND EMESIS - A REVIEW A93-39703 N. TAKEDA, M. MORITA, S. HASEGAWA, A. HORN, T. KUBO, AMINOHYDROXYBUTANE BISPHOSPHONATE AND and T. MATSUNAGA (Osaka Univ., Japan) Acta CLENBUTEROL PREVENT BONE CHANGES AND RETARD Oto-Laryngologica, Supplement (ISSN 0365-5237) vol. 501 MUSCLE ATROPHY RESPECTIVELY IN TAIL-SUSPENDED 1993 p. 10-15. RATS Copyright G. APSELOFF, B. GIRTEN, M. WALKER, D. R. SHEPARD, M. E. Histamine H1-receptors are involved in the development of KRECIC, L S. STERN, and N. GERBER (Ohio State Univ., the symptoms and signs of motion sickness, including emesis. On Columbus) Journal of Pharmacology and Experimental provocative motion stimulus, a signal for sensory conflict activates

271 51 LIFE SCIENCES (GENERAL)

the histaminergic neuron system, and the histaminergic descending effects of combined treatments, it is postulated that the primary impulse stimulates H1-receptors in the emetic center of the brain cause of AVCR changes is an alteration in the distribution of yolk stem. The histaminergic input to the emetic center through platelets and the rearrangement of microtubule arrays. Embryos H1-receptors is independent of dopamine D2-receptors in the with a decreased AVCR exhibited reduced survival in early chemoreceptor trigger zone and serotonin 5HT3-receptors in the developmental stages, indicating serious difficulties in cleavage, visceral afferent, which are also involved in the emetic reflex. blastulation and/or gastrulation. Cold-shocked embryos with a Antihistamines block emetic H1-receptors to prevent motion reduced AVCR could be rescued by D2O pretreatment or sickness. Acetylcholine muscarinic receptors are involved in the clinostating, an observation which supports the notion that changes generation of signals for sensory conflict. Anti-cholinergic drugs accompanying AVCR modifications represent the primary cause prevent motion sickness by modifying the neural store to facilitate of the reduction in percent survival. Author the acquisition of habituation to provocative motion. Author A93-40308* National Aeronautics and Space Administration, A93-39712 Washington, DC. MOTION SICKNESS INDUCED BY SINUSOIDAL LINEAR MICROFOSSILS OF THE EARLY ARCHEAN APEX CHERT - ACCELERATION IN RATS NEW EVIDENCE OF THE ANTIQUITY OF LIFE A. HORII, N. TAKEDA, M. MORITA, T. KUBO, and T. MATSUNAGA J. W. SCHOPF (California Univ., Los Angeles) Science (ISSN (Osaka Univ., Japan) Acta Oto-Laryngologica, Supplement (ISSN 0036-8075) vol. 260, no. 5108 April 30, 1993 p. 640-646. 0365-5237) vol. 501 1993 p. 31-33. refs Copyright (Contract NAGW-825; NGR-05-007-407; NSF BSR-86-13583; The characteristics of linear acceleration to cause motion NAGW-2147) sickness of rats were examined using pica as a behavioral index Copyright of motion sickness. A vestibular sled was used to generate Eleven taxa (including eight heretofore undescribed species) sinusoidal linear acceleration. At 0.4 Hz and with a peak of cellularly preserved filamentous microbes, among the oldest acceleration of 0.15 G, the effectiveness of linear acceleration in fossils known, have been discovered in a bedded chert unit of inducing motion sickness was X-axis greater than Y-axis greater the Early Archean Apex Basalt of northwestern Western Australia. than Z-axis. At 0.4 Hz and along the X-axis, rats suffered from This prokaryotic assemblage establishes that trichomic more severe motion sickness with a high peak G load (0.15 G) cyanobacterium-like microorganisms were extant and morpho- than with a low one (0.08 G). Along the X-axis and with a peak logically diverse at least as early as about 3465 million acceleration of 0.15 G, the severity of motion sickness was not years ago and suggests that oxygen-producing photoautotrophy related to frequency (0.4, 0.6 Hz). Author (revised) may have already evolved by this early stage in biotic history. Author (revised) A93-39715 INHIBITION OF EGF-INDUCED SIGNAL TRANSDUCTION BY A93-40548* National Aeronautics and Space Administration, MICROGRAVITY IS INDEPENDENT OF EGF RECEPTOR Washington, DC. REDISTRIBUTION IN THE PLASMA MEMBRANE OF HUMAN ABSENCE OF A GROWTH HORMONE EFFECT ON RAT A431 CELLS SOLEUS ATROPHY DURING A 4-DAY SPACEFLIGHT P. J. RIJKEN, R. P. DE GROOT, N. VAN BELZEN, S. W. DE BIAN JIANG, ROLAND R. ROY, CHRISTINE NAVARRO, and V. LAAT, J. BOONSTRA, and A. J. VERKLEIJ (Utrecht, R. EDGERTON (California Univ., Los Angeles) Journal of Applied Rijksuniversiteit, Netherlands) Experimental Cell Research (ISSN Physiology (ISSN 8750-7587) vol. 74, no. 2 Feb. 1993 p. 0014-4827) vol. 204, no. 2 Feb. 1993 p. 373-377. 527-531. Research supported by NASA, Pennsylvania State Univ., Copyright and Genentech refs Epidermal growth factor (EGF)-induced c-fos and c-jun Copyright expression is strongly suppressed in microgravity. We investigate The effect of a 4-day-long spaceflight on the size and the here whether this is due to inhibition of processes occurring during enzyme properties of soleus fibers of rats and the effects of the initiation of EGF-induced signal transduction. For this purpose, exogenous growth hormone (GH) on the atrophic response of the EGF-induced receptor clustering is used as a marker. The lateral soleus muscle were investigated in four groups of rats: (1) control, distribution of EGF receptors is directly visualized at an (2) control plus GH treatment, (3) flight, and (4) flight plus GH ultrastructural level by the label-fracture method. Quantification of treatment. Results showed that the fiber size and the type of the receptor distributions shows that EGF-induced receptor myosin heavy chain expressed fibers (but not the metabolic redistribution is similar under normal and microgravity conditions. properties) of the soleus were affected by four days of This suggests that microgravity influences EGF-induced signal weightlessness and that the effects were not ameliorated by the transduction downstream of EGF binding and EGF receptor administration of growth hormone. AIAA redistribution, but upstream of early gene expression in human A431 cells. Author A93-40773 OXYGEN REGIME IN THE FRONTAL CEREBRAL CORTEX OF A93-39717 MONKEYS DURING A TWO-WEEK SPACE FLIGHT ALTERING THE POSITION OF THE FIRST HORIZONTAL [KISLORODNYJ REZHIM LOBNOJ KORY GOLOVNOGO CLEAVAGE FURROW OF THE AMPHIBIAN (XENOPUS) EGG MOZGA OBEZ'YANY V PROTSESSE 2-NEDEL'NOGO REDUCES EMBRYONIC SURVIVAL KOSMICHESKOGO POLETA] H. YOKOTA, A. W. NEFF, and G. M. MALACINSKI (Indiana Univ., V. P. KROTOV, V. A. YUSHIN, A. VATSEK, V. I. KOROL'KOV, A. Bloomington) International Journal of Developmental Biology SHEBELA, A. N. TRUZHENNIKOV, and V. YU. KUNYAEV (ISSN 0214-6282) vol. 36, no. 4 Dec. 1992 p. 527-535. Aviakosmicheskaya i Ekologicheskaya Meditsina (ISSN Copyright 0233-528X) vol. 26, no. 2 Mar.-Apr. 1992 p. 42-46. In The animal/vegetal cleavage ratio (AVCR), defined as the RUSSIAN refs ratio of the height of the animal blastomere to the height of the Copyright Xenopus embryo at the 8 cell stage, can be shifted by placing Changes in the oxygen partial pressure (pO2) in the frontal embryos in novel gravitational fields: clinostating (microgravity cerebral cortex of Macaca mulata monkeys fitted with platinum simulation) increases AVCR, and centrifugation (hypergravity electrodes were measured during a two-week space flight. It was simulation) reduces AVCR. This report contributes to an found that, in monkeys undergoing the space flight, there was an understanding of the subcellular mechanism responsible for the initial increase of pO2, which reached a maxium of 203 percent furrow relocation and assesses its significance. Embryo inversion on days 5-8, followed by normalization by day 11, whereas the and D2O immersion were found to increase AVCR, and cold shock pO2 values in the cortical zone of on-ground control monkeys was found to reduce AVCR. Based on the additive or antagonistic remained at the base level. Results of an analysis of the pO2-curve

272 51 LIFE SCIENCES (GENERAL) oscillations in the frequency range 0.2-0.01 Hz for the in-flight spaceflight rats, but showed no difference between control and monkeys revealed a shift of the oscillation power spectrum in the flight animals after a 9-d recovery. These findings were probably long-wave direction, suggesting a decrease in the rate of tissue due to an acute stress undergone during landing. The NE content metabolism. AIAA was unchanged in the A2 and A5 cell groups. In rats flown aboard SLS-1, the vasopressin content was increased in the posterior A93-41075* National Aeronautics and Space Administration, pituitary, and was significantly decreased in the hypothalamus. Washington, DC. We conclude that the NE depletion in the locus coeruleus and GEOGRAPHY OF END-CRETACEOUS MARINE BIVALVE the alteration in vasopressin release were consistent with an acute EXTINCTIONS stress, likely occurring during and/or after landing. These changes DAVID M. RAUP and DAVID JABLONSKI (Chicago Univ., IL) tend to mask the actual neuroendocrine modifications caused by Science (ISSN 0036-8075) vol. 260, no. 5110 May 14, 1993 microgravity. Author (revised) p. 971-973. refs (Contract NAGW-1508; NAGW-1527; NSF EAR-90-05744; NSF A93-41388 INT-86-2045) RELATIVE RESISTANCE OF BIOFILMS AND PLANKTONIC Copyright CELLS OF COMMON MOLDS AND YEASTS TO Analysis of the end-Cretaceous mass extinction, based on 3514 ANTIMICROBIALS occurrences of 340 genera of marine bivalves (Mollusca), suggests D. G. AHEARN, P. A. GANDHI, L. L. MAY (Georgia State Univ., that extinction intensities were uniformly global; no latitudinal Atlanta), D. L. PRICE (Interface Research Corp., Scottsdale, AZ), gradients or other geographic patterns are detected. Elevated and S. A. CROW (Georgia State Univ., Atlanta) Jul. 1992 7 p. extinction intensities in some tropical areas are entirely a result of SAE, International Conference on Environmental Systems, 22nd, the distribution of one extinct group of highly specialized bivalves, Seattle, WA, July 13-16, 1992 Research supported by Krug Life the rudists. When rudists are omitted, intensities at those localities Sciences, Inc. refs are statistically indistinguishable from those of both the rudist-free (Contract EPA-CR-818696-01-0) tropics and extratropical localities. Author (SAE PAPER 921212) Copyright Various antimicrobials, including benzalkonium chloride, A93-41124 dimethyl benzyl ammonium chloride, chlorhexidine, pofyhexa- MYOSIN AND TROPONIN CHANGES IN RAT SOLEUS methylene biguanide and hydrogen peroxide, were screened MUSCLE AFTER HINDLIMB SUSPENSION for their inhibitory effects against planktonic and adhered MARINA CAMPIONE, SIMONETTA AUSONI, CHARLES Y. cells of selected yeasts and molds. A resistant strain of Serratia GUEZENNEC, and STEFANO SCHIAFFINO (Padova, Univ.; CNR, marcescens was employed as a control. Quaternary compounds Padua, Italy; Centre d'Etudes et des Recherches de Medecine often merely damaged cells; recoveries varied with the neutralizing Aerospatiale, Bretigny-sur-Orge, France) Journal of Applied medium and whether agar or broths were used. In general, Physiology (ISSN 8750-7587) vol. 74, no. 3 March 1993 p. quaternary compounds and biguanides at concentrations of less 1156-1160. Research supported by ASI refs than 1.0 percent gave static inhibition, but with borate ions present Copyright biocidal activity was observed for certain compounds. Cells dried We examined the myosin heavy-chain (MHC), troponin T (TriT), to polyethylene surfaces were usually more resistant to disinfectant and troponin I (Tnl) isoform composition in the rat soleus muscle concentrations than planktonic cells, but in a few instances dried after 21 days of hindlimb suspension using electrophoretic and biofilms showed increased susceptibility. Molds such as Aspergillus immunoblotting analysis with specific monoclonal antibodies. The flavus and A. furmigatus were more resistant to certain biguanides suspended soleus showed a shift in the MHC isoform distribution than the yeasts Candida albicans and C. parapsilosis. Hydrogen with a marked increase (from 1.0 to 33 percent) in the relative peroxide tested at a maximum concentration of 3.0 percent, in amount of type lla and llx MHC and a corresponding decrease in general, was one of the most effective disinfectants for adhered type I MHC. However, type lib MHC, which represents a major and planktonic cells. Author component in fast-twitch muscles, was not detected in suspended soleus muscles. TnT and Tnl isoform composition was also A93-41390* National Aeronautics and Space Administration. changed with the appearance of fast-type Tnl and TnT bands. Lyndon B. Johnson Space Center, Houston, TX. However, a high-mobility TnT band, which represents a major EFFECTS OF REFRIGERATING PREINOCULATED VITEK component in fast-twitch muscles, was not expressed in the CARDS ON MICROBIAL PHYSIOLOGY AND ANTIBIOTIC suspended soleus. These isoform transitions may be related to SUSCEPTIBILITY the increased maximal velocity of shortening and higher calcium JOYCE A. SKWERES, VIRGINIA J. BASSINGER, S. K. MISHRA sensitivity previously reported in the rat soleus after hindlimb (Krug Life Sciences, Inc., Houston, TX), and DUANE L. PERSON suspension. Author (revised) (NASA, Johnson Space Center, Houston, TX) Jul. 1992 11 p. SAE, International Conference on Environmental Systems, 22nd, A93-41167* National Aeronautics and Space Administration. Seattle, WA, July 13-16, 1992 refs Ames Research Center, Moffett Field, CA. (SAE PAPER 921214) Copyright NOREPINEPHRINE CONTENT IN DISCRETE BRAIN AREAS Reference cultures of 16 microorganisms obtained from the AND NEUROHYPOPHYSIAL VASOPRESSIN IN RATS AFTER A American Type Culture Collection and four clinical isolates were 9-D SPACEFLIGHT (SLS-1) used in standardized solutions to inoculate 60 cards for each test JEANNETTE FAREH, JEAN-MARIE COTTET-EMARD, strain. A set of three ID and three susceptibility cards was JEAN-MARC PEQUIGNOT (Lyon I, Univ., France), GARY JAHNS processed in the Vitek AutoMicrobic System (AMS) immediately (NASA, Ames Research Center, Moffett Field, CA), JOHN MEYLOR after inoculation. The remaining cards were refrigerated at 4 C, (Lockheed Engineering & Sciences Co.; NASA, Ames Research and sets of six cards were removed and processed periodically Center, Moffett Field, CA), MICHEL VISO, DIDIER VASSAUX for up to 17 days. The preinoculated AMS cards were evaluated (CNES, Paris, France), GUILLEMETTE GAUQUELIN, and CLAUDE for microorganism identification, percent probability of correct GHARIB (Lyon I, Univ., France) Aviation, Space, and identification, length of time required for final result, individual Environmental Medicine (ISSN 0095-6562) vol. 64, no. 6 June substrate reactions, and antibiotic minimal inhibitory/concentration 1993 p. 507-511. Research supported by DRET and CNES (MIC) values. Results indicate that 11 of the 20 microbes tested refs withstood refrigerated storage up to 17 days without detectable Copyright changes in delineating characteristics. MIC results appear variable, The norepinephrine (NE) content in discrete brain areas and but certain antibiotics proved to be more stable than others. The the vasopressin content in the neurohypophysial system were results of these exploratory studies will be used to plan a assessed in rats after a 9-d spaceflight and after a recovery period. microgravity experiment designed to study the effect of microgravity The NE content in the locus coeruleus decreased significantly in on microbial physiology and antibiotic sensitivity. Author

273 51 LIFE SCIENCES (GENERAL)

A93-41391 National Aeronautics and Space Administration. required. The trade-offs between these two types of sensors are Lyndon B. Johnson Space Center, Houston, TX. based on engineering constraints, sensitivity spectra, and the quality ALTERED IMMUNOLOGICAL RESPONSE IN MICE of imagery possible from each type. This paper presents results SUBJECTED TO STRESS AND EXPOSED TO FUNGAL of a study conducted by the Biological Flight Research Projects SPORES Office in conjunction with the Spacecraft Data Systems Branch at VISWANATH P. KURUP, HONGYUNG CHOI, ANOOPA KUMAR, ARC to investigate the use of charged-coupled-device and IR PAZHAYANNUR S. MURALI (Wisconsin Medical College, cameras to meet the scientific requirements. Also examined is Milwaukee), S. K. MISHRA (Krug Life Sciences, Inc., Houston, the effect of low levels of near-IR illumination on the circadian TX), and DUANE L PERSON (NASA, Johnson Space Center, rhythm in rats. Author Houston, TX) Jul. 1992 9 p. SAE, International Conference on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 N93-27122'# Umpqua Research Co., Myrtle Creek, OR. Research supported by NASA, Krug Life Sciences, Inc., and Aerospace Div. USVA refs REGENERABLE BIOCIDE DELIVERY UNIT, VOLUME 1 Final (SAE PAPER 921215) Copyright Report Space flight and related factors such as stress appear to have JAMES E. ATWATER and RICHARD R. WHEELER, JR. Sep. an adverse effect on astronauts' immune systems. The presence 1992 310 p of potentially pathogenic microbes including several genera of fungi (Contract NAS9-18361) reported from spacecraft environment may be a cause of concern (NASA-CR-185701; NAS 1.26:185701; URC-80356) Avail: CASI in such situations. In order to study the role of such organisms in HC A14/MF A03 causing opportunistic or allergic diseases in crewmembers, we The Microbial Check Valve (MCV), which is currently used have tried to develop an animal model. BALB/c mice were aboard the Shuttle Orbiter for disinfection of the potable water suspended upside down for varying periods of time to induce supply, is an expendable flow-through canister containing iodinated stress, and their lymphocyte functions were evaluated. These ion exchange resin. Means for extension of MCV life are desirable studies indicate that the stress resulted in lowered mitogen induced to avoid resupply penalties. The Phase 1 Regenerate Biocide lymphocyte stimulation as represented by 3H-thymidine uptake. Delivery Unit program demonstrated the feasibility of regenerating We have also studied the ability of these animals to respond to an MCV in situ, using a strong aqueous elemental iodine solution Aspergillus fumigatus spores. The results of the study clearly resulting from diversion of the MCV influent to a packed bed demonstrate a definite down-regulation in T-cell proliferation and containing iodine crystals. In small column tests, eight manual a higher incidence of infection with A. fumigatus. regenerations of an MCV resin were accomplished. The term Author (revised) Regenerative Microbial Check Valve (RMCV) was adopted describing this new technology. The Phase 2 program resulted in A93-41520* National Aeronautics and Space Administration, the development of a full scale and fully autonomous prototype Washington, DC. RMCV, capable of maintaining residual l(sub 2) levels between INACTIVATION OF A MODEL COLIPHAGE VIRUS IN WATER 2.0 - 4.0 mg/L for prolonged periods. During six months of testing BY IODINE at the Space Station baseline flow rate of 120 cm(sup 3)/min, GAIL M. BRION and JOANN SILVERSTEIN (Colorado Univ., the prototype RMCV underwent nine regenerations. RMCV life Boulder) Jul. 1992 9 p. SAE, International Conference on cycle tests, using a variety of influent streams, were conducted Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 over an eighteen month period to determine the useful lives of Research supported by NASA refs MCV's incorporating this new technology and to determine ultimate (SAE PAPER 921361) Copyright failure mechanisms. MCV life extensions of 130 fold were Until now, NASA's space water reuse research program has demonstrated, limited only by the Phase 2 performance period. not considered the transport of water-borne infectious enteric Based upon this work, it is certain that RMCV units can be viruses; however, viral diseases probably are a signifficant concern developed to provide unattended biocide addition for the thirty in long-duration space missions. To simplify monitoring and year life of Space Station Freedom, or for other longer duration prediction of pathogen distribution, model indicator strains applications such as a Lunar Base or Mars mission. RMCV historically have been used. In this research, the male specific technology was also demonstrated capable of delivering, on RNA coliphage MS-2 is used as a model of enteric viruses due to demand, a concentrated aqueous l(sub 2) solution for potential their similar size and biochemical composition. Inactivation of some use as a disinfectant during transient episodes of microbial surface water-borne enteric viruses by iodine has previously been contamination, for the control of biofilm formation, or as a characterized. In this paper, iodine inactivation of the model preventative measure in systems which are particularly susceptible coliphage MS-2 in buffered water is compared with earlier to the growth of microorganisms. Author (revised) bench-scale disinfection survival data and with survival in iodinated Simulated shower water used in a test water recycling system. N93-27152# Civil Aeromedical Inst., Oklahoma City, OK. Author (revised) VARIATIONS OF TIME-TO-INCAPACITATION AND CARBOXYHEMOGLOBIN VALUES IN RATS EXPOSED TO A93-41551 National Aeronautics and Space Administration. Ames TWO CARBON MONOXIDE CONCENTRATIONS Final Report Research Center, Moffett Field, CA. DONALD C. SANDERS, BOYD R. ENDECOTT, ROXANE M. DARK CYCLE MONITORING OF BIOLOGICAL SPECIMENS ON RITTER, and ARVIND K. CHATURVEDI May 1993 18 p SPACE STATION FREEDOM (DOT/FAA/AM-93/7) Avail: CASI HC A03/MF A01 ARSHAD MIAN and SHERRY CHUANG (NASA, Ames Research It has been suggested that passenger protective breathing Center, Moffett Field, CA) Jul. 1992 9 p. SAE, International equipment protect aircraft passengers from smoke for 5 min during Conference on Environmental Systems, 22nd, Seattle, WA, July an evacuation phase and for 35 min during an 13-16, 1992 Previously announced in STAR as N93-19103 in-flight-plus-evacuation phase. Carbon monoxide (CO) is one of refs the most abundant smoke components and is the major threat in (Contract RTOP 476-14-03) most fire atmospheres. Time-to-incapacitation (t(sub i)) is an (SAE PAPER 921393) Copyright end-point related to escape from a fire, and variations in t(sub i) The operational environment for biological research on Space measurements at specific CO concentrations have not been Station Freedom will incorporate video technology for monitoring statistically documented. Therefore, variance in t(sub i) at two CO plant and animal subjects. The video coverage must include concentrations that produce 5- and 35-min t(sub i) in rats were dark-cycle monitoring because early experiments will use rodents determined; blood carboxyhemoglobin (COHb) saturation at t(sub that are nocturnal and therefore most active during the dark part i) was measured. Fifty male Sprague-Dawley rats were individually of the daily cycle. Scientific requirements for monitoring during exposed to each CO concentration in a chamber equipped with a the dark cycle are exacting. Infrared (IR) or near-IR sensors are rotating cage, and t(sub i) was recorded as the time from insertion

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of the animal into the cage until it could no longer walk. In another (FOA-B-40419-4.4; ETN-93-93764) Avail: CASI HC A01/MF set of experiments, blood COHb saturation was determined in A01 rats exposed to these CO concentrations at stepwise intervals The expression of virulence plasmid encoded virulence less than t(sub i). At incapacitation and at the end of each exposure determinants is discussed and it is concluded that the three virulent interval, rats were quickly removed from the cage and killed for species of Yersinia contain homologous virulence plasmids that blood collection and COHb quantization. Values (mean +/- SD) encode a number of temperature inducible Ca(2+) regulated for measured parameters were: for the 5-min t(sub i) study, CO proteins (Yops (Yersinia outer membrane proteins)). Mapping and = 5706 + /- 178 ppm, t(sub i) = 5.0 + /- 0.36 min, and COHb regulation of Yop genes is discussed and it is concluded that the ' = 80.8 +/- 1.3%; for the 35-min t(sub i) study, CO = 1902 +/- expression of the Yops is regulated at the level of transcription 33 ppm, t(sub i) = 34.8 + /- 6.8 min, and COHb = 71.2 +/- involving negative as well as positive control elements encoded 1.0%. COHb levels tended to plateau prior to incapacitation. by the Ca(2+) region. Work which resulted in the conclusion that Coefficients of variation for t(sub i) were 7.2% and 19.5% for the YopH and YopE are essential virulence determinants which obstruct ! 5- and 35-min study, respectively. The significant difference in the the primary host defense by preventing phagocytosis is I two COHb levels and the approach of COHb to a maximal level discussed. ESA i before incapacitation suggest that blood COHb saturation levels I may not necessarily be indicative of the onset of incapacitation. ' Author (revised) N93-28200# National Defence Research Establishment, Umea i (Sweden). Microbiology Div. CHARACTERIZATION AND CLASSIFICATION OF STRAINS OF N93-27360*# Umpqua Research Co., Myrtle Creek, OR. FRANCISELLA TULARENSIS ISOLATED IN THE CENTRAL Aerospace Div. ASIAN FOCUS OF THE SOVIET UNION AND IN JAPAN I REGENERABLE BIOCIDE DELIVERY UNIT, VOLUME 2 Final G. SANDSTROEM, A. SJOESTEDT, M. FORSMAN, N. V. ) Report PAVLOVICH (Rostov State Univ., Rostov-on-Don, USSR.), and B. I JAMES E. ATWATER and RICHARD R. WHEELER, JR. Sep. N. MISHANKIN (Rostov State Univ., Rostov-on-Don, USSR.) Jan. | 1992 98 p 1992 4 p Repr. from Journal of Clinical Microbiology, v. 30, i (Contract NAS9-18361) no. 1, Jan. 1992 p 172-175 , (NASA-CR-185701-VOL-2; NAS 1.26:185701-VOL-2; URC-80356) (FOA-B-40421-4.4; ETN-93-93766) Copyright Avail: CASI HC { Avail: CASI HC A05/MF A02 A01/MF A01 Source code for programs dealing with the following topics An experiment which suggests that classification of strains of ' are presented: (1) life cycle test stand-parametric test stand control Francisella on the basis of 16S rRNA analysis may be preferable (in BASIC); (2) simultaneous aqueous iodine equilibria-true to classification on the basis of biochemical analysis is described equilibrium (in C); (3) simultaneous aqueous iodine and results and conclusions given. The two subspecies of equilibria-pseudo-equilibrium (in C); (4) pseudo-(fast)-equilibrium Francisella tularensis, F. tularensis subsp. tularensis (type A) and with iodide initially present (in C); (5) solution of simultaneous F. tularensis subsp. palaearctica (type B), differ from each other iodine rate expressions (Mathematica); (6) 2nd order kinetics of in biochemistry and virulence. Strains of type A are believed to 12-formic acid in humidity condensate (Mathematica); (7) prototype be confined to North America, whereas strains of type B occur in RMCV onboard microcontroller (CAMBASIC); (8) prototype RAM Europe, in Asia, and in North America. Moreover, the existence of data dump to PC (in BASIC); and (9) prototype real time data two other subspecies, designated F. tularensis subsp. mediaasiatica transfer to PC (in BASIC). CASI and F. tularensis subsp. palaearctica japonica, has been suggested for strains of F. tularensis isolated in the central Asian focus of N93-27989# National Defence Research Establishment, Umea the Soviet Union and in Japan, respectively. Strains biochemically (Sweden). Microbiology Div. classified as F. tularensis subsp. mediaasiatica or F. tularensis INTRACELLULAR TARGETING OF THE YERSINIA YOPE subsp. palaeartica japonica were investigated by hybridization with CYTOTOXIN IN MAMMALIAN CELLS INDUCES ACTIN probes specific to 16S rRNAs of the two main species. Furthermore, MICROFILAMENT DISRUPTION the virulence and biochemical characteristics of the strains were ROLAND ROSQVIST, AAKE FORSBERG, and HANS WOLF-WATZ compared with those of strains belonging to type A and type B. It (Umea Univ., Sweden.) Dec. 1991 8 p Sponsored in part by was found that 16S rRNAs of F. tularensis subsp. mediaasiatica Swedish Board of Technical Development Repr. from Infection and F. tularensis subsp. palaeartica japonica hybridize with the and Immunity, v. 59, no. 12, Dec. 1991 p 4562-4569 probe specifc to a geniotype proposed, genotype A (type A), which (Contract SMRC-07490-5A; SNSRC-4426-3011) (ISSN shows that strains genetically related to this subspecies are found 0281-0263) outside North America. However, the central Asian strains differed (FOA-B-40420-4.4; ETN-93-93765) Copyright Avail: CASI HC • from type A and type B strains when investigated by fermentation A02/MF A01 of glucose. It was concluded that the results of the biochemical An experiment which showed that isolated Yop (Yersinia outer tests could not be unambiguously used for differentiation of strains membrane proteins) present in Pathogenic Yersinia spp. that into F. tularensis subsp. palaearctica or F. tularensis subsp. encode a number of essential virulence determinants, cause cytoxic tularensis. ESA; ; effects in vitro if the proteins are introduced intracellulary into the i ! eukaryotic cell, is described. Isolated Yop proteins of Yersinia i N93-28212# National Defence Research Establishment, Umea • pseudotuberculosis were found to disrupt the microfilament (Sweden). Cell Biology and Microbiology Dept. structure only when microinjected intracellulary into the host cell. USE OF RNA HYBRIDIZATION IN THE DIAGNOSIS OF A In particular, YopE was demonstrated to be directly involved in CASE OF ULCEROGLANDULAR TULAREMIA I the cytotoxication, whereas YopD seems to have a critical role in M. FORSMAN, K. KUOPPA, A. SJOESTEDT, and A. TAERNVIK I translocating the YopE protein through the host cell membrane. (Umea Univ., Sweden.) 1990 2 p Repr. from Eur. J. Clin. These results elucidate the requirement for at least some of the Microbiol. Infect Dis., v. 9, 1990 p 784-785 Yop proteins to leave the pathogen during infection. ESA (FOA-B-40422-4.4; ETN-93-93767) Avail: CASI HC A01/MF i A01 N93-28199# National Defence Research Establishment, Umea A case study in which 16S ribosomal RNA of Francisella (Sweden), Cell and Microbiology Dept. tularensis were successfully used in the diagnosis of a wound PLASMID ENCODED VIRULENCE OF YERSINIA specimen from a patient with ulceroglandular tularemia is presented. H. WOLF-WATZ, A. FORSBERG, R. ROSQVIST, I. BOELIN, K. A genus specific probe was constructed from the 16S ribosomal ERICKSON, L NORLANDER, M. RIMPILAEINEN, T. BERGMAN, RNA which was used in the diagnosis. It was shown that the i and S. HAAKANSSON 1991 5 p Prepared in cooperation hybridization technique is much more rapid than culture procedures with Umea Univ., Sweden and carries a lower risk of laboratory infection. As illustrated, the

275 51 LIFE SCIENCES (GENERAL)

hybridization procedure is also useful for determination of the some transcripts are increased in cells exposed to EM fields. Francisella tularensis biovar. ESA While the research is basic in nature, the ramifications have bearing on the general safety of exposure to EM fields in industrial and N93-28415*# Pennsylvania State Univ., University Park. everyday life. A large array of diverse biological effects are reported ELECTROPHORETIC SEPARATION OF CELLS AND to occur as the result of exposure to elf EM fields, suggesting PARTICLES FROM RAT PITUITARY AND RAT SPLEEN Final that the cell response to EM fields is at a basic level, presumably Report, period ending 31 Mar. 1993 initiated by molecular and/or biophysical events at the cell WESLEY C. HYMER 31 Mar. 1993 81 p membrane. The hypothesized route is a signal transduction pathway (Contract NAG8-807) involving membrane calcium fluxes. Information flow resulting from (NASA-CR-193073; NAS 1.26:193073) Avail: CASI HC A05/MF signal transduction can mediate the induction of regulatory factors A01 in the cell, and directly affect how transcription is regulated. There are 3 parts to the IML-2 TX-101 experiment. Part 1 is DOE a pituitary cell culture experiment. Part 2 is a pituitary cell separation experiment using the Japanese free flow electrophoresis unit N93-28890# Oak Ridge National Lab., TN. (FFEU). Part 3 is a pituitary secretory granule separation experiment INTRODUCTIONS TO THE PROCEEDINGS OF THE using the FFEU. The objectives of this three part experiment are: FOURTEENTH SYMPOSIUM ON BIOTECHNOLOGY FOR (1) to determine the kinetics of production of biologically active FUELS AND CHEMICALS growth hormone (GH) and prolactin (PRL) in rat pituitary GH and J. WOODWARD, C. E. WYMAN (Midwest Research Inst., Golden, PRL cells in microgravity (micro-g); (2) to investigate three CO.), and B. J. GOODMAN (Midwest Research Inst., Golden, mechanisms by which a micro-g-induced lesion in hormone CO.) 1992 9 p Symposium held in Gatlinburg, TN, 11-15 production may occur; and (3) to determine the quality of May 1992 separations of pituitary cells and organelles by continuous flow (Contract DE-AC05-84OR-21400; DE-AC02-83CH-10093) electrophoresis (CFE) in micro-g under conditions where (DE93-006235; CONF-920508-6) Avail: CASI HC A02/MF A01 buoyancy-induced convection is eliminated. Author (revised) This report is a collection of introductions to sessions made at the Fourteenth Symposium on Biotechnology for Fuels and N93-28651# Massachusetts Inst. of Tech., Cambridge. Center Chemicals. DOE for Environmental Health Sciences. COMPARATIVE MUTAGENESIS OF HUMAN CELLS IN VIVO N93-28952*# National Aeronautics and Space Administration. AND IN VITRO Marshall Space Flight Center, Huntsville, AL. W. G. THILLY May 1993 23 p AMINO ACID SEQUENCES FOR THE BINDING REGIONS IN (Contract DE-FG02-86ER-60448) SERUM ALBUMIN PROTEINS Patent Application (DE93-012269; DOE/ER-60448/T6) Avail: CASI HC A03/MF DANIEL C. CARTER, inventor (to NASA) 1 Mar. 1993 17 p A01 (NASA-CASE-MFS-28402-1; NAS 1.71:MFS-28402-1; This annual progress report describes advances made in US-PATENT-APPL-SN-024547) Avail: CASI HC A03/MF A01 combining denaturing gradient gel electrophoresis with high fidelity In accordance with the present invention, biologically active DNA amplification and with mismatch amplification (MAMA) along protein fragments can be constructed which contain only those with advances in high efficiency restriction enzyme digestion of specific portions of the serum albumin family of proteins such as wild type sequences. Also, theoretical studies on gene mutations regions known as subdomains MA and IMA which are primarily in oncogenesis are described. DOE responsible for the binding properties of the serum albumins. The artificial serums that can be prepared from these biologically active N93-28683# Joint Publications Research Service, Arlington, VA. protein fragments are advantageous in that they can be produced JPRS REPORT: SCIENCE AND TECHNOLOGY. CENTRAL much more easily than serums containing the whole albumin, yet EURASIA: LIFE SCIENCES still retain all or most of the original binding potential of the full 30 Mar. 1993 32 p Transl. into ENGLISH from various Russian albumin proteins. In addition, since the protein fragment serums articles of the present invention can be made from non-natural sources (JPRS-ULS-93-005) Avail: CASI HC A03/MF A01 using conventional recombinant DNA techniques, they are far safer Translated articles cover the following topics: aerospace than serums containing natural albumin because they do not carry medicine; agricultural science; biotechnology; environment; the potentially harmful viruses and other contaminants that will be immunology; laser bioeffects; medicine; microbiology; physiology; found in the natural substances. NASA public health; psychology; and radiation biology. CASI

N93-28684# Joint Publications Research Service, Arlington, VA. N93-29174*# National Aeronautics and Space Administration. JPRS REPORT: SCIENCE AND TECHNOLOGY. CENTRAL Marshall Space Flight Center, Huntsville, AL. EURASIA: LIFE SCIENCES PROCESS FOR SELECTIVELY RECOVERING ALGAE AND 30 Dec. 1992 65 p Transl. into ENGLISH from various Russian PROTOZOA Patent Application articles DAVID A. NOEVER, inventor (to NASA) (Universities Space (JPRS-ULS-92-027) Avail: CASI HC A04/MF A01 Research Association, Huntsville, AL.) 12 Apr. 1993 8 p Translated articles cover the following topic: aerospace (NASA-CASE-MFS-26124-1-NPO; NAS 1.71:MFS-26124-1-NPO; medicine; biochemistry; biotechnology; environment; epidemiology; US-PATENT-APPL-SN-045142) Avail: CASI HC A02/MF A01 genetics; medicine; pharmacology and toxicology; physiology; A process is presented for selectively recovering swimming psychology; and radiation biology. CASI microorganisms from a liquid wherein the liquid is placed in a container and the container is rotated such that the coriolis force N93-28848# Hunter Coll., New York, NY. and the swimming activity of the microorganisms cause the GENE TRANSCRIPTION AND ELECTROMAGNETIC FIELDS microorganisms to concentrate in rings at different radii from the A. S. HENDERSON 1992 7 p axis of rotation of the liquid. Liquid is withdrawn from the container (Contract DE-FG01-89CE-34023) at different distances from the axis of rotation of the container to (DE93-010854; DOE/CE-34023/T1) Avail: CASI HC A02/MF selectively recover the microorganisms. NASA A01 Our overall aim is to obtain sufficient information to allow us N93-29181# Ohio State Univ., Columbus. Research to ultimately determine whether ELF EM field exposure is an Foundation. initiating factor in neoplastic transformation and/or if exposure can REGULATION OF ALTERNATIVE CO2 FIXATION PATHWAYS mimic characteristics of the second-step counterpart in neoplastic IN PROCARYOTIC AND EUCARYOTIC PHOTOSYNTHETIC disease. This aim is based on our previous findings that levels of ORGANISMS

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1992 3 p A06/MF A02; Original German version available from DLR, (Contract DE-FG02-91ER-20033) Wissenschaftliches Berichtswesen, VB-PL-DO, Postfach 90 60 58, (DE93-012109; DOE/ER-20033/1) Avail: CASI HC A01/MF A01 5000 Cologne, Germany, HC The major goal of this project is to determine how Ultraviolet action spectra of inactivation were compared microorganisms regulate the assimilation of CO2 via pathways between wet and dry state spores of the Streptomyces griseus. alternative to the usual Calvin reductive pentose phosphate In vacuum, the spores are more resistant to UV by a factor of 2 scheme. In particular, we are interested in the molecular basis for than under wet conditions. Their photoreactivability is reduced. switches in CO2 metabolic paths. Several earlier studies had The cross sections for induction of DNA (Deoxyribonucleic Acid) indicated that purple nonsulfur photosynthetic bacteria assimilate double strand breaks and for inactivation show similar dependence significant amounts of CO2 via alternative non-Calvin routes. We on wavelengths. ESA have deleted the gene that encodes. RubisCo (ribulose bisphosphate carboxylase/oxygenase) in both the Rhodobacter sphaeroids and Rhodospirillum rubrum. The R. sphaeroides RubisCO deletion strain (strain 16) could not grow under 52 photoheterotrophic conditions with malate as electron donor and CO2 as the electron acceptor; however the R. rub RubisCO deletion AEROSPACE MEDICINE strain (strain 1-19) could. Over the past year we have sought to physiologically characterize strain 16PHC. We found that, 16PHC Includes physiological factors; biological effects of radiation; and exhibited rates of whole-cell CO2 fixation which were significantly effects of weightlessness on man and animals. higher than strain 16. Strain 16PHC could not grow photolithoautotrophically in a CO2 atmosphere; however, CO2 fixation catalyzed by photoheterotrophically grown 16PHC was A93-39261* National Aeronautics and Space Administration. repressed by the addition of DMSO. Likewise, we found that cells Langley Research Center, Hampton, VA. initially grown in the presence of DMSO could induce the CO2 RADIATION EXPOSURE PREDICTIONS FOR fixation system when DMSO was removed. Thus, these results SHORT-DURATION STAY MARS MISSIONS suggested that both PHC and 1-19 could be used to study alternative SCOTT A. STRIEPE, JOHN E. NEALY, and LISA C. SIMONSEN CO2 fixation reactions and their significance in R. sphaexoides (NASA, Langley Research Center, Hampton, VA) Journal of and R. rubrum. DOE Spacecraft and Rockets (ISSN 0022-4650) vol. 29, no. 6 Nov.-Dec. 1992 p. 801-807. AAS and AIAA, Spaceflight N93-29216*# Texas A&M Univ., College Station. Research Mechanics Meeting, Colorado Springs, CO, Feb. 24-26, 1992 Foundation. refs GROWING WHEAT TO MATURITY IN REDUCED GAS (AAS PAPER 92-107) Copyright PRESSURES Final Report, 1 Apr. 1992 - 30 Jun. 1993 The human radiation environment for several short-duration stay EDWARD J. RYKIEL, JR., MALCOLM C. DREW, and BRAD D. manned Mars missions is predicted using the Mission Radiation ETTER 30 Jun. 1993 70 p Calculation program, which was developed at NASA Langley (Contract NAG9-582) Research Center. This program provides dose estimates for (NASA-CR-193245; MAS 1.26:193245) Avail: CASI HC A04/MF Galactic cosmic rays (GCR) and large and ordinary solar proton A01 flare events for various amounts of effective spacecraft shielding The main objective of this project was to determine assimilation and a given time history of the spacecraft's heliocentric position. of CO2 and efficiency of water use in wheat grown to maturity in The results of this study show that most of the missions can a low pressure total gas pressure environment. A functional test survive the most recent large flares if a 25 g/sq cm storm shelter of the low pressure plant growth chamber system was is assumed. The dose predictions show that missions during solar accomplished in February and March of 1993 wherein this objective minima are not necessarily the minimum dose cases, due to was partially achieved. Plants were grown to maturity in the increased GCR contribution during this time period. The direct chambers. Data were actively collected during the first 29 days. transfer mission studied has slightly lower doses than the outbound The plants were allowed to maintain themselves at the CO2 Venus swingby mission, with the greatest dose differences for the compensation point until day 45 of the study at which point active assumed worst case scenario. The GCR dose for a mission can atmospheric regulation was resumed. This provided data at the be reduced by having the crew spend some fraction of its day vegetative and reproductive stages of the life cycle of the plants. nominally in the storm shelter. Author (revised) However, this information may not be representative of the performance of the plants due to the loss of low pressure on a A93-39704* National Aeronautics and Space Administration. number of days during the study, which affected the plants by Lyndon B. Johnson Space Center, Houston, TX. changing the pressure potential of the tissues. The performance HUMAN PERFORMANCE AND PHYSIOLOGICAL FUNCTION of the system will be discussed on a component by component DURING A 24-HR EXPOSURE TO 1 PERCENT basis. The maintenance of the plants at the CO2 compensation BROMOTRIFLUOROMETHANE (HALON 1301) point was driven by the failure of the computer program operating D. S. CALKINS, J. J. DEGIOANNI, M. N. TAN, J. R. DAVIS, and the system. The software problems that arose during the functional D. L PIERSON (Krug Life Sciences; NASA, Johnson Space Center, test have since been corrected. Results from the functional test Houston, TX) Fundamental and Applied Toxicology (ISSN also indicated that the plants were not receiving adequate light 0272-0590) vol. 20, no. 2 Feb. 1993 p. 240-247. and nutrients. The growth chambers have been relocated and the Copyright growth room modified to compensate for these deficiencies. Performance and physiological measurements were obtained Derived from text from four pairs of men exposed for 24 hr to 1 percent (10,000 ppm) Halon 1301 (CBrFS) and to air with order counterbalanced N93-29274# European Space Agency, Paris (France). using a double-blind protocol. Cognitive and motor performance PHOTOBIOLOGICAL INVESTIGATIONS ON SPORES OF was assessed before, during, and after the exposures, using seven STREPTOMYCES GRISEUS scales of the Automated Portable Testing System, which produced BIRGIT KELLER (Deutsche Forschungsanstalt fuer Luft- und 13 measures of performance. Halon inhalation induced decrements Raumfahrt, Cologne, Germany.) Nov. 1992 118 p Transl. in 2 of the 13 measures, but actual and estimated magnitudes of into ENGLISH of Photobiologische Untersuchungen an Sporen von the decrements were no greater than 5 percent of baseline values. Streptomyces griseus (Cologne, Germany, DLR) Mar. 1991 p Physiological data obtained before, during, and after the exposures 1-111 Original language document was announced as revealed significant changes during Halon inhalation for 6 of the N91-32748 52 variables assessed; however, all physiological values remained (ESA-TT-1269; DLR-FB-91-14; ETN-93-93715) Avail: CASI HC within clinically acceptable limits. No cardiovascular effects were

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noted. This study demonstrated that exposure to 1 percent Halon produced by parabolic flight on board a KC-135 aircraft. Intraocular 1301 for 24 hr can produce minor disturbance of central nervous pressures increased 58 percent during parabolic flight compared system function as assessed by cognitive tasks. Author (revised) to baseline values (19 +/- 1 mm Hg vs 12 +/- 1 mm Hg, respectively; P less than 0.001). A 4 percent reduction in the A93-39705* National Aeronautics and Space Administration. caliber of retinal arteries was also noted during microgravity, but Lyndon B. Johnson Space Center, Houston, TX. this change did not achieve statistical significance. The increase TOXICOKINETICS OF INHALED BROMOTRIFLUOROMETHANE in the intraocular pressure and the trend of arteries to constrict (HALON 1301) IN HUMAN SUBJECTS are thought to result from cephalad shifts in intravascular and C. W. LAM, F. W. WEIR, K. WILLIAMS-CAVENDER, M. N. TAN, extravascular body fluids as a result of the absence of the 1g T. J. GALEN, and D. L PIERSON (NASA, Johnson Space Center, hydrostatic gradient. The results of our study confirm that this Houston, TX) Fundamental and Applied Toxicology (ISSN fluid shift and its effects on the eye occur rapidly, within 20 seconds 0272-0590) vol. 20, no. 2 Feb. 1993 p. 231-239. of exposure to microgravity. Author (revised) Copyright Bromotrifluoromethane (Halon 1301, CBrF3), is used as a fire A93-39713 extinguishant in the Space Shuttle, where several scenarios, such LONG-LASTING NEUROPSYCHOLOGICAL CHANGES AFTER as a fire or a faulty alarm, could lead to its discharge resulting in A SINGLE HIGH ALTITUDE CLIMB a Halon 1301 concentration of up to 1 percent in the cabin G. CAVALETTI and G. TREDICI (Inst. for Biomedical Sciences, atmosphere. The effect of Halon 1301 on mental performance Monza, Italy) Acta Neurologica Scandinavica (ISSN 0001-6314) and physiologic function was investigated in a NASA-sponsored vol. 87, no. 2 Feb. 1993 p. 103-105. human inhalation study in which four pairs of male subjects were Copyright each exposed in a double-blind fashion for 24 hr to 1 percent Acute neuropsychological changes due to high altitude climbing Halon 1301 and to air in two exposures about 1 week apart. without supplementary oxygen are well known. However, many Blood and breath samples from the exposed subjects were climbers report vague symptoms of brain dysfunction after return collected to provide dosimetric and toxicokinetic information. Halon to sea level, suggesting that long-lasting neuropsychological 1301 blood levels increased rapidly and approached a steady state impairment may ensue even after a single ascent. In this study, within 2 hr of the beginning the exposure; the steady-state we evaluated a series of neuropsychological functions in a group concentration was approximately 3-4.5 microg/ml. Breath samples of 11 climbers who ascended over 5000 m. Besides memory collected during exposures closely reflected chamber impairment, reaction time and concentration were also less efficient concentrations. Analysis of postexposure blood samples revealed when the climbers were evaluated 75 days after their return to that Halon 1301 was eliminated biphasically with an average t(1/2) sea level, confirming that even a single high altitude climb may alpha and t(112) beta of 4.5 min and 200 min, respectively. be harmful for central nervous system functions. Author (revised) Author (revised)

A93-39706 A93-39714 BAROTRAUMA IN BOEING 737 CABIN CREW THE PREDICTION OF THE ADAPTATION OF ORCADIAN H. W. KORTSCHOT and W. J. OOSTERVELD (Academical Medical RHYTHMS TO RAPID TIME ZONE CHANGES Centre, Amsterdam, Netherlands) ORL: Journal for S. SUVANTO, M. HARMA, and J. T. LAITINEN (Inst. of Oto-rhino-laryngology and Its Related Specialties (ISSN Occupational Health, Vantaa, Finland) Ergonomics (ISSN 0301-1569) vol. 55, no. 2 Mar.-Apr. 1993 p. 114-116. 0014-0139) vol. 36, no. 1-3 Jan.-Mar. 1993 p. 111-116. Copyright Copyright Several aircrew members of a Boeing 737 aircraft were referred Factors which could explain individual differences in the to our department because they suffered from a barotrauma. The ^synchronization speed of circadian rhythms of salivary melatonin fast rate of pressure change during the descent of a Boeing 737 and subjective alertness after transmeridian flights over 10 time aircraft, as compared to the Boeing 747, DC-10 and Airbus 310 zones were investigated. The data were gathered in female subjects aircrafts, is most likely the cause of the development of the aged 33.0 +/- 6.9 years by measurements of the circadian rhythms barotraumata. Author of melatonin excretion and altertness at 2 h intervals in Helsinki (Finland) two days before westward flight to Los Angeles (USA), A93-39709 where the measurements were repeated on the 2nd day after the HIGH-ALTITUDE PULMONARY EDEMA WITH PULMONARY flights and on the 2nd day in Finland after return flight. The age, THROMBOEMBOLISM day length, marital status, and physical exercise explained the S. NAKAGAWA, K. KUBO, T. KOIZUMI, T. KOBAYASHI, and M. acrophase adaptation of the melatonin rhythm after the westward SEKIGUCHI (Shinshu Univ., Matsumoto, Japan) Chest (ISSN flight, while the day length, neuroticism, and extroversion were 0012-3692) vol. 103, no. 3 March 1993 p. 948-950. the relevant factors after eastward flight. The marital status, Copyright neuroticism, and physical exercise explained the variation of the High-altitude pulmonary edema (HAPE) is a form of acrophase adjustment of the alertness rhythm after westward flight, noncardiogenic pulmonary edema. The pathophysiology of HAPE and the age and eveningness after eastward flight. It is concluded remains unclear. A case of HAPE was associated with pulmonary that the amount of daylight and personality are the best predictors thromboembolism of a left upper pulmonary artery. Pulmonary of the circadian rhythm adaptation after transmeridian flights. thromboembolism was an important factor in development of HAPE Author (revised) in this case. Author A93-39716 A93-39710 MICROGRAVITY AND ORTHOSTATIC INTOLERANCE - INTRAOCULAR PRESSURE AND RETINAL VASCULAR CAROTID HEMODYNAMICS AND PERIPHERAL RESPONSES CHANGES DURING TRANSIENT EXPOSURE TO P. J. LACOLLEY, B. M. PANNIER, J. L. CUCHE, J. S. HERMIDA, MICROGRAVITY S. LAURENT, P. MAISONBLANCHE, J. L. DUCHIER, B. I. LEVY, T. H. MADER, C. R. GIBSON, M. CAPUTO, N. HUNTER, G. and M. E. SAFAR (Hopital Broussais, Paris, France) American TAYLOR, J. CHARLES, and R. T. MEEHAN (U.S. Army, Madigan Journal of Physiology (ISSN 0002-9513) vol. 264, pt. 2 Feb. Army Medical Center, Tacoma, WA) American Journal of 1993 p. H588-H594. Ophthalmology (ISSN 0002-9394) vol. 115, no. 3 March 15, Copyright 1993 p. 347-350. A ground-based model (24 h of bed rest (BR) with head-down Copyright tilt (HOT)) was used to investigate the cardiovascular deconditioning We measured intraocular pressures and retinal vascular responsible for orthostatic intolerance, frequently observed after diameters from 11 subjects during 20 seconds of microgravity weightlessness flights. This experimental deconditioning is shown

278 52 AEROSPACE MEDICINE to be distinguished by an increase of mean blood pressure, with capillaries. Pressure waveforms were recorded in 40 separate increased total peripheral resistances (TPRs). Systolic tangential capillary vessels and 14 separate postcapillary venules over periods tension of the carotid arterial wall, cardiac output and frequency, ranging from 5 to 64 s. Localization and determination of capillary and plasma norepinephrine and epinephrine were not significantly and postcapillary vessels were ascertained anatomically before altered, while plasma dopamine was increased. Cardiovascular pressure measurements. Capillary pressure was 33.2 +/- 1.5 (SE) homeostasis was challenged before and after 24 h of BR with mm Hg in lips of subjects seated upright. Repeated micropunctures HOT, through -40 mmHg lower body negative pressure (LBNP). of the same vessel gave an average coefficient of variation of Systolic tangential tension of the carotid wall was decreased, with 0.072. Postcapillary venule pressure was 18.9 + /- 1.6 mm Hg. a decrease of systolic pressure and cardiac output; increased heart This procedure produces a direct and reproducible means of rate was likely due to an increase of sympathetic drive with a measuring microvascular blood pressures in a vascular bed above decrease of vagal braking. The overall picture was not changed heart level in humans. Author (revised) after 24 h of BR with HOT, except for a lack of increase of TPRs. Author (revised) A93-40774 NEW TECHNOLOGY FOR THE ANALYSIS OF THE RESULTS A93-39725 OF AN ULTRASOUND EXPERIMENT PERFORMED IN EFFECTS OF LONG-TERM WEIGHTLESSNESS ON ROLL AVIATION-MEDICINE MEDICAL EXAMINATION [NOVAYA CIRCULARVECTION TEKHNOLOGIYA ANALIZA REZUL'TATOV D. G. D. WATT (McGill Univ., Montreal, Canada), J. P. LANDOLT ULTRAZVUKOVOGO ISSLEDOVANIYA V TSELYAKH (Defence and Civil Inst. of Environmental Medicine, Toronto, VRACHEBNO-LETNOJ EKSPERTIZY] Canada), and L. R. YOUNG (MIT, Cambridge, MA) Canadian A. YU. VASIL'EV, A. P. IVANCHIKOV, and A. P. KOZLOVSKIJ Aeronautics and Space Journal (ISSN 0008-2821) vol. 39, no. 1 Aviakosmicheskaya i Ekologicheskaya Meditsina (ISSN March 1993 p. 52-55. CASI, Astronautics Conference, 7th, 0233-528X) vol. 26, no. 2 Mar.-Apr. 1992 p. 62-65. In Ottawa, Canada, Nov. 4-6, 1992 Research supported by Canadian RUSSIAN refs Space Agency, DND, and Medical Research Council of Canada Copyright refs The paper describes an equipment complex developed for the The 8-day Spacelab IML-1 mission employed simulations, digital processing of ultrasound images, developed for a measurements and their results' analysis to investigate the effects military-aviation-research hospital. The system consists of a of continuous roll circularvection. The results obtained suggest personal computer with peripheral equipment, specialized that roll circularvection temporarily increases during weightlessness, installations for the display and processing of video information, reflecting a process of compensation for the need to solve problems and a system for storing video data. The complex can be used in spatial orientation, rather than constituting the result of such a with ultrasound scanners ETS-01-R, Aloka-260, Aloka-630, and compensating process. AIAA Toshiba-77. Results of the processing ultrasound scans of 100 aviators, performed for diagnosing various health problems, are A93-40549* National Aeronautics and Space Administration. John discussed. AIAA F. Kennedy Space Center, Cocoa Beach, FL. MAPPING OF ELECTRICAL MUSCLE STIMULATION USING A93-41117 MRI INTERACTIONS BETWEEN HB, MG, DPG, ATP, AND CL GREGORY R. ADAMS, ROBERT T. HARRIS, DANIEL WOODARD, DETERMINE THE CHANGE IN HB-O2 AFFINITY AT HIGH and GARY A. DUDLEY (Bionetics Corp., Biomedical and ALTITUDE Environmental Labs.; NASA, Kennedy Space Center, Cocoa Beach, HEIMO MAIRBAEURL, OSWALD OELZ, and PETER BAERTSCH FL; Ohio Univ., Athens) Journal of Applied Physiology (ISSN (Yale Univ., New Haven, CT; Zuerich, Universitaetsspital, Zurich; 8750-7587) vol. 74, no. 2 Feb. 1993 p. 532-537. refs Eidgenoessische Sportschule, Magglingen, Switzerland) Journal (Contract NAS10-11624) of Applied Physiology (ISSN 8750-7587) vol. 74, no. 1 Jan. Copyright 1993 p. 40-48. Research supported by Eidgenoessische The pattern of muscle contractile activity elicited by Sportschule Magglingen refs electromyostimulation (EMS) was mapped and compared to the (Contract SNSF-3,200,0092,85; FFWF PROJECT P-6221) contractile-activity pattern produced by voluntary effort. This was Copyright done by examining the patterns and the extent of contrast shift, The intracellular distribution of the various species of Hb, DPG, as indicated by T2 values, im magnetic resonance (MR) images ATP, Cl, and Mg was determined to evaluate' the role that various after isometric activity of the left m. quadriceps of human subjects potential ligands of Hb play in altering standard P(O2) at 50 percent was elicited by EMS (1-sec train of 500-microsec sine wave pulses O2 saturation (P sub 50, st) and to clarify the mechanism of an at 50 Hz) or voluntary effort. The results suggest that, whereas 2,3 diphosphoglycerate (DPG) independent increase in P sub 50, EMS stimulates the same fibers repeatedly, thereby increasing st during early altitude acclimatization. Subjects were examined at the metabolic demand and T2 values, the voluntary efforts are low altitude and during the early phase of acclimatization to high performed by more diffuse asynchronous activation of skeletal altitude (3 days at 4,559 m) to determine ligand binding by Hb muscle even at forces up to 75 percent of maximal to maintain and Hb-O2 affinity. Results indicate that P sub 50, st increased at performance. AIAA high altitude (HA) by about 4.5 Torr and the concentration of DPG increased by 28 percent. The sum of concentrations of all A93-40550 National Aeronautics and Space Administration. Ames liganded Hb species increased, reaching 79 percent of its total Research Center, Moffett Field, CA. change within 22 h after ascent, which is mainly attributed to the DIRECT MEASUREMENT OF CAPILLARY BLOOD PRESSURE change in the concentration of Hb (DPG) (+77 percent of total IN THE HUMAN LIP increase). AIAA S. E. PARAZYNSKI, B. J. TUCKER, M. ARATOW, A. CRENSHAW, and A. R. HARGENS (NASA, Ames Research Center, Moffett Field, A93-41118 CA) Journal of Applied Physiology (ISSN 8750-7587) vol. 74, RESPONSE OF GENIOGLOSSUS EMG ACTIVITY TO PASSIVE no. 2 Feb. 1993 p. 946-950. Research supported by NASA TILT IN MEN and Stanford Medical Scholars Program refs MICHAEL J. WASICKO, SUSAN L KNUTH, and JAMES C. LEITER Copyright (Dartmouth College, Lebanon, NH) Journal of Applied Physiology In this study, we developed and tested a new procedure for (ISSN 8750-7587) vol. 74, no. 1 Jan. 1993 p. 73-81. Research measuring microcirculatory blood pressures above heart level in supported by Parker B. Francis Foundation refs humans. Capillary and postcapillary venule blood pressures were (Contract NIH-HL-07449; NIH-HL-01998) measured directly in 13 human subjects by use of the servonulling Copyright micropressure technique adapted for micropuncture of lip The effect of passive tilt on upper airway muscle activity in

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men was analyzed under the assumption that changes in degree Tibet Inst. of Medical Sciences, Lhasa, China; Sydney Univ., of tilt would change local pressure at the carotid baroreceptors. Australia) Journal of Applied Physiology (ISSN 8750-7587) vol. Data obtained revealed that the transient response of 74, no. 1 Jan. 1993 p. 312-318. refs electromyogram (EMG) activity of the genioglossus to tilt was (Contract DAMD17-87-C-7202; NIH-HL-14985; NIH-HD-00681; biphasic: when moving from upright to supine position, there was NSF BNS-89-19645) a rapid increase in activity during the tilt maneuver followed by a Copyright progressive decline. Thus passive tilt from upright to supine position Elevated pulmonary arterial pressure in high-altitude residents results in inhibition of EMG independent of changes in level of may be a maladaptive response to chronic hypoxia. If so, arousal. AIAA well-adapted populations would be expected to have pulmonary arterial pressures that are similar to sea-level values. Five normal A93-41119 National Aeronautics and Space Administration. male 22-yr-old lifelong residents of 3,600 m or higher elevations Lyndon B. Johnson Space Center, Houston, TX. who were of Tibetan descent were studied in Lhasa (3,658 m) at ORTHOSTATIC INTOLERANCE DURING A 13-DAY BED REST rest and during near-maximal upright ergometer exercise. We found DOES NOT RESULT FROM INCREASED LEG COMPLIANCE that resting mean pulmonary arterial pressure and pulmonary FRANCOIS M. MELCHIOR and SUZANNE M. FORTNEY (NASA, vascular resistance were within sea-level norms and were little Johnson Space Center, Houston, TX) Journal of Applied changed while subjects breathed a hypoxic gas mixture. Physiology (ISSN 8750-7587) vol. 74, no. 1 Jan. 1993 p. Near-maximal exercise increased cardiac output more than 286-292. Research supported by DRET refs threefold to values of 18.3 +/- 1.2 l/min but did not elevate (Contract RTOP 199-15-11-14; RTOP 199-14-11-13) pulmonary vascular resistance. Breathing 100 percent O2 during Copyright near-maximal exercise did not reduce pulmonary arterial pressure Increased leg compliance (LC) has been proposed as a or vascular resistance. We concluded that this small sample of mechanism for orthostatic intolerance after spaceflight or bed rest. healthy Tibetans with lifelong residence above 3,658 m had resting Using venous occlusion plethysmography with mercury-in-Silastic pulmonary arterial pressures that were normal by sea-level strain gauge, we evaluated LC before, during, and after a 13-day standards and exhibited minimal hypoxic pulmonary head-down bed rest in 10 men. LC was measured by the vasoconstriction, both at rest and during exercise. These findings relationship between the increased calf areas at thigh cuff are consistent with remarkable cardiac performance and occlusions of 20, 30, 50, 70, and 80 mmHg. Orthostatic tolerance high-altitude adaptation. Author (revised) was evaluated by a presyncopal-limited lower body negative pressure test before and after bed rest. The 10 subjects were A93-41122* National Aeronautics and Space Administration. divided into TOL (n= 5) and INT (n=5) groups for which the Lyndon B. Johnson Space Center, Houston, TX. orthostatic tolerance was similar and lower after bed rest, CEREBRAL BLOOD VELOCITY AND OTHER respectively. For TOL (INT) before bed rest, calf area increases CARDIOVASCULAR RESPONSES TO 2 DAYS OF were 2.2 +/- 0.5 (SE) (1.3 +/- 0.4), 3.5 + /- 0.7 (2.3 + /- 0.5), HEAD-DOWN TILT 5.0 +/- 0.9 (3.5 + /- 0.6), 5.6 + /- 0.9 (4.4 +/- 0.6), and 6.4 MARY A. B. FREY, THOMAS H. MADER, JAMES P. BAGIAN, + /- 1.1 (4.7 -f/- 0.6) sq cm for thigh occlusion pressures of 20, JOHN B. CHARLES, and RICHARD T. MEEHAN (U.S. Army, 30, 50, 70, and 80 mmHg, respectively. Neither for INT nor for Madigan Army Medical Center, Tacoma, WA; Universities Space TOL were these results significantly changed by bed rest. These Research Association; NASA, Johnson Space Center, Houston; results suggest that other mechanisms than increased LC have to Texas Univ., Galveston) Journal of Applied Physiology (ISSN be taken into account to explain the decreased orthostatic tolerance 8750-7587) vol. 74, no. 1 Jan. 1993 p. 319-325. refs induced by this 13-day bed rest. Author (revised) (Contract NIH-MO1-RR-00073) Copyright A93-41120 Spaceflight induces a cephalad redistribution of fluid volume HYPOXIC VENTILATORY RESPONSIVENESS IN TIBETAN and blood flow within the human body, and space motion sickness, COMPARED WITH HAN RESIDENTS OF 3,658 M which is a problem during the first few days of space flight, could JIANGUO ZHUANG, TARSHI DROMA, SHINFU SUN, CRAIG be related to these changes in fluid status and in blood flow of JANES, ROBERT E. MCCULLOUGH, ROSANN G. MCCULLOUGH, the cerebrum and vestibular system. To evaluate possible changes ALLEN CYMERMAN, SHAO YUNG HUANG, JOHN T. REEVES, in cerebral blood flow during simulated weightlessness, we and LORNA G. MOORE (Tibet Inst. of Medical Sciences, Lhasa; measured blood velocity in the middle cerebral artery (MCA) along Shanghai Inst. of Physiology, China; Colorado Univ., Denver; U.S. with retinal vascular diameters, intraocular pressure, impedance Army, Research Inst. of Environmental Medicine, Natick, MA) cardiography, and sphygmomanometry on nine men (26.2 +/- Journal of Applied Physiology (ISSN 8750-7587) vol. 74, no. 1 6.6 yr) morning and evening for 2 days during continuous 10 deg Jan. 1993 p. 303-311. refs head-down tilt (HOT). When subjects went from seated to (Contract DAMD17-87-C-7202; NIH-HD-00681; NIH-HL-14985; head-down bed rest, their heart rate and retinal diameters NSF BNS-89-19645) decreased, and intraocular pressures increased. After 48 h of HDT, Copyright blood flow velocity in the MCA was decreased and thoracic A study is conducted of the ventilatory characteristics of impedance was increased, indicating less fluid in the thorax. Percent Himalayan high-altitude residents, in view of their reportedly lower changes in blood flow velocities in the MCA after 48 h of HDT hemoglobin levels; 27 lifelong Tibetan residents of Lhasa were were inversely correlated with percent changes in retinal vascular compared with 30 acclimatized Chinese newcomers that were diameters. Blood flow velocities in the MCA were inversely matched for physical characteristics and exercise training, in order correlated (intersubject) with arterial pressures and retinal vascular to determine whether Tibetans exhibited levels of ventilation and diameters. Heart rate, stroke volume, cardiac output, systolic arterial hypoxic ventilatory drives as great as the acclimatized newcomers. pressure, and at times pulse pressure and blood flow velocities in The Tibetans had higher hypoxic ventilatory response shape the MCA were greater in the evening. Total peripheral resistance parameter A values and hypercapnic ventilatory responsiveness was higher in the morning. Although cerebral blood velocity is than the Han subjects. AIAA reduced after subjects are head down for 2 days, the inverse relationship with retinal vessel diameters, which have control A93-41121 analogous to that of cerebral vessels, indicates cerebral blood MINIMAL HYPOXIC PULMONARY HYPERTENSION IN flow is not reduced. Author (revised) NORMAL TIBETANS AT 3,658 M BERTRON M. GROVES, TARSHI DROMA, JOHN R. SUTTON, A93-41123 ROSANN G. MCCULLOUGH, ROBERT E. MCCULLOUGH, INFLUENCE OF IN VIVO HYPOBARIC HYPOXIA ON JIANGUO ZHUANG, GARRISON RAPMUND, SHINFU SUN, FUNCTION OF LYMPHOCYTES, NEUTROCYTES, NATURAL CRAIG JANES, and LORNA G. MOORE (Colorado Univ., Denver; KILLER CELLS, AND CYTOKINES

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M. KLOKKER, A. KHARAZMI, H. GALBO, I. BYGBJERG, and B. A93-41168 K. PEDERSEN (Danish Armed Forces Health Services, Panum EFFECTS OF DYNAMIC EXERCISE ON CARDIOVASCULAR Inst; Rigshospitalet; Copenhagen Univ., Denmark) Journal of REGULATION DURING LOWER BODY NEGATIVE PRESSURE Applied Physiology (ISSN 8750-7587) vol. 74, no. 3 March TAKESHI NISHIYASU, XIANGRONG SHI, CHRISTOPHER M. 1993 p. 1100-1106. Research supported by Danish Armed GILLEN, GARY W. MACK, and ETHAN R. NADEL (Yale Univ., Forces Health Services, Royal Danish Air Force, and Simon Spies New Haven, CT) Aviation, Space, and Environmental Medicine Foundation refs (ISSN 0095-6562) vol. 64, no. 6 June 1993 p. 517-521. Copyright refs The effects of short-term hypoxia in vivo on the human cellular (Contract NIH-HL-20634; NIH-HL-39818) immune system are investigated. The experiments were carried Copyright out in a decompression chamber simulating cabin pressure in The cardiovascular responses to blood pooling at rest with nondecompressed flight at an altitude of 18,000 ft with and without those during moderate dynamic exercise are compared to test supplemental O2. The leukocyte concentration increased during the hypothesis that the defense of arterial blood pressure against hypobaric conditions because of an increased concentration of a marked decrease in venous return would be preserved during lymphocytes. The absolute and relative concentration of CD16+ moderate dynamic exercise. In ten physically active men, blood natural killer (NK) cells increased markedly during hypoxia and pooling was varied by applying different levels of lower body returned to pretest values after 2 h of recovery. The NK cell negative pressure at rest and during various intensities of supine activity of blood mononuclear cells boosted with interferon-alpha, dynamic exercise. Results show that the change in total peripheral interleukin-2 (IL-2), and indomethacin rose in parallel with resistance with respect to stroke volume was linear confirming unboosted NK cell activity during hypoxia. It is concluded that that peripheral vascular adjustments were proportional to changes acute hypoxia induced marked alterations in the immune system in the heart's preload. It is concluded that the control characteristics and that the NK cells are especially sensitive to the hypoxic of arterial blood pressure regulation are similar during rest and stimulus. AIAA moderate dynamic exercise. AIAA

A93-41125 A93-41169 National Aeronautics and Space Administration. Ames BODY FLUID COMPARTMENTS, RENAL BLOOD FLOW, AND Research Center, Moffett Field, CA. HORMONES AT 6,000 M IN NORMAL SUBJECTS PERFORMANCE AND MOOD-STATE PARAMETERS DURING INDER S. ANAND, Y. CHANDRASHEKHAR, SUDHAKAR K. RAO, 30-DAY 6 DEC HEAD-DOWN BED REST WITH EXERCISE RAVI M. MALHOTRA, ROBERTO FERRARI, JAGDISH TRAINING CHANDANA, B. RAMESH, K. J. SHETTY, and M. S. BOPARAI CHARLES W. DEROSHIA and J. E. GREENLEAF (NASA, Ames (Postgraduate Inst. of Medical Education and Research, Research Center, Moffett Field, CA) Aviation, Space, and Chandigarh; High Altitude Medical Research Centre, Leh, India; Environmental Medicine (ISSN 0095-6562) vol. 64, no. 6 June Brescia Univ., Italy) Journal of Applied Physiology (ISSN 1993 p. 522-527. Research supported by U.S. Army refs 8750-7587) vol. 74, no. 3 March 1993 p. 1234-1239. refs (Contract RTOP 199-21-12; RTOP 199-22-12; RTOP 199-22-22; Copyright RTOP 199-22-32; RTOP 199-22-44; NAG2-410) Results are presented of an experimental study of body fluid Copyright compartments, renal bipod flow, and a variety of plasma hormones A study aimed at determining if the performance and mood in normal subjects residing at an altitude of 6000 m for more impairments occur in bed-rested subjects, and if different than 10 wk. There was a marked expansion of all the fluid spaces: exercise-training regimens modify or prevent them is presented. total body sodium was 14 percent above normal, total body water Eighteen healthy men were divided into three groups performing was 18 percent above normal, plasma volume was 33 percent no exercise, isotonic exercise, and isokinetic exercise. Few above normal, and blood volume was 84.5 percent above normal. deleterious changes occurred in performance and mood of the The effective renal plasma flow was 55 percent lower than normal, three groups which did not exceed baseline ambulatory levels. It but the reduction in the effective renal blood flow was 37 percent is concluded that mood and performance did not deteriorate in below normal because the hematocrit was high. It is suggested response to prolonged bedrest and were not altered by exercise that a prolonged stay at extreme altitude can cause salt and training. AIAA water retention to an extent approximately similar to that in untreated congestive heart failure. It is likely that the stress of hypobaric hypoxia, cold, and exertion at high altitude increases catecholamines, which reduce renal blood flow and lead to a A93-41170 congestive state in normal subjects at extreme altitude. AIAA FLOW CYTOMETRIC ANALYSIS OF LYMPHOCYTE SURFACE MARKERS FOLLOWING A 1-GY DOSE OF GAMMA RADIATION DENNIS A. ROWLEY, WILLIAM A. KELLEY, and JULIAN H. A93-41165 MANDERS (Naval Hospital, Portsmouth, VA) Aviation, Space, EFFECTS OF SLEEP DEPRIVATION AND EXERCISE ON and Environmental Medicine (ISSN 0095-6562) vol. 64, no. 6 GLUCOSE TOLERANCE June 1993 p. 528-533. Research supported by U.S. Navy T. VANHELDER, J. D. SYMONS, and M. W. RADOMSKI (Defence refs and Civil Inst. of Environmental Medicine; Toronto Univ., Canada) Copyright Aviation, Space, and Environmental Medicine (ISSN 0095-6562) Lymphocytes labeled with monoclonal antibodies were analyzed vol. 64, no. 6 June 1993 p. 487-492. Research supported by using a llow cytometer to compare the mean fluorescent intensity NSERC refs of several surface membrane antigens (markers) from irradiated Copyright and nonirradiated blood samples. Whole blood subjected to a 1-Gy The impact of sleep deprivation (SD) on the capability of (100-rad) dose of 1.25 MeV gamma radiation from a Co-60 subjects to handle an oral glucose load was studied. The effects radioisotope source was compared with nonirradiated blood drawn of daily prolonged physical activity during SD were examined to simultaneously from the same healthy subject. Results show that verify the concept that the physical activity modulates glucose the fluorescent intensity is proportional to the number of intact uptake and insuline secretion. It is concluded that sleep loss of binding sites on the lymphosyte surface and the observed 60 h combined with physical inactivity increased the insulin decrement directly infers that damage occurred to some sites. It response to a glucose challenge provided there were no changes is concluded that there is a measurable effect on the lymphocyte in glucose uptake. Physical activity reversed partially some of these membrane at a radiation dose at which many of the lymphocytes effects. AIAA will survive. AIAA

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A93-41171 N93-27102*# Brown Univ., Providence, Rl. Dept. of Pathology CASE REPORT - CHRONIC SUB-DURAL HEMATOMA and Lab. Medicine. FOLLOWING HIGH-SPEED EJECTION MECHANICAL STIMULATION OF SKELETAL MUSCLE RICHARD WARBURTON (Royal Saudi Air Force Aeromedical INCREASES PROSTAGLANDIN F2(ALPHA) SYNTHESIS AND Centre, King Abdulaziz Air Base, Saudi Arabia) Aviation, Space, CYCLOOXYGENASE ACTIVITY BY A PERTUSSIS TOXIN and Environmental Medicine (ISSN 0095-6562) vol. 64, no. 6 SENSITIVE MECHANISM June 1993 p. 534-537. HERMAN H. VANDENBURGH, JANET SHANSKY, ROSA Copyright SOLERSSI, and JOSEPH CHROMIAK 1992 48 p A case of chronic subdural hematoma occurring in a pilot after (Contract NAG2-414) a high speed ejection based on the survival envelope of the Mark (NASA-CR-193041; NAS 1.26:193041) Avail: CASI HC A03/MF 10 Martin Baker ejection seat is reported. The surgical treatment, A01 recovery, and final assessment are discussed along with the Repetitive mechanical stimulation of differentiated skeletal possible causes of the subdural hematoma. It is pointed out that muscle in tissue culture increases the production of prostaglandin flight surgeon should analyze carefully the events in the case. F(sub 2(alpha)), an anabolic stimulator of myofiber growth. Within Subdural hematoma is considered to be difficult to diagnose but it 4 h of initiating mechanical activity, the activity of cyclooxygenase, can cause late complications from an ejection. AIAA a regulatory enzyme in prostaglandin synthesis, was increased 82% (P is less than .005), and this increase was maintained for at least 24 h. Kinetic analysis of the stretch-activated cyclooxygenase indicated a two to three-fold decrease in the A93-41468* National Aeronautics and Space Administration. enzyme's K(sub m) with no change in V(sub max). The Ames Research Center, Moffett Field, CA. stretch-induced increase in enzymatic activity was not inhibited by METABOLIC RESPONSES TO SIMULATED EXTRAVEHICULAR cycloheximide, was independent of cellular electrical activity ACTIVITY (tetrodotoxin-insensitive), but was prevented by the G protein REBECCA C. WILLIAMSON, PETER J. SHARER (Sterling Federal inhibitor pertussis toxin. Pertussis toxin also inhibited the Systems, Inc., Palo Alto, CA), BRUCE W. WESSON (NASA, Ames stretch-induced increases in PGF(sub 2(alpha)) production, and Research Center, Moffett Field, CA), and LISA R. RENDON (Foothill cell growth. It is concluded that stretch of skeletal muscle increases College, Los Altos Hill, CA) Jul. 1992 10 p. SAE, International the synthesis of the anabolic modulator PGF(sub 2(alpha)) by a G Conference on Environmental Systems, 22nd, Seattle, WA, July protein-dependent process which involves activation of 13-16, 1992 refs cyclooxygenase by a posttranslational mechanism. (SAE PAPER 921303) Copyright Author (revised) Automatic control of the liquid cooling garment (LCG) worn by astronauts during extravehicular activity (EVA) would more efficiently regulate astronaut thermal comfort and improve astronaut productivity. An experiment was conducted in which subjects performed exercise profiles on a unique, supine upper body N93-27113*# Brown Univ., Providence, Rl. Dept. of Pathology. ergometer to elicit physiological and thermal responses similar to GROWTH FACTOR INVOLVEMENT IN TENSION-INDUCED those achieved during zero-g EVAs. Results were analyzed to SKELETAL MUSCLE GROWTH Semiannual Report, 1 Nov. quantify metabolic rate, various body temperatures, and other heat 1992 - 30 Apr. 1993 balance parameters. Such data may lead to development of a HERMAN H. VANDENBURGH 30 Apr. 1993 8 p microprocessor-based system to automatically maintain astronaut (Contract NAG2-414) heat balance during extended EVAs. Author (NASA-CR-193023; NAS 1.26:193023) Avail: CASI HC A02/MF A01 Long-term manned space travel will require a better understanding of skeletal muscle atrophy which results from A93-41546* National Aeronautics and Space Administration, microgravity. Astronaut strength and dexterity must be maintained Washington, DC. for normal mission operations and for emergency situations. POTENTIAL HEALTH HAZARDS FROM THERMAL Although exercise in space slows the rate of muscle loss, it does DEGRADATION EVENTS - PARTICULATE VS. GAS PHASE not prevent it. A biochemical understanding of how EFFECTS gravity/tension/exercise help to maintain muscle size by altering GUNTER OBERDORSTER, JURAJ FERIN, JACOB FINKELSTEIN, protein synthesis and/or degradation rate should ultimately allow RAYMOND BAGGS (Rochester Univ., NY), D. M. STAVERT, and pharmacological intervention to prevent muscle atrophy in BRUCE E. LEHNERT (Los Alamos National Lab., NM) Jul. 1992 microgravity. The overall objective is to examine some of the basic 17 p. SAE, International Conference on Environmental Systems, biochemical processes involved in tension-induced muscle growth. 22nd, Seattle, WA, July 13-16, 1992 refs With an experimental in vitro system, the role of exogenous and (Contract NAGW-2356) endogenous muscle growth factors in mechanically stimulated (SAE PAPER 921388) Copyright muscle growth are examined. Differentiated avian skeletal The effect of instillation of ultrafine TiO2 particles (10-nm myofibers can be 'exercised' in tissue culture using a newly anatase-TiO2 and 12-nm rutile-TiO2 (administered in doses from developed dynamic mechanical cell stimulator device which 60 to 1000 microg/rat and 500 microg/rat, respectively) on the simulates different muscle activity patterns. Patterns of mechanical respiratory tract of exposed rats was compared to the effects of activity which significantly affect muscle growth and metabolic larger (250 nm anatase-TiO2 and 220-nm rutile-TiO2 particles characteristics were found. Both exogenous and endogenous (given in doses 500 or 1000 microg/rat and 500 microg/rat, growth factors are essential for tension-induced muscle growth. respectively). These effects were also compared to the effects of Exogenous growth factors found in serum, such as insulin, inhalation of 20-nm and 250-nm anatase-TiO2 particles and insulin-like growth factors, and steroids, are important regulators inhalation with surrogate gas phase components (HF and HCI). It of muscle protein turnover rates and mechanically-induced muscle was found that ultrafine TiO2 particles induced greater inflammatory growth. Endogenous growth factors are synthesized and released reaction in the lung, had greater adverse effect on alveolar into the culture medium when muscle cells are mechanically macrophage-mediated clearance function, and had a greater stimulated. At least one family of mechanically induced endogenous potential to induce mediators which can adversely affect other factors, the prostaglandins, help to regulate the rates of protein lung cells than did larger-sized particles. Inhalation of surrogate turnover in muscle cells. Endogenously synthesized IGF-1 is gas phase components caused injury only to the upper respiratory another. The interaction of muscle mechanical activity and these tract, in contrast to the ultrafine particles, which affected the deep growth factors in the regulation of muscle protein turnover rates lung. AIAA with our in vitro model system is studied. Author

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N93-27158# Civil Aeromedical Inst., Oklahoma City, OK. Office involvement of opiate and GABAergic systems, in different brain of Aviation Medicine. regions, in regulating the storage of memory for different types of VARIATIONS IN TIME-TO-INCAPACITATION AND BLOOD tasks. The proposed experiments were based on previous findings CYNANIDE VALUES FOR RATS EXPOSED TO TWO providing extensive evidence that memory storage is influenced HYDROGEN CYANIDE GAS CONCENTRATIONS Final Report by treatments affecting neuromodulatory systems in the amygdala ARVIND K. CHATURVEDI, BOYD R. ENDECOTT, ROXANE M. as well as preliminary evidence suggesting the possibility that such RITTER, and DONALD C. SANDERS May 1993 20 p influences might be limited to restricted domains (or forms) of (DOT/FAA/AM-93-8) Avail: CASI HC A03/MF A01 learning and memory. The view that GABAergic and opiate drugs It has been suggested that protective breathing devices protect act by influencing memory storage is supported by previous, as aircraft passengers from combustion products for 5 min during well as recent evidence that the drugs do not induce evacuation and for 35 min during in-flight-plus-evacuation. Hydrogen state-dependency. That is, the effects on retention performance cyanide (HCN), a combustion gas, produces incapacitation at do not depend upon a congruence between drug states at the relatively low concentrations, and time-to-incapacitation (t(sub i) is time of training (or shortly after training) and retention testing. an applicable index for predicting escape from a fire. Variations in The research supported by this grant has provided additional t(sub i) and blood cyanide (CN-) at specific HCN gas exposure evidence that memory storage is influenced by opiate and concentrations have not been evaluated. Therefore, t(sub i) and GABAergic influences. Within the range of tasks examined, the blood CN- at t(sub i) for two HCN concentrations that produce 5- effects did not depend upon the forms of learning and memory and 35-min t(sub i) were determined in male Sprague-Dawley rats. examined. Both the amygdala and septum appear to be involved Blood CN- levels as a function of HCN exposure time were in regulating GABAergic influences on memory and the effects measured. Animals were individually exposed to HCN gas in a appear to be mediated through cholinergic influences. DTIC chamber equipped with a rotating cage, and t(sub i) was recorded as the time from insertion of the animal into the cage until it N93-27923# Army Aeromedical Research Lab., Fort Rucker, could no longer walk. At incapacitation and at selected intervals AL. prior to t(sub i), rats were quickly removed from the cage and THE USE OF ELECTROPHYSIOLOGICAL AND COGNITIVE killed for blood collection and CN- quantitation. Chamber HCN VARIABLES IN THE ASSESSMENT OF DEGRADATION concentrations were monitored during the exposures. For the 5-min DURING PERIODS OF SUSTAINED WAKEFULNESS Final test (mean plus or minus SD; n = 50), HCN gas = 184 plus or Report minus 10.0 ppm, t(sub i) = 5.1 plus or minus 0.8 min, and blood CARLOS A. COMPERATORE, JOHN A. CALDWELL, JR., ROBERT CN- = 2.3 plus or minus 0.5 micro-g/mL; for the 35-min test, L. STEPHENS, JIM A. CHIARAMONTE, and JACQUELYN Y. HCN gas = 64 plus or minus 6.1 ppm, t(sub i) = 31.1 plus or PEARSON Dec. 1992 64 p minus 11.2 min, and blood CN- = 4.2 plus or minus 1.3 micro-g/mL. (Contract DA PROJ. 3M1-62787-A-897) Blood CN- levels increased as a function of HCN exposure time, (AD-A263033; USAARL-93-5) Avail: CASI HC A04/MF A01 but the blood CN- level at the 5-min t(sub i) was half of the Army aviation personnel often encounter work schedules which 35-min blood CN- level; the HCN gas uptake rate at 184 ppm require the transition from daytime to nighttime duty hours without was about 3 times that at 64 ppm. These findings suggest that the benefit of an adaptation period. Rotations from daytime and the blood CN- level at incapacitation may vary substantially, nighttime duty hours, particularly those that occur within a 24-hour depending upon the HCN exposure concentration; an equation is period, usually result in loss of sleep, fatigue, and cognitive proposed for predicting blood CN- levels in rats. Author (revised) degradation. Strategies in the scheduling of sleep, meals, work, and exercise are currently under study with the purpose of N93-27409# Veterans Administration Hospital, San Francisco, identifying patterns that assist in the physiological adaptation to CA. nighttime duty hours. These coping strategies are composed of SECONDARY INJURY FACTORS AND PREVENTATIVE countermeasures designed to prevent the sleep loss and chronic TREATMENT Final Report, 15 Jul. 1987 - 14 Jul. 1991 fatigue usually associated with rapid transitions from daytime to A. I. FADEN May 1992 170 p nighttime duty hours. The study of shiftwork coping strategies (Contract DHHS-R59-CCR-902269) requires the empirical characterization of effective countermeasures (PB93-176014) Avail: CASI HC A08/MF A02 which prevent chronic fatigue and preserve normal cognitive The project included three independent, parallel studies: two function. In the laboratory, the study of variables such as alertness, involving experimental animals (head injury, spinal cord injury) and sensory processing, reaction time, and cognitive processing one involving humans (head injury). The underlying hypotheses assessment approach requires the use of multidisciplinary test for this work were that: (1) secondary, delayed injury resulting batteries that not only challenge cognitive processes, but also from actions of endogenous, autodestructive factors represents a document the functional status of brain regions associated with significant contributing factor to the neurological disability that sensory processing and alertness. The aim of this study was to follows brain or spinal cord trauma; (2) that endogenous opioids evaluate the usefulness of a test battery designed to characterize (particularly dynorphin) and excitatory amino acids represent major the state of alertness and cognitive ability of subjects involved in classes of autodestructive factors; (3) that opioid receptor postponing sleep for approximately 60 consecutive hours. DTIC antagonists, or N-methyl-D-aspartate (NMDA) receptor antagonists administered within the first hours of trauma, improve neurological N93-28122# Los Alamos National Lab., NM. Life Sciences Div. outcome; (4) that kappa-selective opioid antagonists are more EVALUATION OF NOW-INDUCED TOXICITY Final Report, 1 effective than non-selective antagonists in treating central nervous Jul. 1985 - 30 Sep. 1992 system trauma; and (5) that magnetic resonance spectroscopy BRUCE E. LEHNERT 31 Dec. 1992 229 p (MRS) may enhance prognostic abilities in CNS trauma by (Contract DA PROJ. 3M1-61102-BS-15) monitoring metabolic changes and the response to treatment. (AD-A261034) Avail: CASI HC A11/MF A03 NTIS Investigations conducted from FY85-FY93 in the project entitled evaluation of NO(x)-induced toxicity are summarized. During the N93-27654# California Univ., Irvine. Center for Neurobiology of course of the studies, investigations were undertaken to address Learning and Memory. numerous objectives. Specific information provided is formatted in ANALYSIS OF NEURAL SYSTEMS INVOLVED IN the context of the objective(s) it concerns, a brief summary of MODULATION OF MEMORY STORAGE Final Report, 1 Jan. accomplishments and findings that are detailed in the section, 1990 - 31 Dec. 1992 and citations of reports and publications that have emanated in JAMES L MCGAUGH 1 Feb. 1993 6 p total or in part from research performed during the accomplishment (Contract N00014-90-J-1626) objective(s). Each section begins with its own Introduction, which (AD-A262418) Avail: CASI HC A02/MF A01 is then followed by a Materials and Methods section, a Results The aims of this research project were to investigate the section and a Summary or Discussion. Author (revised)

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N93-28293# Ohio State Univ., Columbus. Coll. of Pharmacy. of roles. A second goal of this model is to support the flow of 13 C NMR SPECTRA OF ALLOSTERIC EFFECTORS OF documents. The description of the role model and its HEMOGLOBIN implementation (the role system) constitutes the second focal point STANISLAW OSTROWSKI, THOMAS G. BURKE, and WALDEMAR of this thesis. ESA PRIEBE 1993 6 p Prepared in cooperation with Texas Univ., Houston N93-28739*# Aerospace Medical Research Labs., (Contract NOO014-90-J-1648) Wright-Patterson AFB, OH. Visual Display Systems Branch. (AD-A262979) Avail: CASI HC A02/MF A01 ARMSTRONG LABORATORY SPACE VISUAL FUNCTION In the last three years, many papers dealing with the preparation TESTER PROGRAM and biological activity of compounds that act as allosteric effectors MELVIN R. ONEAL, H. LEE TASK, and GERALD A. GLEASON of hemoglobin have been published. Among the numerous moieties, In NASA, Washington, NASA/DOD Flight Experiments Technical some urea derivatives were found to be very effective in reducing Interchange Meeting Proceedings 6 p 1992 oxygen affinity of hemoglobin. The structures of most of the Avail: CASI HC A02/MF A10 compounds were confirmed by H-1 NMR spectra; however, to our Viewgraphs on space visual function tester program are knowledge, C-13 NMR spectra have not been published for any presented. Many astronauts and cosmonauts have commented of these allosteric modifiers of hemoglobin. We prepared in this on apparent changes in their vision while on-orbit. Comments have series over 30 new urea and thiourea derivatives with the intent included descriptions of earth features and objects that would of investigating their biological activity. An analysis of C-13 NMR suggest enhanced distance visual acuity. In contrast, some spectra revealed high regularity in the chemical shifts of the similar cosmonaut observations suggest a slight loss in their object fragments of the structures and revealed signal deviations among discrimination during initial space flight. Astronauts have also structures having different substituents in the aromatic rings. mentioned a decreased near vision capability that did not recover DTIC to normal until return to earth. Duntley space vision experiment, USSR space vision experiments, and visual function testers are N93-28306# Federal Aviation Administration, Washington, DC. described. Derived from text Office of Aviation Medicine. INDEX OF INTERNATIONAL PUBLICATIONS IN AEROSPACE N93-28740*# Aerospace Medical Research Labs., MEDICINE Final Report Wright-Patterson AFB, OH. Visual Display Systems Branch. MELCHOR J. ANTUNANO Feb. 1993 26 p EFFECT OF MICROGRAVITY ON SEVERAL VISUAL (AD-A262908; DOT/FAA/AM-93/3) Avail: CASI HC A03/MF FUNCTIONS DURING STS SHUTTLE MISSIONS: VISUAL A01 FUNCTION TESTER-MODEL 1 (VFT-1) The Index of International Publications in Aerospace Medicine MELVIN R. ONEAL, H. LEE TASK, and LOUIS V. GENCO In is a comprehensive listing of international publications in clinical NASA, Washington, NASA/DOD Flight Experiments Technical aerospace medicine, operational aerospace medicine, aerospace Interchange Meeting Proceedings 14 p 1992 physiology, environmental medicine/physiology, diving medi- Avail: CASI HC A03/MF A10 cine/physiology, aerospace human factors, as well as other Viewgraphs on the effect of microgravity on several visual important topics directly- or indirectly-related to aerospace functions during STS shuttle missions are presented. The purpose, medicine. The Index is divided into six major sections: (1) Open methods, results, and discussion are discussed. The visual function Publications in General Aerospace Medicine; (2) Government tester model 1 is used. CASI Publications in General Aerospace Medicine; (3) Publications in other Topics related to Aerospace Medicine; (4) Proceedings from N93-28741*# Aerospace Medical Research Labs., Scientific Meetings, Conferences, and Symposiums in Aerospace Wright-Patterson AFB, OH. Visual Display Systems Branch. Medicine; (5) Journals, Newsletters, and Bulletins in Aerospace EFFECT OF MICROGRAVITY ON VISUAL CONTRAST Medicine; and (6) Online Computerized Databases containing THRESHOLD DURING STS SHUTTLE MISSIONS: VISUAL Bibliographic Information in Aerospace Medicine and Related FUNCTION TESTER-MODEL 2 (VFT-2) Disciplines. DTIC MELVIN R. ONEAL, H. LEE TASK, and LOUIS V. GENCO In NASA, Washington, NASA/DOD Flight Experiments Technical N93-28469# Technische Univ., Berlin (Germany). Fachbereich Interchange Meeting Proceedings 6 p 1992 Informatik. Avail: CASI HC A02/MF A10 DOKMA: A DOCUMENT ORIENTED COMMUNICATION MODEL Viewgraphs on effect of microgravity on visual contrast threshold FOR MEDICAL APPLICATIONS AS A BASIS OF A ROLE during STS shuttle missions are presented. The purpose, methods, SYSTEM IN THE MEDICAL FIELD Ph.D. Thesis [DOKMA: EIN and results are discussed. The visual function tester model 2 is DOKUMENTENORIENTIERTESKOMMUNIKATIONSMODELL used. CASI FUER MEDIZINISCHE ANWENDUNGEN ALS BASIS FUER EIN ROLLENSYSTEM IM MEDIZINISCHEN UMFELD] CHRISTIAN GAYDA 1992 248 p In GERMAN N93-28742*# Aerospace Medical Research Labs., (ETN-93-93799) Avail: CASI HC A11/MF A03 Wright-Patterson AFB, OH. Visual Display Systems Branch. Starting with an abstract communication model that examines EFFECT OF MICROGRAVITY ON THE VISUAL NEAR POINT: communication aspects in general, the document oriented VISUAL FUNCTION TESTER-MODEL 4 (VFT-4) communication model for medical applications is developed. It relies GERALD A. GLEASON, H. LEE TASK, and MELVIN R. ONEAL on a transfer model. The requirements towards this transfer model In NASA, Washington, NASA/DOD Flight Experiments Technical are defined by means of the document oriented communication Interchange Meeting Proceedings 8 p 1992 model for medical applications. The communication model itself Avail: CASI HC A02/MF A10 has to fulfill three requirements. A specification phase has to be Viewgraphs on effect of microgravity on the visual near point supported by this model. Furthermore, it should constitute a kind are presented. Background, problem, objectives, approach, of reference model for discussion purposes and it must support a benefits, and status are discussed. The visual function tester model verification phase. In order to reach these goals within the 4 is used. CASI communication model for medical applications, the related problems concerning document oriented communication are N93-28758# Chemical Warfare/Chemical and Biological Defense assigned to layers that are put in relation to each other. The Information Analysis Center, Edgewood, MD. integration and communication of patient data by means of EVALUATION AND OPTIMIZATION OF A FLEXIBLE computers imply special requirements on data security. Therefore, FILTRATION SYSTEM FOR RESPIRATORY PROTECTION the document oriented communication model for medical SYSTEM 21 Final Report applications takes these aspects into consideration within a security K. C. HOFACRE, R. L. MARKHAM, and V. M. NORTHRUP Feb.

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1993 43 p 1992 30 p (Contract DLA900-86-C-2045) (AD-A262762; DCIEM-92-60) Avail: CASI HC A03/MF A01 (AD-A262467; CBIAC-SS-373) Avail: CASI HC A03/MF A01 In a recent study, we have shown that the commercially Current filter elements for the M40 series of respirators are available Cold BusterfTM) Sports bar, purported to improve cold housed in rigid, metal canisters that contain media for aerosol resistance, did not do so in our subjects exposed to a relatively filtration, and adsorption of gases or vapors. The filtration media severe cold test. One possible explanation for our conflicting results is often pleated for increased surface area. Certain harmful gases is that our metabolic rate (M) was too high for the possibly small are removed by adsorption to activated carbon that has been thermogenic effect of the bar to be measurable. The goal of this treated with hexavalent chromium or zinc metal cations in a process study was therefore to re-evaluate, under milder conditions, the known as whetlerization. Whetlerization provides active sites to influence of the Cold Buster(TM) on heat balance (heat debt = chemisorb certain poison gases. The carbon is generally present heat production - heat losses) and body temperatures. Eight as a coarse granular bed, but can also be present in a powder semi-nude fasted subjects were exposed to the cold (3h at rest, form incorporated in a fabric, as in the M13A2 filter element. 10 C, less than 0.4 m/s wind) on two occasions following the DTIC ingestion of either a placebo (100 ml water) or a Cold Buster(TM) (all feedings at min 0 and 90). As a result of the cold, M, dry heat losses and heat debt (S) increased whereas mean skin N93-28759# California Univ., San Diego, La Jolla. Dept. of Chemistry. temperature decreased (P less than 0.05). Rectal temperature WOUND HEALING AND CONNECTIVE TISSUE METABOLISM: remained unchanged due to the mild cold. In all of the above parameters, there were no differences between treatments. THE ROLE OF HYPERBARIC OXYGEN THERAPY Final Report, 1 Jul. 1991 - 30 Jun. 1992 Ingestion of the Colt Buster(TM) significantly increased ELVIN HARPER Jun. 1992 6 p carbohydrate oxidation compared to the placebo. However, this was without impact on M, since it occurred entirely at the expense (Contract AF-AFOSR-0413-91) of fat oxidation. Interestingly, the Cold Buster(TM) increased plasma (AD-A262483; AFOSR-93-0202TR) Avail: CASI HC A02/MF A01 glucose and insulin levels 2h into the cold. This secretion of insulin The effect of hyperbaric oxygen on wound healing by the seems to have blunted lipid mobilization since it significatly reduced following growth promoting factors is discussed: Epidermal growth factor (EGF), platelet derived growth factor (PDGF), and plasma free fatty acids levels. The result confirm previous data transforming growth factor B (TGFB). These compounds are of where the ingestion of the Cold Buster(TM) Sports bar did not alter heat production, heat losses, heat debt or even body particular interest since they have been reported to increase collagenase secretion. EGF when applied directly to skin increased temperatures, and extended these observations to a mild cold the rate of healing by 100%. DTIC stress. DTIC

N93-28835# Department of Energy, Washington, DC. Medical N93-29041*# Mount Sinai School of Medicine, New York, NY. Applications and Biophysical Research Div. Dept. of Neurology. PROCEEDINGS OF A WORKSHOP ON MOLECULAR NASA SUPPORTING STUDIES FOR MICROGRAVITY NUCLEAR MEDICINE RESEARCH ON EYE MOVEMENTS Final Technical Report, 1 R. C. REBA, ed. 1992 161 p Workshop held in Washington, Jan. - 31 Dec. 1990 DC, 22-23 Jan. 1992 BERNARD COHEN 31 Dec. 1990 6 p (DE93-010828; CONF-920113-7) Avail: CASI HC A08/MF A02 (Contract NAGW-1998) The Office of Health and Environmental Research (OHER) of (NASA-CR-193233; NAS 1.26:193233) Avail: CASI HC A02/MF the Department of Energy (DOE) has increased the emphasis on A01 research in structural biology and molecular biology. The The purpose of the work on this project was to provide support department has increased support substantially in the area of basic for ground-based studies on the effects of gravity on eye molecular and structural biology research. To exploit the advances movements. The effects of microgravity on the optokinetic eye in these fields, OHER has sought to apply those advances in movements of humans are investigated. OKN was induced by their other areas of responsibility, e.g., health effects research, having subjects watch 3.3 deg stripes moving at 35 deg/s for 45 environmental biology, and, in particular, nuclear medicine. The s in a binocular, head-fixed apparatus. The field (hor., 88 deg; applications of biotechnology have contributed greatly to the vert., 72 deg), was rotated about axes that were upright or tilted productive research efforts of molecular biology. These techniques 45 deg or 90 deg. The head was upright or tilted 45 deg on the include gene manipulation for targeted gene delivery; body. Head-horizontal (yaw axis) and head-vertical (pitch axis) characterization of molecular probes for hormone, tumor, and components of OKN were recorded with electro-oculography neuroreceptors; the receptor-agonist/antagonist binding (EOG). Slow phase velocity vectors were determined relative to interactions; studies of mechanisms of cellular communication; and gravity. With the head upright, the axis of eye rotation during yaw the development of in vitro diagnostics such as molecular probes axis OKN was coincident with the stimulus axis and the spatial for studying the aging process and patients with mental disorders, vertical. With the head tilted 45 deg on the body, a persistent cancer, and atherosclerosis. The importance of this work is the vertical component of eye velocity developed during yaw axis reasonable expectation that mainly, through an appreciation of stimulation, and there was an average shift of the axis of eye the molecular basis of disease, will the most effective and rapid rotation toward the spatial vertical of approximately 18 deg in six progress be made toward understanding, identifying, solving, and subjects. During oblique optokinetic stimulation with the head preventing specific disease processes. Critical questions arising upright, the axis of eye rotation shifted 12 deg toward the spatial before and during the workshop are how the following technologies vertical. When the head was tilted, the axis of eye rotation rotated can be applied in a practical clinical research or patient to the other side of the spatial vertical by 5.4 deg during the management setting: the recombinant DMA methodology, the same oblique stimulation. This counter-rotation of the axis of eye technology of engineered monoclonal antibodies, the new methods rotation is similar to the 'Muller (E) effect', in which the perception for protein production and purification, and the production of of the upright counter-rotates to the opposite side of the spatial transgenic animals, DOE vertical when subjects are tilted in darkness. The data were simulated by a model of OKN. Despite the short OKAN time N93-28939# Defence and Civil Inst. of Environmental Medicine, constants, strong horizontal to vertical cross-coupling was produced Downsview (Ontario). if the horizontal and vertical time constants were in proper ratio, INFLUENCE OF THE COLD BUSTER (TM) SPORTS BAR ON and there was no suppression of nystagmus orthogonal to the HEAT DEBT, MOBILIZATION AND OXIDATION OF ENERGY stimulus direction. This shows that the spatial orientation of OKN SUBSTRATES can be due to a restructuring of the system matrix of velocity <\. L. VALLERAND, I. F. SCHMEGNER, and I. JACOBS Dec. storage as a function of gravity. It is concluded that although

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human OKAN is weak, velocity storage orients the slow phase A93-39572 velocity of OKN towards the spatial vertical. Author (revised) STRUCTURED INTERVIEWS FOR PILOT SELECTION - NO INCREMENTAL VALIDITY N93-29199# Utah Univ., Salt Lake City. Ergonomics Lab. LAURIE C. WALTERS, MARK R. MILLER, and MALCOLM J. REE SUDDEN LOADING AND FATIGUE EFFECTS ON THE HUMAN (USAF, Armstrong Lab., Brooks AFB, TX) International Journal SPINE Final Report of Aviation Psychology (ISSN 1050-8414) vol. 3, no. 1 1993 DANIEL R. BAKER and DONALD S. BLOSWICK 16 Nov. 1992 p. 25-38. refs 54 p Copyright (Contract PHS-R03-OHO-2821-01) An investigation of a structured interview for the selection of (PB93-167526) Avail: CASI HC A04/MF A01 U.S. Air Force pilots was conducted on a sample of 223 pilot The effects of fatigue and load magnitude on the in vivo trainees. The interview yielded seven ratings of subject attributes, torso response of human subjects to a sudden load were analyzed including educational background, self-confidence and leadership, in six individuals. Parameter identification of the human spine was flying motivation, success in training, and success in flying various performed within a sudden loading, short duration, high intensity classes of aircraft. Two other types of predictors were also available fatigue paradigm. The findings indicated that fatigue is an important - paper-and-pencil aptitude tests and computer-driven cognitive factor under conditions of sudden loading. The fatigued subject tests of information processing and personality. Using linear does not respond in the same way as he does when not tired. It models, the validity and incremental validity of the interview as is suggested that a higher degree of injury would be expected compared to the other classes of tests were evaluated. The under conditions of fatigue. Most of the time the worker is not at interview was found to be valid but not incrementally so. Last, a the point of fatigue, and performance of certain tasks is usually partial test of a single aspect of the Dipboye (1989) process model practiced under conditions which are better than those prevalent of interviews was conducted. Author under conditions of fatigue. Two reports are being produced from the data gathered in the study. The first will examine the A93-39575 electromyographic responses of the individual and compare them INCREASING HITS AND REDUCING MISSES IN CRM/LOS to the dynamics of the torso. The second study will mathematically SCENARIOS - GUIDELINES FOR SIMULATOR SCENARIO study the compression levels expected as a result of earlier work. DEVELOPMENT The authors suggest that their most important finding was the CAROLYN PRINCE, RANDALL OSER, EDUARDO SALAS (U.S. ability to mathematically model a complex response of the torso Navy, Naval Training Systems Center, Orlando, FL), and WALTER WOODRUFF (USAF, Orlando, FL) International Journal of Aviation to a sudden load with a : ,

286 53 BEHAVIORAL SCIENCES declines in working memory capacity. Capacity declines would EEC, and Univ. de Quebec refs produce greater age differences on communication than on routine Copyright flying tasks because the communication tasks imposed a greater Human subjects tracked a visual target controlled either by a load on working memory. Author function generator (sine wave at different frequencies) or directly by the observer's arm. Gain and phase curves of the oculomotor A93-40771 response as a function of target frequency were determined. Data COGNITIVE PREDICTORS OF VIGILANCE show that the upper frequency limit of smooth pursuit is higher GERALD MATTHEWS (Dundee Univ., United Kingdom), D. R. when the target is driven by the observer's hand, confirming DAVIES, and PETER J. HOLLEY (Aston Univ., Birmingham, United previous reports that smooth pursuit can reach higher velocities Kingdom) Human Factors (ISSN 0018-7208) vol. 35, no. 1 when tracking self-moved targets. Comparative analysis of ocular March 1993 p. 3-24. Research supported by Medical Research tracking with and without manual target control showed that Council refs subjects could be classified into two groups. One group exhibited Copyright an increase in gain at high frequency, but showed no significant Three studies are reported of individual differences in phase changes. Conversely, the reverse was found in the other performance of high event rate vigilance tasks. In each study, group: a significant decrease of phase lag at high frequency and measures of attentional resource availability and elementary no change in gain. These results demonstrate the existence, within cognitive components of sustained attention were correlated with the oculo-manual coordination control system, of at least two vigilance performance. It was predicted that correlates of vigilance separate mechanisms (or strategies), tending either to synchronize should vary with two parameters of the task: the type of target the eye and arm motor activities (timing coordination) or to adjust discrimination required (simultaneous or successive) and the type their gain (spatial coordination). Author of stimuli used (sensory or symbolic). Speed and accuracy of controlled, resource-demanding visual search predicted overall A93-41322 perceptual sensitivity on three out of four successive tasks used, A STUDY OF DECISION MAKING AND PERFORMANCE IN but only one out of four simultaneous tasks, partially confirming REJECTED TAKEOFFS the hypothesis that successive tasks are more strongly WILLIAM C. ROBERSON and WILLIAM D. SHONTZ (Boeing resource-limited than simultaneous tasks. Other correlates of Commercial Airplane Group, Seattle, WA) Jul. 1992 10 p. overall level vigilance did not appear to vary systematically with SAE, International Conference on Environmental Systems, 22nd, task parameters. Few correlates of temporal decrement in Seattle, WA, July 13-16, 1992 refs perceptual sensitivity were found, possibly for statistical reasons. (SAE PAPER 921134) Copyright The data suggest that measures of controlled search may be A study was conducted in a B-737 full flight simulator at the useful in predicting vigilance on certain real-world tasks, although Boeing Customer Training facility to evaluate pilot decision making a substantial part of the variance of vigilance tasks may not be and performance under various situations in which decisions on predictable from short cognitive tasks. Author whether or not to reject a take off had to be made and executed. A total of eight (8) situations were defined in which Go/NoGo decisions had to be made near V1 speed. Subjects included 24 A93-40772* National Aeronautics and Space Administration. Boeing instructor pilots and 24 line pilots from five different airlines. Ames Research Center, Moffett Field, CA. The sequence in which pilots encountered the situations was PERFORMANCE UNDER DICHOPTIC VERSUS BINOCULAR carefully balanced across subjects to control for learning effects. VIEWING CONDITIONS - EFFECTS OF ATTENTION AND The results of the study are reported as quantitative data on RTO TASK REQUIREMENTS decisions, stopping performance, and procedure accomplishment RUTH KIMCHI (Haifa Univ., Israel), DANIEL GOPHER, YIFAT plus a summary of data derived from post-run debriefings of the RUBIN, and DAVID RAIJ (Technion - Israel Inst. of Technology, airline pilots. Lessons learned, conclusions, and recommendations Haifa) Human Factors (ISSN 0018-7208) vol. 35, no. 1 March for RTO training are presented. Author 1993 p. 35-55. Research supported by NASA refs Copyright A93-41324* National Aeronautics and Space Administration. Three experiments investigated subjects' ability to allocate Langley Research Center, Hampton, VA. attention and cope with task requirements under dichoptic versus IDENTIFICATION OF HAZARDOUS AWARENESS STATES IN binocular viewing conditions. Experiments 1 and 2 employed a MONITORING ENVIRONMENTS target detection task in compound and noncompound stimuli, and ALAN T. POPE (NASA, Langley Research Center, Hampton, VA) Experiment 3 employed a relative-proximity judgment task. The and EDWARD H. BOGART (Lockheed Engineering & Sciences tasks were performed in a focused attention condition in which Co., Hampton, VA) Jul. 1992 11 p. SAE, International subjects had to attend to the stimulus presented to one eye or Conference on Environmental Systems, 22nd, Seattle, WA, July field (under dichoptic and binocular viewing conditions, respectively) 13-16, 1992 refs while ignoring the stimulus presented to the other eye or field, (SAE PAPER 921136) Copyright and in a divided attention condition in which subjects had to attend A state identification procedure and a model for predicting to the stimuli presented to both eyes or fields. Subjects' aerospace crew/system combination that interact to produce performance was affected by the interaction of attention conditions hazardous states are describee1.1 nis procedure in conjunction with with task requirements, but it was generally the same under the model provide a capability for evaluating the design of advanced dichoptic and binocular viewing conditions. The more dependent flight deck automation concepts based on the pilot's ability to the task was on finer discrimination, the more performance was maintain effective states of awareness. The model describes impaired by divided attention. These results suggest that at least individual and situational factors that affect the likelihood that with discrete tasks and relatively short exposure durations, persons in operational settings will experience hazardous states performance when each eye is presented with a separate stimulus of awareness. AIAA is the same as when the entire field of stimulation is viewed by both eyes. Author A93-41369 THE PSYCHOLOGICAL EFFECTS OF ISOLATION ON A A93-41166 SPACE STATION - A SIMULATION STUDY DYNAMIC ANALYSIS OF HUMAN VISUO-OCULO-MANUAL RAGNAR J. VAERNES, TONE BERGAN, HOLGER URSIN, and COORDINATION CONTROL IN TARGET TRACKING TASKS MARIT WARNCKE (Norwegian Underwater Technology Centre; JEAN-LOUIS VERCHER, MICHEL VOLLE, and GABRIEL M. Bergen Univ., Norway) Jul. 1992 12 p. SAE, International GAUTHIER (Aix-Marseille I, Univ., Marseille, France) Aviation, Conference on Environmental Systems, 22nd, Seattle, WA, July Space, and Environmental Medicine (ISSN 0095-6562) vol. 64, 13-16, 1992 refs no. 6 June 1993 p. 500-506. Research supported by CNRS, (SAE PAPER 921191) Copyright

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Psychological experiments conducted within the framework of awareness. The difficulty level of the game is increased as the an Isolation Study for European Manned Space Infrastructure are awareness level value decreases and is decreased as this described. Six subjects were locked up in NUTEC's hyperbaric awareness level value increases. NASA chamber facility for a period of four weeks. Results show that simple performance such as reaction time and vigilance were unaffected during the isolation. The more complicated mental N93-28307# Aerospace Medical Research Labs., strategies showed some temporal changes throughout the 28 days. Wright-Patterson AFB, OH. The perceived workload indicated that the overall load was THEORY OF SIGNAL DETECTION AND ITS APPLICATION TO emotionally, cognitively, and physically in the middle range, even VISUAL TARGET ACQUISITION: A REVIEW OF THE though the actual working hours were up to 12 hours. AIAA LITERATURE Final Report, Oct. 1991 - May 1992 DENISE L WILSON May 1992 56 p N93-27103# Advanced Aviation Concepts, Jupiter, FL. (AD-A262920; AL-TR-1992-0083) Avail: CASI HC A04/MF A01 HOW EXPERT PILOTS THINK: COGNITIVE PROCESSES IN An operator's performance in a target acquisition task may be EXPERT DECISION MAKING Final Report influenced by variables which are not directly associated with the RICHARD J. ADAMS Feb. 1993 82 p Sponsored by DOT/FAA target and imagery but are associated with the decision rule Research and Development Service, Washington, DC employed by the operator. The separation of factors that influence (Contract DTFA01-90-C-00042) the operator's decision criterion from those that influence sensitivity (DOT/FAA/RD-93/9) Avail: CASI HC A05/MF A01 is a major contribution of the psychophysical application of the This report is the second in the investigation of the role of Theory of Signal Detection (TSD). This report focuses on practical expert cognitive processes in Aeronautical Decision Making (ADM). application of TSD to the problem of operator acquisition of targets The first report defined the differences between expert and novice in sensor imagery which ray, or may not, have been prescreened decision makers and correlated the development of expert pilot by an automatic target recognizer. The foundation of TSD in cognitive processes with training and experience. This volume Statistical Decision Theory is discussed as well as specific methods continues the research into the understanding of how pilots think for applying TSD to laboratory evaluation of the target acquisition by examining human information processing and expert problem task. A brief review is presented of target acquisition studies in solving characteristics. From this analysis, the mental attributes which TSD was utilized. DTIC critical to developing expert decision making are explained, and three basic limits on decision making are identified. These are attention span, short term memory, and long term memory. Next, the analysis examines the development of Expert Decision Making N93-28622# Civil Aeromedical Inst., Oklahoma City, OK. (EDM) from the comparison of how novices and experts perceive, ACCIDENT PRONENESS: A RESEARCH REVIEW Final Report store, organize and use their knowledge. This analysis shows that MARK D. RODGERS and ROBERT E. BLANCHARD May 1993 high levels of competence result from the interaction between 6 p knowledge organization and processing abilities. Experts are found (DOT/FAA/AM-93/9) Avail: CASI HC A02/MF A01 to possess the abilities of rapid access to, and efficient utilization Accident proneness is a concept that refers to an enduring or of a highly organized body of conceptual and procedural knowledge. stable personality characteristic that predisposes an individual That is, an elaborately structured set of associated concepts, toward having accidents. The concept is controversial and has procedures and events-based upon many years of study, training, sustained a lively debate in the literature over the past 75 years. and experience in a aviation. The use of this knowledge base is For the most part, though, continual interest has been fueled by described in terms of the characteristics of EDM related to poor experimental procedures, misinterpretation of previously perception, attention, memory, creativity, and superior situational reported results, the need to assign blame to individuals, and a awareness. Since the speed and accuracy of expert cognitive rather curious doggedness in attempting to establish a relationship processes make them take on the characteristics of insight or between accidents and personality traits, despite the lack of intuition, the role of intuition in decision making is the next analytical supporting scientific evidence. The origins of the notion of accident part of the investigation. Intuition is defined and the properties of proneness are reported and the studies that purport to support or intuition relevant to EDM delineated. Finally, the report concludes refute it are reviewed. Author (revised) by presenting alternative EDM training opportunities including: training to enhance memory, computer based training tools, and promising methods for testing pilots which will also provide training N93-28901# Georgia Univ., Athens. Dept. of Psychology. and the opportunity to learn the cognitive skills of experts without EXPERTISE, TEXT COHERENCE, AND CONSTRAINT spending all of the learning time in actual flight. Author SATISFACTION: EFFECTS ON HARMONY AND SETTLING RATE Quarterly Report N93-28128*# National Aeronautics and Space Administration. BRUCE K. BRITTON and F. J. EISENHART 8 Mar. 1993 10 p Langley Research Center, Hampton, VA. (AD-A262703) Avail: CASI HC A02/MF A01 METHOD OF ENCOURAGING ATTENTION BY CORRELATING This paper reports four experiments showing that 27 experts' VIDEO GAME DIFFICULTY WITH ATTENTION LEVEL Patent mental representations had significantly higher harmony and faster Application settling rates than 652 novices when activation was spread through ALAN T. POPE, inventor (to NASA) and EDWARD H. BOGART, the representations in a simulation of thinking; that when coherent inventor (to NASA) (Lockheed Engineering and Sciences Co., texts were read by novices, they produced mental representations Hampton, VA.) 8 Mar. 1993 37 p with significantly higher harmony and faster settling rates than (NASA-CASE-LAR-15022-1; NAS 1.71 :LAR-15022-1; less coherent texts; and that novices whose representations US-PATENT-APPL-SN-029808) Avail: CASI HC A03/MF A01 matched the experts' mental representations had significantly A method of encouraging attention in persons such as those higher harmony and faster settling rates. The results were found suffering from Attention Deficit Disorder is provided by correlating for declarative experts in history and procedural experts in literary the level of difficulty of a video game with the level of attention in interpretation, for Dutch and American experts, for novice groups a subject. A conventional video game comprises a video display including U.S. Air Force recruits and U.S. and Dutch which depicts objects for interaction with a player and a difficulty undergraduates, and for both history texts and literary texts. These adjuster which increases the difficulty level, e.g., action speed results were consistent with our hypothesis that the quality of a and/or evasiveness of the depicted object, in a predetermined person's prior knowledge determines the harmony and settling manner. The electrical activity of the brain is measured at selected rates of their representations and that these can be measured by sites to determine levels of awareness, e.g., activity in the beta, simulating the spread of activation through the person's mental theta, and alpha states. A value is generated based on this representation of a subject matter domain. Harmony may also be measured electrical signal which is indicative of the level of used as a metacognitive signal. DTIC

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54 of 16 months. Safety and health were not compromised and job performance was favorably affected. AIAA MAN/SYSTEM TECHNOLOGY AND LIFE A93-41173 SUPPORT PREVALENCE OF CORRECTIVE LENS WEAR IN ROYAL AUSTRALIAN AIR FORCE FLIGHT CREWS Includes human engineering; biotechnology; and space suits and MICHAEL R. MORK and LAURANCE A. WATSON (USAF, protective clothing. Aerospace Medicine Div., Hickam AFB, HI) Aviation, Space, and Environmental Medicine (ISSN 0095-6562) vol. 64, no. 6 June 1993 p. 541-545. refs A93-39573 Copyright AN EXPLORATORY STUDY OF PLAN-VIEW TERRAIN The effect of restrictive entry visual standards for the Royal DISPLAYS FOR AIR CARRIER OPERATIONS Australian Air Force (RAAF) on the prevalence of corrective lens JAMES K. KUCHAR and R. J. HANSMAN, JR. (MIT, Cambridge, wear in its aircrew were studied. Entry visual refraction standards MA) International Journal of Aviation Psychology (ISSN for the RAAF and USAF were compared. It is found that the 1050-8414) vol. 3, no. 1 1993 p. 39-54. refs RAAF's standards for entry into aircrew training programs (Contract DTRS-57-88-C-00078) significantly reduced the prevalence of corrective lens wear among Copyright all crew positions when compared to the USAF. AIAA Two prototypical terrain situational awareness (TSA) displays were examined in a preliminary part-task simulation study using A93-41174 the MIT Aeronautical Systems Laboratory Advanced Cockpit NEW TECHNOLOGIES FOR IN-FLIGHT PASTELESS Simulator. Pilots, qualified on autoflight aircraft, flew simulated BIOELECTRODES approaches while using a moving-map terrain display in addition DAVID PRUTCHI (Tel Aviv Univ., Israel) and ALYSIA M. to typical glass-cockpit navigation displays. During the simulation, SAGI-DOLEV (Israeli Air Force, Aeromedical Center, Ramat Gan, TSA was evaluated by issuing erroneous air traffic control (ATC) Israel) Aviation, Space, and Environmental Medicine (ISSN vectors toward hazardous terrain. When given vectors toward such 0095-6562) vol. 64, no. 6 June 1993 p. 552-556. Research terrain, there was a 50 percent overall hazard-recognition rate supported by Tel Aviv Univ refs when pilots used a terrain display based on current terrain-depiction Copyright methods and a 78 percent recognition rate when using a terrain Advances in development of in-flight electrophysiological based display based on smoothed-contour terrain depiction. After the systems such as G-LOC detectors, ECG-synchronized G-suits, and subject-pilots realized they could not rely on ATC for terrain clinical monitors have dictated the need for pasteless electrodes separation, hazard-recognition rates increased from 20 percent to that meet realistic operational demands and are suitable for the 62 percent for the display based on current depiction methods cockpit environment. New technologies appropriate for the design and from 25 percent to 93 percent for the smoothed-contour of bioelectrodes that meet these demands are described, including display. Advanced terrain displays appear to be an effective means a stable dielectric electrode-skin interface material, miniaturized by which flight crews can ensure terrain separation without reliance high-impedance electronics, and circuit fabrication methods. Design on ATC. Author examples and resulting electrophysiological recordings are presented to demonstrate the new technologies. Author A93-39574 A93-41175 INSTRUMENT-APPROACH-PLATE DESIGN CONSIDERATIONS FOR DISPLAYING RADIO FREQUENCIES SIMULATING REDUCED GRAVITY - A REVIEW OF JORDAN MULTER, ROBERT DISARIO, M. S. HUNTLEY, JR. (DOT, BIOMECHANICAL ISSUES PERTAINING TO HUMAN National Transportation Systems Center, Cambridge, MA), and LOCOMOTION MARGARET WARNER (EG&G Dynatrend, Inc., Cambridge, MA) BRIAN L. DAVIS (Pennsylvania State Univ., University Park; International Journal of Aviation Psychology (ISSN 1050-8414) vol. Cleveland Clinic Foundation, Dept. of Biomedical Engineering and 3, no. 1 1993 p. 55-68. Research supported by FAA refs Applied Therapeutics, OH) and P. R. CAVANAGH (Pennsylvania Copyright State Univ., University Park) Aviation, Space, and Environmental This experiment examined the effectiveness of four different Medicine (ISSN 0095-6562) vol. 64, no. 6 June 1993 p. layouts for displaying radio frequencies on instrument approach 557-566. refs plates. Three of the four layouts were similar to those found in Copyright existing charts published by the National Oceanic and Atmospheric Findings in neuromuscular and biomechanical issues in the Administration (NOAA), Jeppesen Sanderson, Inc., and the context of human locomotion research are reviewed. The research Canadian Department of Energy, Mines, and Resources. The fourth was based on water immersion, parabolic aircraft flights, supine layout was a two-column format not currently found on existing and erect cable suspension, and centrifugal methods. Data obtained charts. Subjects' performance with the two column and boxed indicate that the present shuttle treadmill running surface would layouts was found to be superior to that of subjects' performance not suffice for its operation at levels greater than 0.6 G. To replicate with the one-column layouts representative of NOAA and Jeppesen typical ground reaction force profiles during locomoter exercise at charts. Author reduced gravity levels it is easier to match the peak rates of the force change than to match values of the peak force magnitudes. AIAA A93-41172 CONTACT LENSES IN AVIATION - THE MARINE CORPS A93-41306 EXPERIENCE SPACE STATION WATER PROCESSOR - CURRENT FLIGHT MICHAEL H. MITTELMAN, BRIAN SIEGEL, and DAVID L STILL DESIGN (U.S. Navy, Naval Aerospace Medical Inst., Pensacola, FL) ALBERT M. BOEHM, ARTHUR K. COLLING, JR., MICHAEL J. Aviation, Space, and Environmental Medicine (ISSN 0095-6562) HELDMANN, JOHN W. STEELE (Hamilton Standard, Windsor vol. 64, no. 6 June 1993 p. 538-540. refs Locks, CT), and R. G. SHAW (Boeing Defense & Space Group, Copyright Seattle, WA) Jul. 1992 10 p. SAE, International Conference Application of contact lenses in the unique U.S. Marine Corps on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 aviation environment which encompasses shipboard, land-based, (SAE PAPER 921112) Copyright and forwardly deployed units, was evaluated in 90 pilots focusing An updated version of a Water Processor (WP) system which on flex-wear disposable lenses. Results revealed that 68 pilots combines a Potable Water Processor and a Hygiene Water were successfully fit and continued contact lens wear for a period Processor is presented. The WP system is aimed at processing

289 54 MAN/SYSTEM TECHNOLOGY AND LIFE SUPPORT the waste hygiene, handwash, and laundry waters, the temperature A93-41311* Jet Propulsion Lab., California Inst. of Tech., and humidity control condensale, Shuttle fuel cell water, and the Pasadena. urine distillate, to produce potable quality water. The WP major HUMAN LIFE SUPPORT DURING INTERPLANETARY TRAVEL functions include waste water collection and storage, processed AND DOMICILE. V - MARS EXPEDITION TECHNOLOGY water storage and delivery, contaminant removal, and microbial TRADE STUDY FOR SOLID WASTE MANAGEMENT separation between the waste and processed water. Key JOE FERRALL, NARESH K. ROHATGI, and P. K. SESHAN (JPL, components of the WP encompass an inlet water separator that Pasadena, CA) Jul. 1992 20 p. SAE, International Conference removes the free gas that is mixed with the inlet waste water, a on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 high temperature sterilizer, particulate filters, multifiltration beds, refs and the volatile removal apparatus. AIAA (SAE PAPER 921119) Copyright A model has been developed for NASA to quantitatively compare and select life support systems and technology options. A93-41307 The model consists of a modular, top-down hierarchical breakdown AN UPDATE ON THE READINESS OF VAPOR COMPRESSION of the life support system into subsystems, and further breakdown DISTILLATION FOR SPACECRAFT WASTEWATER of subsystems into functional elements representing individual PROCESSING processing technologies. This paper includes the technology trades LAWRENCE D. NOBLE, JR., FRANZ H. SCHUBERT, and ROBERT for a Mars mission, using solid waste treatment technologies to P. WERNER (Life Systems, Inc., Cleveland, OH) Jul. 1992 11 recover water from selected liquid and solid waste streams. p. SAE, International Conference on Environmental Systems, Technologies include freeze drying, thermal drying, wet oxidation, 22nd, Seattle, WA, July 13-16, 1992 refs combustion, and supercritical-water oxidation. The use of these (SAE PAPER 921114) Copyright technologies does not have any significant advantages with respect An account is given of the development status of the to weight; however, significant power penalties are incurred. A NASA-Space Station Freedom Urine Processor Assembly (UPA), benefit is the ability to convert hazardous waste into a useful which employs a vapor compression distillation cycle. Recent resource, namely water. Author (revised) design efforts have concentrated on the systems's Orbital-Replacement Units, giving attention to process control loops, fault-detection, and fault isolation. The UPA's performance A93-41312* Jet Propulsion Lab., California Inst. of Tech., capabilities show it to be the most mature of available systems Pasadena. for both orbital and interplanetary spacecraft. AIAA HUMAN LIFE SUPPORT DURING INTERPLANETARY TRAVEL AND DOMICILE. VI - GENERIC MODULAR FLOW SCHEMATIC FOR HYBRID PHYSICAL/CHEMICAL-BIOLOGICAL LIFE A93-41309* National Aeronautics and Space Administration. SUPPORT SYSTEMS Marshall Space Flight Center, Huntsville, AL. GANI B. GANAPATHI, P. K. SESHAN, JOSEPH FERRALL, and PHASE III INTEGRATED WATER RECOVERY TESTING AT NARESH ROHATGI (JPL, Pasadena, CA) Jul. 1992 24 p. MSFC - CLOSED HYGIENE AND POTABLE LOOP TEST SAE, International Conference on Environmental Systems, 22nd, RESULTS AND LESSON LEARNED Seattle, WA, July 13-16, 1992 refs DONALD W. HOLDER, JR. and ROBERT M. BAGDIGIAN (NASA, (SAE PAPER 921120) Copyright Marshall Space Flight Center, Huntsville, AL) Jul. 1992 16 p. An extension is proposed for the NASA Space Exploration SAE, International Conference on Environmental Systems, 22nd, Initiative's Generic Modular Flow Schematics for physical/chemical Seattle, WA, July 13-16, 1992 refs life support systems which involves the addition of biological (SAE PAPER 921117) Copyright processes. The new system architecture includes plant, microbial, A series of tests has been conducted at the NASA Marshall and animal habitat, as well as the human habitat subsystem. Major Space Flight Center (MSFC) to evaluate the performance of a Feedstock Production and Food Preparation and Packaging Space Station Freedom (SSF) pre-development water recovery components have also been incorporated. Inedible plant, system. Potable, hygiene, and urine reclamation subsystems were aquaculture, microbial, and animal solids are processed for integrated with end-use equipment items and successfully operated recycling. AIAA for a total of 35 days, including 23 days in closed-loop mode with man-in-the-loop. Although several significant subsystem physical anomalies were encountered, reclaimed potable and hygiene water A93-41313* National Aeronautics and Space Administration. routinely met current SSF water quality specifications. This paper Ames Research Center, Moffett Field, CA. summarizes the test objectives, system design, test RECYCLING AND SOURCE REDUCTION FOR LONG activities/protocols, significant results/anomalies, and major DURATION SPACE HABITATION lessons learned. Author T. M. HIGHTOWER (NASA, Ames Research Center, Moffett Field, CA) Jul. 1992 23 p. SAE, International Conference on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 A93-41310 National Aeronautics and Space Administration, refs Washington, DC. (SAE PAPER 921121) Copyright OVERVIEW OF NASA'S 1991 LIFE SUPPORT SYSTEMS A direct mathematical approach has been established for ANALYSIS WORKSHOP characterizing the performance of closed-loop life support systems. PEGGY L. EVANICH (NASA, Washington), P. K. SESHAN (JPL, The understanding that this approach gives clearly illustrates the Pasadena, CA), CHIN LIN (NASA, Johnson Space Center, Houston, options available for increasing the performance of a life support TX), VINCENT BILARDO (NASA, Ames Research Center, Moffett system by changing various parameters. New terms are defined Field, CA), and THOMAS M. CRABB (Orbital Technologies Corp., and utilized, such as Segregation Factor, Resource Recovery Madison, Wl) Jul. 1992 13 p. SAE, International Conference Efficiency, Overall Reclamation Efficiency, Resupply Reduction on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 Factor, and Life Support Extension Factor. The effects of increases (SAE PAPER 921118) Copyright in expendable system supplies required due to increases in life Results from the first NASA Life Support Systems Analysis support system complexity are shown. Minimizing resupply through Workshop conducted by the Office of Aeronautics and Space increased recycling and source reduction is illustrated. The effects Technology on June 24-27, 1991, in Milwaukee, Wisconsin are of recycling upon resupply launch cost is also shown. Finally, reviewed. Attention is also given to a bn'ef review of the second material balance analyses have been performed based on quantity workshop held on May 12-14, 1992. It is noted that the workshops and composition data for both supplies and wastes, to illustrate defined the key issues and characterized the status of current the use of this approach by comparing ten different closed-loop developments in life support systems analysis. AIAA life support system cases. Author

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A93-41314* National Aeronautics and Space Administration. Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 Lyndon B. Johnson Space Center, Houston, TX. refs ANALYSIS OF THE VARIABLE PRESSURE GROWTH (SAE PAPER 921129) Copyright CHAMBER USING THE CASE/A SIMULATION PACKAGE Biosphere 2 is a large closed ecological system occupied by CARL D. MCFADDEN (McDonnell Douglas Space Systems, eight human inhabitants in complete material isolation. It has been Huntington Beach, CA) and MARYBETH A. EDEEN (NASA, in operation continuously for 9 months of the initial 2 year run Johnson Space Center, Houston, TX) Jul. 1992 12 p. SAE, which commenced on Sept 26, 1991. The major areas of International Conference on Environmental Systems, 22nd, Seattle, observation summarized in this paper are the dynamics of WA, July 13-16, 1992 refs atmospheric composition, food production, health, quantification (SAE PAPER 921122) Copyright of leakage, plant growth, and species survival. Author A computer simulation of the Variable Pressure Growth Chamber (VPGC), located at the NASA Johnson Space Center, has been developed using the Computer Aided Systems Engineering and A93-41319 Analysis (CASE/A) package. The model has been used to perform THE EFFECT OF GEOMETRIC FIELD OF VIEW AND TUNNEL several analyses of the VPGC. The analyses consisted of a study DESIGN FOR PERSPECTIVE FLIGHT-PATH DISPLAYS of the effects of a human metabolic load on the VPGC and a WOODROW BARFIELD and CRAIG ROSENBERG (Washington study of two new configurations for the temperature and humidity Univ., Seattle) Jul. 1992 8 p. SAE, International Conference control (THC) subsystem in the VPGC. The objective of the human on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 load analysis was to study the effects of a human metabolic load Research supported by Boeing Military Airplane Co. refs on the air revitalization and THC subsystems. This included the (Contract NSF DMC-88-57851; NSF CDA-88-06866) effects on the quantity of carbon dioxide injected and oxygen (SAE PAPER 921131) Copyright removed from the chamber and the effects of the additional Previous studies have shown that use of flight-path displays sensible and latent heat loads. The objective of the configuration may lead to increased situational awareness during final approach analysis was to compare the two new THC configurations against and landing. However, there are a number of research issues the current THC configuration to determine which had the best which remain to be investigated concerning the optimum design performance. Author of a perspective flight-path display. The purpose of this paper is to report the results of a study which investigated the relationship between the geometric field of view, number of tunnels in the A93-41315 display, and flight-path complexity on the subject's ability to fly a TRIALSS - TOOL FOR RAPID AND INTELLIGENT ADVANCED computer-simulated aircraft during final approach. Implications of LIFE SUPPORT SYSTEM SELECTION AND SIZING the results for the design of perspective flight-path displays are SUSAN DOLL and BRIAN TILLOTSON (Boeing Defense & Space discussed. Author Group, Seattle, WA) Jul. 1992 10 p. SAE, International Conference on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 refs A93-41320 (SAE PAPER 921123) Copyright FLIGHT DECK AUTOMATION AND PILOT WORKLOAD TRIALSS is a tool which makes use of modern software BARRY H. KANTOWITZ (Battelle Seattle Research Center, WA) technology to assist in the life support systems (LSS) analysis Jul. 1992 8 p. SAE, International Conference on Environmental process. TRIALSS has an icon-driven, user-friendly interface which Systems, 22nd, Seattle, WA, July 13-16, 1992 refs allows the user to select from several physical/chemical LSS (SAE PAPER 921132) Copyright technologies. It displays power, mass, and volume at system, This article focuses upon some of the potential problems that subsystem, and assembly levels. A unique feature of TRIALSS is can occur with 'glass cockpits', especially as they relate to pilot the ability to easily vary mission parameters, including crew size, workload. The goal is not to condemn automation but to emphasize mission duration and location, power and thermal control system potential problems so that they can be avoided in the future. The technologies, pressurized volume construction, and launch and implementation of automation should be human-centered, with due transportation vehicle options. A powerful development appreciation of the limitations and expectations of the pilots who environment, G2, allows the programmer to make rapid changes are the end users of such automation. Author (revised) or additions and to incorporate rules to help the user avoid pitfalls. An example analysis for lunar applications shows the importance of mission context for system-level analysis, and demonstrates A93-41321 the utility of TRIALSS in enabling such analyses. TOWARD A FLIGHT DECK AUTOMATION PHILOSOPHY FOR Author (revised) THE BOEING HIGH SPEED CIVIL TRANSPORT DAVID M. REGAL and ROLF J. BRAUNE (Boeing Commercial Airplane Group, Seattle, WA) Jul. 1992 9 p. SAE, International A93-41316 Conference on Environmental Systems, 22nd, Seattle, WA, July A LOW PRESSURE ELECTROLYZER FOR THE NEXT 13-16, 1992 refs GENERATION SUBMARINE (SAE PAPER 921133) Copyright ANDREI LEONIDA, JAMES F. MCELROY, and ROGER N. In this paper we address the role that automation will play in SEXAUER (Hamilton Standard, Windsor Locks, CT) .Jul. 1992 an advanced High Speed Civil Transport (HSCT) flight deck. It is 7 p. SAE, International Conference on Environmental Systems, argued that an automation philosophy is necessary to optimize 22nd, Seattle, WA, July 13-16, 1992 design in the face of new technology that creates additional design (SAE PAPER 921125) Copyright options and adds to the complexity of the future flight deck design A low-pressure oxygen generation system for advanced process. An overview of issues that influence the determination submarine life support is presented which makes it possible to of an automation philosophy are presented along with specific achieve significant cost savings. It is concluded that single cell items that will be part of that philosophy. We do not provide a performance at high differential pressure confirmed the feasibility comprehensive automation philosophy at this time, however. After of low pressure water electrolysis for a submarine oxygen a brief summary of Boeing's HSCT program, a detailed definition generator. AIAA of automation, as it applies to the flight deck, is provided. A systems approach to flight deck design is described which is based on A93-41317 satisfying the aircraft's non-normal as well as normal mission BIOSPHERE 2 • OVERVIEW OF SYSTEM PERFORMANCE requirements. Areas where pilots can make their strongest DURING THE FIRST NINE MONTHS contributions as part of an overall flight deck system are identified, WILLIAM F. DEMPSTER (Space Biospheres Ventures, Oracle, but it is suggested that the full potential of the crew can only be AZ) Jul. 1992 7 p. SAE, International Conference on realized through the use of human-centered automation. Author

291 54 MAN/SYSTEM TECHNOLOGY AND LIFE SUPPORT

A93-41323* National Aeronautics and Space Administration. Automated Microbiological Identification System. Attention is given Ames Research Center, Moffett Field, CA. to Glovebox volume relations to the user's functional and other VISUALIZATION AND MODELING OF FACTORS INFLUENCING human factors, ventilation system components, lighting conditions, VISIBILITY IN COMPUTER-AIDED CREWSTATION DESIGN and display and control locations. Maintainability has been a ARIES ARDITI, STEVEN AZUETA (Lighthouse, Inc., New York), prominent consideration throughout, due to limited on-orbit JAMES LARIMER (NASA, Ames Research Center, Moffett Field, resources. AIAA CA), MICHAEL PREVOST (Sterling Software, Inc., Palo Alto, CA), JEFFREY LUBIN, and JAMES BERGEN (David Sarnoff Research A93-41327 National Aeronautics and Space Administration, Center, Princeton, NJ) Jul. 1992 12 p. SAE, International Washington, DC. Conference on Environmental Systems, 22nd, Seattle, WA, July PROGRAM DEVELOPMENT FOR EXERCISE 13-16, 1992 refs COUNTERMEASURES (Contract NCC2-541; NAS2-12852) J. C. HAYES (Krug Life Sciences, Houston, TX), D. F. STEWART (SAE PAPER 921135) Copyright (NASA, Washington), B. A. HARRIS, S. F. SICONOLFI, M. C. We have developed two modules for use in computer-aided GREENISEN, and F. T. LAROCHELLE (NASA, Johnson Space design (CAD) of crewstation environments that enhance the Center, Houston, TX) Jul. 1992 8 p. SAE, International designer's appreciation of factors influencing the pilot's vision and Conference on Environmental Systems, 22nd, Seattle, WA, July visual processing capacity. The Binocular Optics Module (BOM) is 13-16, 1992 refs an interactive tool for visualizing geometric aspects of (1) how (SAE PAPER 921140) Copyright retinal imagery of the environment changes on the pilot's retinas The concern of NASA's Exercise Countermeasures Project under conditions of eye and object motion, and (2) how visual (ECP) is to ensure crew physical effectiveness for flight- or capabilities that can be modeled as regions or contours on the mission-related tasks, and encompasses postflight as well as retinas, affect spatial perception of the environment. The Visual preflight and inflight exercise components. Attention is given to Performance Module (VPM) contains a signal processing model the implementation of ECP via the Space Shuttle Orbiter's treadmill, of human visual discrimination that quantitatively predicts visual rower, cycle ergometer, and lower body negative pressure discrimination performance. The outputs of the VPM are retinal apparatus. AIAA contours that represent performance probabilities. These contours may be used as inputs to the BOM for visualizing those volumes of space within the crewstation that bound different levels of the A93-41328 pilot's of visual discrimination capability. Used together, the BOM HYPERBARIC TREATMENT OPERATIONS ABOARD SPACE and VPM provide the designer with the opportunity to interactively STATION FREEDOM explore relationships between environmental retinal imagery and COURTNEY A. BUCK and MICHAEL F. STOLLE (McDonnell visual function, and the ability to factor the pilot's visual capabilities Douglas Space Systems, Space Station Div., Huntington Beach, into the earliest phases of crewstation CAD. Author CA) Jul. 1992 16 p. SAE, International Conference on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 A93-41325* National Aeronautics and Space Administration. refs Lyndon B. Johnson Space Center, Houston, TX. (SAE PAPER 921142) Copyright SPACE STATION FREEDOM ENVIRONMENTAL HEALTH Hyperbaric operations are required onboard Space Station CARE PROGRAM Freedom to treat decompression sickness, air embolism, and ELIZABETH E. RICHARD (Krug Life Sciences, Inc., Houston, TX) ebullism and are essential to assure a continuing EVA capability. and DANE M. RUSSO (NASA, Johnson Space Center, Houston, The Space Station Airlock provides the resources and equipment TX) Jul. 1992 9 p. SAE, International Conference on to accommodate hyperbaric operations, as well as a number of Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 other operations including nominal EVA egress and ingress, refs prebreathing procedures, and space suit servicing. The Space (SAE PAPER 921138) Copyright Station Airlock has two chambers: the crewlock and the equipment The paper discusses the environmental planning and monitoring lock. The crewlock is used as the hyperbaric chamber and can aspects of the Space Station Freedom (SSF) Environmental Health be pressurized to 41.1 psia for treatment. Both the crewlock and Care Program, which encompasses all phases of the SSF assembly the equipment lock contain medical equipment and environmental and operation from the first element entry at MB-6 through the control equipment to support hyperbaric operations. This paper Permanent Manned Capability and beyond. Environmental planning discusses the role that both chambers play in efficiently involves the definition of acceptability limits and monitoring accommodating the equipment in support of required hyperbaric requirements for the radiation dose barothermal parameters and procedures. In addition, a description of the medical hardware is potential contaminants in the SSF air and water and on internal offered, and the likely responsibilities and scenarios that include surfaces. Inflight monitoring will be implemented through the the two crew medical officers are detailed. Author (revised) Environmental Health System, which consists of five subsystems: Microbiology, Toxicology, Water Quality, Radiation, and Barothermal A93-41333 Physiology. In addition to the environmental data interpretation THE DEVELOPMENT OF AN ATMOSPHERE COMPOSITION and analysis conducted after each mission, the new data will be MONITOR FOR THE ENVIRONMENTAL CONTROL AND LIFE compared to archived data for statistical and long-term trend SUPPORT SYSTEM analysis and determination of risk exposures. Results of these WILLIAM NIU, MARY ROTHERAM, WALLY DENCKER, and analyses will be used to modify the acceptability limits and LAARNI DAVIDSON (Perkin-Elmer Corp., Pomona, CA) Jul. monitoring requirements for the future. AIAA 1992 12 p. SAE, International Conference on Environmental Systems, 22nd, Seattle, WA, July 13-16,1992 Research supported A93-41326 by Boeing Aerospace & Electronics refs GLOVEBOX DESIGN FOR SPACE STATION FREEDOM CREW (SAE PAPER 921149) Copyright HEALTH CARE SYSTEM The Atmosphere Composition Monitor (ACM), which is a part FRANK T. EICHSTADT (McDonnell Douglas Space Systems, Space of the Environmental Control and Life Support System being Station Div., Huntington Beach, CA) Jul. 1992 12 p. SAE, developed for the Space Station Freedom, is described. The ACM International Conference on Environmental Systems, 22nd, Seattle, will measure the major atmospheric constituents in the cabin to WA, July 13-16, 1992 provide feedback for the nitrogen/oxygen replenishment control, (SAE PAPER 921139) Copyright as well particulates and minor gaseous constituents. The An account is given of the design status of the NASA-SSF instruments of the ACM system include a single focusing mass Environmental Health System 'Glovebox', whose microbiology spectrometer to monitor major air constituents; a gas equipment encompasses incubators, a slide-stainer, and an chromatograph/mass spectrometer, to detect trace organic

292 54 MAN/SYSTEM TECHNOLOGY AND LIFE SUPPORT contaminants resulting from material outgassing; a nondispersive THOMAS F. CALLAGHAN, JOHN W. GOSBEE (Lockheed IR spectrometer, to determine CO concentration; and a laser Engineering & Sciences Co., Houston, TX), and SUSAN C. ADAM particle counter for measuring particulates in air. AIAA (NASA, Johnson Space Center, Houston, TX) Jul. 1992 11 p. SAE, International Conference on Environmental Systems, 22nd, A93-41335 Seattle, WA, July 13-16, 1992 refs OXYGEN GENERATION BY STATIC FEEDWATER (SAE PAPER 921156) Copyright ELECTROLYSIS FOR SPACE STATION FREEDOM The Human Factors Assessment of Orbiter Missions (Detailed MICHAEL G. WOOD (Boeing Defense & Space Group, Huntsville, Supplementary Objective 904) was conducted on STS-40 (Spacelab AL) Jul. 1992 11 p. SAE, International Conference on Life Sciences 1) in order to bring human factors into the operational Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 world of manned space flight. This paper describes some of its Research supported by Life Systems, Inc refs methods. Included are explanations of general and space human (SAE PAPER 921151) Copyright factors, and a description of DSO 904 study objectives and results. The paper describes the Static Feed Water Electrolysis System The methods described include ways to collect background (SFWES), designed for the ECLSS as part of the Atmosphere information for studies and also different in-flight data collection Revitalization Subsystem, with particular attention given to the techniques. Several lessons for the space human factors engineer technology and operation of the SFWES. The SFWES will generate are reflected in this paper. First, method development is just as oxygen and hydrogen aboard the Space Station Freedom from important as standards generation. Second, results of investigations water obtained from the potable water processor. Oxygen will be should always have applicability to design. Third, cooperation with produced at a level sufficient to support astronaut metabolic other NASA groups is essential. Finally, the human is the most consumption, animal metabolic consumption, experiment ingestion, important component of the space exploration system, and often cabin leakage, and airlock loss. The hydrogen byproduct will enter the most difficult to study. Author the Carbon Dioxide Reduction Subassembly where the hydrogen will react with concentrated CO2 to form recyclable water and A93-41340* National Aeronautics and Space Administration. waste methane. Results of testing to date are presented, and the Lyndon B. Johnson Space Center, Houston, TX. viability of the SFWES as the oxygen generator for SSF is A STUDY TO EXPLORE LOCOMOTION PATTERNS IN discussed. AIAA PARTIAL GRAVITY ENVIRONMENTS SUDHAKAR L. RAJULU (Lockheed Engineering & Sciences Co., A93-41337* National Aeronautics and Space Administration. Houston, TX), GLENN K. KLUTE, and NATHAN R. MOORE (NASA, Lyndon B. Johnson Space Center, Houston, TX. Johnson Space Center, Houston, TX) Jul. 1992 12 p. SAE, A COMPARISON OF TWO SHUTTLE LAUNCH AND ENTRY International Conference on Environmental Systems, 22nd, Seattle, SUITS - REACH ENVELOPE, ISOKINETIC STRENGTH, AND WA, July 13-16, 1992 refs TREADMILL TESTS (SAE PAPER 921157) Copyright LAUREN E. SCHAFER, SUDHAKAR L. RAJULU (Lockheed An effort is made to ascertain the factors affecting stability Engineering & Sciences Co., Houston, TX), and GLENN K. KLUTE during locomotion in lunar and Martian gravity environments, as (NASA, Johnson Space Center, Houston, TX) Jul. 1992 7 p. well as to establish criteria for the enhancement of stability and SAE, International Conference on Environmental Systems, 22nd, traction. The effects of changing both the speed and the pattern Seattle, WA, July 13-16, 1992 of locomotion under three different gravity conditions were (SAE PAPER 921154) Copyright investigated. As gravity level increased, vertical and horizontal A quantification has been conducted of any existing differences forces significantly declined; similarities were noted across gravity between the performance, in operational conditions, of the Space levels, however, with respect to locomotion speed and pattern Shuttle crew Launch Entry Suit (LES) and the new Advanced changes, where increasing speed enhanced both vertical and Crew Escape Suit (ACES). While LES is a partial-pressure suit, horizontal forces. With decreasing gravity, the ratio of horizontal the ACES system which is being considered as a replacement for to vertical forces increased significantly. AIAA LES is a full-pressure suit. Three tests have been conducted with six subjects to ascertain the suits' reach envelope, strength, and A93-41341* National Aeronautics and Space Administration. treadmill performance. No significant operational differences were Ames Research Center, Moffett Field, CA. found between the two suit designs. AIAA THE CENTRIFUGE FACILITY LIFE SCIENCES GLOVEBOX CONFIGURATION STUDY A93-41338* National Aeronautics and Space Administration. SIDNEY C. SUN (NASA, Ames Research Center, Moffett Field, Lyndon B. Johnson Space Center, Houston, TX. CA) and CARLA V. GOULART (Colorado Univ., Boulder) Jul. PILOT INVESTIGATION - NOMINAL CREW INDUCED FORCES 1992 13 p. SAE, International Conference on Environmental IN ZERO-G Systems, 22nd, Seattle, WA, July 13-16, 1992 refs GLENN K. KLUTE (NASA, Johnson Space Center, Houston, TX) (SAE PAPER 921158) Copyright Jul. 1992 8 p. SAE, International Conference on Environmental Crew operations associated .with nonhuman life sciences Systems, 22nd, Seattle, WA, July 13-16, 1992 refs research on Space Station Freedom will be conducted in the Life (SAE PAPER 921155) Copyright Sciences Glovebox, whose enclosed work volume must This report presents pilot-study data of test subject forces accommodate numerous life science procedures. Two candidate induced by intravehicular activities such as push-offs and landings Glovebox work volume concepts have been developed: one in with both hands and feet. Five subjects participated in this which two operators work side-by-side, and another that conforms investigation. Three orthogonal force axes were measured in the to the reach envelope of a single operator. Six test volunteers NASA KC-135 research aircraft's 'zero-g' environment. The largest tested the concepts according to preestablished operational criteria. forces were induced during vertical foot push-offs, including one The wrap-around, single-operator concept has been judged the of 534 newtons (120 Ibs). The mean vertical foot push-off was superior system. AIAA 311 newtons (70 Ibs). The vertical hand push-off forces were also relatively large, including one of 267 newtons (60 Ibs) with a mean A93-41342 of 151 newtons (34 Ibs). These force magnitudes of these forces ZERO GRAVITY PHASE SEPARATOR TECHNOLOGIES - would result in a Shuttle gravity environment of about 1 x exp 10 PAST, PRESENT AND FUTURE -4 g's. Author (revised) W. C. DEAN (Hamilton Standard, Windsor Locks, CT) Jul. 1992 9 p. SAE, International Conference on Environmental Systems, A93-41339* National Aeronautics and Space Administration. 22nd, Seattle, WA, July 13-16, 1992 Lyndon B. Johnson Space Center, Houston, TX. (SAE PAPER 921160) Copyright OPERATIONAL SPACE HUMAN FACTORS - METHODOLOGY Accounts are given of the development history, current status FOR A DSO and prospective trends in the design of systems for removing

293 54 MAN/SYSTEM TECHNOLOGY AND LIFE SUPPORT condensate from temperature/humidity control heat exchangers and the Water Recovery and Management Subsystem (WRMS), in zero gravity. Attention is given to such major configurational which will allow extended testing of equipment under microgravity possibilities as the integral-wick and face-wick separators, the conditions. The separate designs for the ARS and the WRMS hydrophylic-coated hollow-chamber 'slurper', the elbow wick, and include storage tanks, plumbing, and limited instrumentation that the hydrophylic gas trap. AIAA would be expected to be common to all air or water treatment equipment of interest. The beds are designed to recycle process A93-41343* National Aeronautics and Space Administration. fluids to the greatest extent possible, thus minimizing the Lyndon B. Johnson Space Center, Houston, TX. spacecraft/test bed interface requirements. Schematic diagrams DESIGN OF A SHUTTLE AIR AND WATER PREFILTER FOR of both the ARS and the WRMS test beds are included. AIAA REDUCED GRAVITY OPERATION EUGENE K. UNGAR and FRED A. OUELLETTE (NASA, Johnson A93-41365* National Aeronautics and Space Administration. Space Center, Houston, TX) Jul. 1992 10 p. SAE, International Marshall Space Flight Center, Huntsville, AL. Conference on Environmental Systems, 22nd, Seattle, WA, July INITIAL ACCOMPLISHMENTS OF THE ENVIRONMENTAL 13-16, 1992 refs CONTROL AND LIFE SUPPORT SYSTEM (ECLSS) (SAE PAPER 921161) Copyright ATMOSPHERE REVITALIZATION (AR) PREDEVELOPMENT The first design concept of the Space Shuttle humidity separator OPERATIONAL SYSTEM TEST (POST) FOR THE SPACE prefilter, developed to remove debris from the air/water stream STATION FREEDOM (SSF) which flows from the cabin condensing heat exchanger to the KEVIN H. DUNN and PETER J. BULGAJEWSKI (Boeing Defense humidity separator, was flown on STS-40 in June 1991. This paper & Space Group, Huntsville, AL) Jul. 1992 14 p. SAE, discusses the design of the first prefilter (which was found not to International Conference on Environmental Systems, 22nd, Seattle, pass water at a constant rate, resulting in a tendency to slug the WA, July 13-16, 1992 refs humidity separator) and explains the on-orbit performance of the (Contract NAS8-50000) prefilter. The redesigned prefilter (made using the results of the (SAE PAPER 921186) Copyright flight test of the first prefilter) is described, with particular attention Initial results of the integrated AR POST conducted by Boeing given to the features which would allow successful reduced gravity at Marshall Space Flight Center in 1992 are presented. The three operation. AIAA baselined ECLSS Man Tended Capability AR assemblies were integrated and operated in a closed door chamber in which the A93-41344 internal atmosphere was monitored. The test provides a prerequisite DEVELOPMENT OF MEMBRANE GAS REMOVAL checkout of the AR subsystem in preparation for longer duration TECHNOLOGY FOR MICROGRAVITY LIQUID FLOW SYSTEMS tests in which the AR subsystem will be integrated with the Water ROBERT C. DALEE (McDonnell Douglas Space Systems, Recovery Management subsystem. The integrated AR POST will Huntsville, AL), JERE POTEAT, and MONTY HEYING (McDonnell serve as an early test bed to evaluate the integration of the space Douglas Missile Systems Co., Saint Louis, MO) Jul. 1992 11 p. station ECLSS AR subsystem during design maturation. AIAA SAE, International Conference on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 refs (SAE PAPER 921162) Copyright A93-41367 The possible problems associated with gas accumulation during DEVELOPMENT OF THE CARBON DIOXIDE REMOVAL long-term microgravity missions are discussed along with the SYSTEM BLOWER USED ON SPACE STATION FREEDOM expected sources of the gases, both free and dissolved. The BERNARD HAFELE (Allied-Signal Aerospace, Torrance, CA) Jul. membrane gas-removal technology considered for alleviating these 1992 9 p. SAE, International Conference on Environmental problems is examined, with particular attention given to two small, Systems, 22nd, Seattle, WA, July 13-16, 1992 Research supported light-weight hardware prototype Shell-N-Tube degassers which by Boeing Aerospace and Electronics Co currently undergo development testing with promising results. Other (SAE PAPER 921188) Copyright methods for gas removal are examined, including the use of The design and development of a blower for the carbon dioxide hydrophilic screen retention devices. AIAA removal assembly (CDRA) system are described. A mixed-flow blower was selected as the optimum design to meet the CDRA application requirements due to its low weight, small size, and A93-41345 outstanding efficiency. The blower unit is equipped with air bearings TWO PHASE FLUID MANAGEMENT FOR HYDROPONICS for extremely long life. AIAA ROBERT L CURTIS (Curtis Aerospace, Inc., Fort Worth, TX) Jul. 1992 7 p. SAE, International Conference on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 refs A93-41368 (SAE PAPER 921163) Copyright SABATIER CARBON DIOXIDE REDUCTION SYSTEM FOR In order to make hydroponics a practical solution in the SPACE STATION FREEDOM microgravity conditions, it is necessary to have a technique for ROBERT B. BOYDA, M. G. LEE, and DAVID J. GRIGGER (Life effectively separating air from water in a simple manner, since air Systems, Inc., Cleveland, OH) Jul. 1992 8 p. SAE, International bubbles in the water supply system could lead to catastrophic Conference on Environmental Systems, 22nd, Seattle, WA, July failure of the hydroponic system. This paper presents several 13-16, 1992 concepts of an efficient liquid/gas separator (LGS), with particular (SAE PAPER 921189) Copyright attention given to the design, development test, and operation of Regenerative processes for the revitalization of spacecraft a LGS in a hydroponic system for microgravity application. AIAA atmospheres are required for extended duration space missions like the Space Station Freedom. A major atmosphere revitalization A93-41346* National Aeronautics and Space Administration. function is the recovery of oxygen from metabolic carbon dioxide Lyndon B. Johnson Space Center, Houston, TX. by means of carbon dioxide reduction. The Sabatier carbon dioxide CONCEPTUAL DESIGN OF ECLSS MICROGRAVITY TEST reduction technology is the baseline technology for the Space BEDS Station Freedom for this purpose. Life Systems has performed MATT KOLODNEY (Lockheed Engineering & Sciences Co., characterization and endurance testing of Sabatier reactor Houston, TX) and LIESE DALL-BAUMAN (NASA, Johnson Space assemblies that has been used to design a prototype Sabatier Center, Houston, TX) Jul. 1992 11 p. SAE, International reactor that complies with the performance requirements of the Conference on Environmental Systems, 22nd, Seattle, WA, July Space Station Freedom Carbon Dioxide Reduction Assembly. 13-16, 1992 refs Information presented in the paper defines the testing that was (SAE PAPER 921164) Copyright used to design the prototype reactor and presents the successful Conceptual designs were prepared for Space Station Freedom test results that have been achieved using this reactor as part of ECLSS test beds for both the Air Revitalization Subsystem (ARS) an automated Sabatier-based Carbon Reduction Assembly. Reactor

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performance as a function of temperature, pressure, and reactant imposed on mass, volume, and power. Depending on the stoichiometry is defined. Author (revised) subsystem, other requirements must also be met. This paper shows the way to examine compatibility of requirements, to define an A93-41371 area of existing solutions (an operational envelope), and to find LABELS AND VISUAL CUES TO REPRODUCE AN EARTHLIKE an optimal solution. The workability of the method is shown using ENVIRONMENT IN SPACE • GOING AHEAD IN DESIGNING problems of heat load on the Plant Growth Chamber, of optimization COLUMBUS APM INTERIOR ARCHITECTURE of the Vapor-Air Membrane Separation Device, and of finding a FABIANA BOBBA, GIORGIO MUSSO, and MARCO BARIN (Alenia CTF configuration with minimum air pressure drop. Author Spazio S.p.A., Turin, Italy) Jut. 1992 9 p. SAE, International Conference on Environmental Systems, 22nd, Seattle, WA, July A93-41376 13-16, 1992 refs EUROPEAN INVOLVEMENT IN CELSS - DEFINITION OF A (SAE PAPER 921193) Copyright CLOSED ECOLOGICAL SYSTEMS TEST BED Labels and cues for the Columbus Attached Pressurized Module C. TAMPONNET (ESTEC, Noordwijk, Netherlands), M. COLASSON (APM) are analyzed in the context of the human factors. Different (Interval, Paris, France), and M. PASTOR (Nuevas Tecnologias methods for supporting crew orientation are proposed for test in Espaciales, S.A., Lissa d'Amunt, Spain) Jul. 1992 10 p. SAE, the Columbus APM habitability mock-up, where color selection International Conference on Environmental Systems, 22nd, Seattle, has been already implemented. General level suggestions on the WA, July 13-16, 1992 refs APM labelling system are presented, which include stress color (SAE PAPER 921200) Copyright coding of large elements and equipment, introduction of clear This work was to provide the ESA with technical and indications of escape routes (hatches), identification of hatches architectural guidelines for the eventual building of a Closed and their mode of aperture, continuous identification of up and Ecological System Test Bed. This work had three successive down, right and left, and the use of areas with different brightness targets. The first target has been the definition of the general level. AIAA objectives and the specific requirements for a closed ecological system test bed. It shall have the appropriate flexibility which will A93-41373 enable the users to perform separately and/or in parallel, multiple CROP INTERACTIONS IN POLYCULTURE AND THEIR tasks. Indeed, some biological life support units may also be IMPLICATIONS FOR CELSS DESIGN investigated as specific support to the currently on-going European T. STROUP and S. SCHWARTZKOPF (Lockheed Missiles & Space manned space projects. In addition, some concepts for the test Co., Inc., Sunnyvale, CA) Jul. 1992 6 p. SAE, International bed have been defined taking into account the rather contractory Conference on Environmental Systems, 22nd, Seattle, WA, July needs for a sealed structure and for structural and functional 13-16, 1992 refs flexibility. One of them has been the subject of a preliminary (SAE PAPER 921197) Copyright architectural definition which is presented with some detail. Finally, A Controlled Ecological Life Support System (CELSS) in which the important terrestrial applications of such a CES test bed have crop plants would be grown to produce food during long duration been considered. Author space missions is described. Lettuce and tomato plants were grown in a shared, recirculation nutrient solution to examine the effects A93-41377 of mutual interaction. Results show that growth of the first crop FUNCTIONS SIMULATION MODEL OF INTEGRATED of lettuce was unaffected or even slightly enhanced by growing it REGENERABLE LIFE SUPPORT SYSTEM in polyculture with tomato plants. These experiments revealed that EHDUARD A. KURMAZENKO, ALEKSANDR A. FOMICHEV there are significant plant-plant interactions in hydroponic nutrient (International Center for Advanced Studies COSMOS, Russia), and solutions. AIAA IVAN V. DOKUNIN (Nil Khimicheskogo Mashinostroeniya, Moscow, Russia) Jul. 1992 15 p. SAE, International Conference on A93-41374 Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 A TRADE STUDY METHOD FOR DETERMINING THE DESIGN refs PARAMETER OF CELSS SUBSYSTEMS (SAE PAPER 921201) Copyright KOZO SATO (Inst. for Future Technology, Tokyo, Japan), HIDEAKI Attention is given to the functions simulation model (FSM) of HAMAMI (Chiyoda Corp., Japan), AKIRA ASHIDA (Hitachi, Ltd., the manned space orbital station integrated life support system Yokohama, Japan), MIKIO SATO (Toyo Engineering Corp., Japan), (IRLSS) designed to investigate IRLSS temporary responses. It is YOSHINORI MIDORIKAWA (JGC Corp., Tokyo, Japan), and KEIJI argued that the FSM which can be used for functional analysis NITTA (National Aerospace Lab., Chofu, Japan) Jul. 1992 10 must be reflected in the structure of the orbital station's p. SAE, International Conference on Environmental Systems, ecological-technical system, including the formalistic functional 22nd, Seattle, WA, July 13-16, 1992 refs descriptions of the IRLSS subsystems and the environment links. (SAE PAPER 921198) Copyright AIAA A trade study method for determining the subsystem design parameters of Controlled Ecological Life Support System (CELSS) A93-41386* National Aeronautics and Space Administration. is presented. The trade study method is based on the break down Lyndon B. Johnson Space Center, Houston, TX. of the system configuration into material flow levels between the A SYSTEMS APPROACH TO WATER RECOVERY TESTING total closed loop life support facility and the outside environment; FOR SPACE LIFE SUPPORT - INITIAL BIOMEDICAL RESULTS between the plantation, habitat, and animal breeding modules; FROM THE ECLSS WATER RECOVERY TEST AND PLANS between each subsysten in each module; and in each subsystem. FOR TESTBED UTILIZATION AIAA LAURIE A. ATEN, WILLIAM J. CRUMP (Alabama Univ., Huntsville), and RICHARD L. SAUER (NASA, Johnson Space Center, Houston, A93-41375* National Aeronautics and Space Administration. TX) Jul. 1992 17 p. SAE, International Conference on Ames Research Center, Moffett Field, CA. Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 AN APPROACH TO THE FUNCTIONAL OPTIMIZATION OF refs THE CELSS TEST FACILITY (SAE PAPER 921210) Copyright BORIS S. YENDLER (NASA, Ames Research Center, Moffett Field, Among the challenges of designing and constructing Space CA) Jul. 1992 10 p. SAE, International Conference on Station Freedom is the development of the water system. A review Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 of past efforts in reclaiming waste water in enclosed environments Research supported by National Research Council refs reveals that there are many gaps in the biomedical understanding (SAE PAPER 921199) Copyright of this process. Some of the key uncertainties of human interaction An optimization of the CELSS Test Facility (CTF) subsystems with a closed water system include determining potential and the entire CTF is necessary in order to meet strict limitations contaminants and establishing safe levels of multiple compounds

295 54 MAN/SYSTEM TECHNOLOGY AND LIFE SUPPORT in the enclosed system of Space Station. Another uncertainty is Jul. 1992 16 p. SAE, International Conference on Environmental the microbial constituency of such a system and what impact if Systems, 22nd, Seattle, WA, July 13-16, 1992 refs could have on crew health and performance. The use of iodine (SAE PAPER 921216) Copyright as the passive biocide may have both an indirect and direct impact A dynamic model of the cabin atmosphere onboard Space on the crew. In this paper the initial results of the Water Recovery Station Freedom is presented. Hardware to regulate the pressure Test are reviewed from a biomedical perspective, revealing areas and temperature is modeled. Control laws that provide regulation where more information is needed to develop the ECLSS water of cabin pressure. Oxygen partial pressure, and temperature are system. By including the approach of 'man as a subsystem', presented. The performance of the proposed controller design consideration is given to how man interacts with the total water concept is evaluated. Author system. Taking this systems approach to providing the crew with a safe source of water gives useful insight into the most efficient design and utilization of closed system testbeds. Author A93-41401 DEW POINT ANALYSIS FOR SPACE STATION FREEDOM A93-41387* National Aeronautics and Space Administration. ROGER G. VON JOUANNE, ROBERT S. BARKER, and GLENN Marshall Space Flight Center, Huntsville, AL. A. SITLER (Boeing Defense & Space Group, Missiles & Space AQUATIC BIOFILMS AND THEIR RESPONSES TO Div., Huntsville, AL) Jul. 1992 16 p. SAE, International DISINFECTION AND INVADING SPECIES Conference on Environmental Systems, 22nd, Seattle, WA, July G. A. SMITHERS, E. B. RODGERS (NASA, Marshall Space Flight 13-16, 1992 refs Center, Huntsville, AL), D. C. OBENHUBER, and T. L HUFF (SAE PAPER 921227) Copyright (Sverdrup Technology, Inc., Huntsville, AL) Jul. 1992 11 p. G189A Environmental Control and Life Support System (ECLSS) SAE, International Conference on Environmental Systems, 22nd, dew point models for Space Station Freedom (SSF) are reviewed. Seattle, WA, July 13-16, 1992 refs The modeling of the cabin air heat exchangers, metabolic modeling (SAE PAPER 921211) Copyright of crew members, the application of latent loads, and the operation The control of microbial contamination is a primary concern in of the CO2 removal assembly are examined. Some significant the development of a water reclamation system for long-duration computed results from these models are reviewed which show manned space flights. This paper describes bench-scale transient dew point responses during maximum and minimum dew experiments, using both static and recycling water systems, point conditions on board SSF. AIAA investigating the interaction of bacterial species in the development of a biofilm and their response to the introduction of a disinfectant or of additional species. The results showed that iodine A93-41402 concentrations as high as 15 to 20 mg/l 12 are necessary to COMPARATIVE TEST DATA ASSESSMENT AND SIMPLIFIED completely disinfect a stable biofilm. When S. aueus and E. coli MATH MODELLING FOR SABATIER CO2 REDUCTION were introduced into a system containing natural mixed culture SUBSYSTEM biofilms, their colonization in the biofilms increased their survival CHANG H. SON and ROBERT S. BARKER (Boeing Defense & time, from 3 to 5 days as unattached cells to over 60 days when Space Group, Missiles & Space Div., Huntsville, AL) Jul. 1992 protected in the biofilms. While iodine concentrations of 0.5 to 1 13 p. SAE, International Conference on Environmental Systems, mg/l were enough to eliminate these organisms from the bulk 22nd, Seattle, WA, July 13-16, 1992 refs water, concentrations higher than 4.0 mg/l were necessary to (SAE PAPER 921228) Copyright completely eliminate these organisms from the biofilm. AIAA An assessment of the test data obtained from the Comparative Test of the Sabatier CO2 Reduction Subsystem of the Environmental Control and Life Support System on Space Station A93-41389* National Aeronautics and Space Administration. Freedom is reported. The assessment was achieved through Lyndon B. Johnson Space Center, Houston, TX. correlation of measured data for outlet gas constituent flow rates MICROBIOLOGY OPERATIONS AND FACILITIES ABOARD and reactor front end temperatures with corresponding computed RESTRUCTURED SPACE STATION FREEDOM data from a simplified mathematical model. The computed data LOUIS A. CIOLETTI, S. K. MISHRA (Krug Life Sciences, Inc., from the model correlates with the test data for bed temperature Houston, TX), and DUANE L. PIERSON (NASA, Johnson Space within 3 percent and gas composition data within 21 percent. Center, Houston, TX) Jul. 1992 10 p. SAE, International AIAA Conference on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 refs (SAE PAPER 921213) Copyright A93-41404 With the restructure and funding changes for Space Station SIMPLIFIED ANALYSIS OF WATER DISTRIBUTION FOR Freedom, the Environmental Health System (EHS)/Microbiology SPACE STATION FREEDOM Subsystem revised its scheduling and operational requirements EDSON A. WORDEN (Boeing Defense & Space Group, Huntsville, for component hardware. The function of the Microbiology AL) Jul. 1992 13 p. SAE, International Conference on Subsystem is to monitor the environmental quality of air, water, Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 and internal surfaces and, in part, crew health on board Space refs Station. Its critical role shall be the identification of microbial (SAE PAPER 921230) Copyright contaminants in the environment that may cause system Space Station Freedom (SSF) is required to distribute water degradation, produce unsanitary or pathogenic conditions, or for use and reprocessing. As SSF is erected, the configuration of reduce crew and mission effectiveness. EHS/Microbiology the water distribution system changes along with specific functions. operations and equipment shall be introduced in concert with a Therefore the interaction of the various components changes phased assembly sequence, from Man Tended Capability (MTC) radically. Also, these components are taken off-line intermittently through Permanently Manned Capability (PMC). Effective for maintenance (such as filter replacement). In order to analyze Microbiology operations and subsystem components will assure a these interactions, a simplified steady state computer model was safe, habitable, and useful spacecraft environment for life sciences prepared. Parameters such as set points and storage tank research and long-term manned exploration. Author capacities were revised based upon new performance understanding. The model was built using a Lotus 1-2-3 program. A93-41392 The model, making extensive use of macros, was iterated over PRESSURE, COMPOSITION, AND TEMPERATURE CONTROL thousands of hours of simulated SSF water processing in orbit. OF CABIN ATMOSPHERE ON SPACE STATION FREEDOM The data was stored and plotted. With the aid of the results of KEVIN C. MOORE, JOHN KNOX, and CRAIG STANTON (Boeing this modeling, the flight design was refined to a high level of Defense & Space Group, Missiles & Space Div., Huntsville, AL) maturity. Author

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A93-41405* National Aeronautics and Space Administration. is based on conductance microbiology which depends on the well Marshall Space Flight Center, Huntsville, AL. established ability of microorganisms to change conductance of EVALUATION OF THE CARBON DIOXIDE REMOVAL their growth media. It is concluded that this innovative technology ASSEMBLY REQUIREMENTS FOR THE SPACE STATION has potential for space applications because individual and multiple FREEDOM IN THE MANNED TENDED CAPABILITY THROUGH sensors can be integrated into a time saving system that PERMANENTLY MANNED CAPABILITY CONFIGURATIONS accommodates microgravity conditions and produced real-time J. C. KNOX (NASA, Marshall Space Flight Center, Huntsville, AL) microbial growth data using computer controlled automation. and S. D. GILLEY (Sverdrup Technology, Inc.; NASA, Marshall AIAA Space Flight Center, Huntsville, AL) Jul. 1992 22 p. SAE, International Conference on Environmental Systems, 22nd, Seattle, A93-41408 WA, July 13-16, 1992 refs WATER PURIFICATION, MICROBIOLOGICAL CONTROL, (SAE PAPER 921231) . Copyright STERILIZATION AND ORGANIC WASTE DECOMPOSITION Analyses have been conducted to assess the capability of the USING AN ELECTROCHEMICAL ADVANCED OZONATION Atmosphere Revitalization Subsystem to control ambient CO2 PROCESS levels of the Space Station Freedom (SSF). The adequacy of the TOM D. ROGERS, G. D. HITCHENS, CARLOS E. SALINAS, Carbon Dioxide Removal Assembly (CDRA) performance to meet OLIVER G. MURPHY (Lynntech, Inc., Bryan, TX), and HOWARD design requirements has been evaluated. Analyses considered W. WHITFORD (Texas Veterinary Medical Diagnostic Lab., TX) transient effects of crew location and metabolic loading on SSF Jul. 1992 11 p. SAE, International Conference on Environmental Restructure configurations. The analyses consisted of computer Systems, 22nd, Seattle, WA, July 13-16,1992 Research supported simulations of on-orbit conditions using both supplier-provided and by Small Business Innovation Research Program refs adjusted CO2 removal performance approximations along with (Contract DAMD17-91-C-1105) derived crew metabolic activities and locations. Results show that (SAE PAPER 921234) Copyright while the current performance of the CDRA will maintain CO2 Electrochemical oxidant generation has been combined with levels within specifications for Man-Tended Operations, it cannot UV photolysis to provide a highly effective means of water maintain the SSF atmosphere below specifications during purification, decomposition of bacterial organic substances, Permanently Manned Operations. Potential design options are microbiological control and sterilization. Ozone is an oxidant with discussed and other relevant analyses are summarized. many unique features that make it a valuable tool for biomedical Author (revised) applications. It is an excellent bactericidal, virucidal and sporicidal agent making it ideal for use as a sterilant. Combining 03 with A93-41406* National Aeronautics and Space Administration. UV radiation stimulates formation of hydroxyl radicals (OH) which Lyndon B. Johnson Space Center, Houston, TX. accelerates a wide range of organic oxidations. While in some MICROBIOLOGICAL CONCERNS AND METHODOLOGICAL instances maintenance of an oxidant residual is necessary, the APPROACHES RELATED TO BACTERIAL WATER QUALITY residual can be rapidly removed by UV light at the point of use IN SPACEFLIGHT (i.e., Water For Injection). Test results on pyrogen decomposition, BARRY H. PYLE and GORDON A. MCFETERS (Montana State bacterial organic decomposition, microbiological sterilization, Univ., Bozeman) Jul. 1992 7 p. SAE, International Conference residual removal and water purification as a final step for producing on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 pharmaceutical grade water are discussed. Author refs (Contract NAG9-241; NAG9-505) A93-41411 (SAE PAPER 921232) Copyright DEVELOPMENT OF THE NITROGEN FIXATION SYSTEM FOR A number of microbiological issues are of critical importance CELSS to crew health and system performance in spacecraft water M. INOUE, S. IIYAMA, T. NUMAGUCHI, K. KIKUCHI (Toyo systems. This presentation reviews an army of these concerns Engineering Corp., Japan), and K. NITTA (National Aerospace Lab., which include factors that influence water treatment and disinfection Chofu, Japan) Jul. 1992 8 p. SAE, International Conference in spaceflight such as biofilm formation and the physiological on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 responses of bacteria in clean water systems. Factors associated refs with spaceflight like aerosol formation under conditions of (SAE PAPER 921238) Copyright microgravity are also discussed within the context of airborne The practical nitrogen fixation system configuration for CELSS infections such as Legionellosis. Finally, a spectrum of analytical is described. The nitrogen fixation system encompasses approaches is reviewed to provide an evaluation of methodological subsystems for low pressure ammonia synthesis based on Ru alternatives that have been suggested or used to detect catalyst, ammonia separation, and nitric acid synthesis with Pt-Rh microorganisms of interest in water systems. These range from catalyst. Results of the ammonia synthesis tests conducted at classical approaches employing colony formation on specific 0-1.0 MPa and 573-673 K are presented. Data obtained microbiological growth media to direct (i.e. microscopic) and indirect demonstrates the feasibility of the proposed nitrogen fixation (e.g. electrochemical) methods as well as the use of molecular process for CELSS. AIAA approaches and gene probes. These techniques are critically evaluated for their potential utility in determining microbiological A93-41412 water quality through the detection of microorganisms under the CONCEPT OF WASTE TRANSFERRING MECHANISMS influence of ambient environmental stress inherent in spaceflight -ATSUSHI SHIRAISHI (Fujitsu, Ltd., Tokyo, Japan) and KEIJI NITTA water systems. Author (revised) (National Aerospace Lab., Chofu, Japan) Jul. 1992 10 p. SAE, International Conference on Environmental Systems, 22nd, A93-41407 Seattle, WA, July 13-16, 1992 refs INSTRUMENTATION FOR MICROBIAL MONITORING OF (SAE PAPER 921239) Copyright DECONTAMINATION OR BIOCIDE SYSTEM EFFECTIVENESS Recycling human and animal excreta is an important part of GORDON SNYDER (Gordon Snyder & Consultants, Inc., Seattle, the proposed Closed Ecology Experiment Facility (CEEF) in Japan. WA) and JARROD D. O'LEARY (Perkin-Elmer Corp., Pomona, This paper introduces a conceptual design for the waste collection CA) Jul. 1992 10 p. SAE, International Conference on and transfer system. Mineral-rich wastes such as urine and wool Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 grease must be separated from other wastes to recover the rels minerals. Solids and liquids also require separate handling methods. (SAE PAPER 921233) Copyright Our design uses inclined conveyer belts to separate feces and A Viable Microbial Monitor (VMM) for detection and enumeration urine. A fluorocarbon polymer coating prevents wastes from sticking of viable microorganisms is presented. The VMM, an instrument to the belt. In-line freezers are used to solidify liquid wastes and system for the rapid detection of bacterial or fungal contamination, retard premature decomposition. A summary of available data on

297 54 MAN/SYSTEM TECHNOLOGY AND LIFE SUPPORT animal excreta is included, but there is a distinct shortage of A93-41420 useful information. This data is insignificant for usual biology or CREW HEALTH CARE SYSTEMS INSTALLATIONS FOR animal husbandry, but is essential for designing the self-contained SPACE STATION FREEDOM environment. Author PETE GADSBY, FRANK EICHSTADT, and ED CORDES (McDonnell Douglas Space Systems, Space Station Div., Huntington Beach, CA) Jul. 1992 9 p. SAE, International A93-41413* National Aeronautics and Space Administration. John Conference on Environmental Systems, 22nd, Seattle, WA, July F. Kennedy Space Center, Cocoa Beach, FL. 13-16, 1992 OCAM - A CELSS MODELING TOOL: DESCRIPTION AND (SAE PAPER 921249) Copyright RESULTS This paper presents an overview of the design and development ALAN DRYSDALE, MARK THOMAS, MARK FRESA (McDonnell of Crew Health Care Systems (CHeCS) for Space Station Freedom Douglas Space Systems Co., Cocoa Beach, FL), and RAY with an emphasis on physical installation and flight crew suitability. WHEELER (NASA, Kennedy Space Center, Cocoa Beach, FL) Particular emphasis is directed at unique aspects of the system Jul. 1992 12 p. SAE, International Conference on Environmental which are driven by environmental peculiarities such as limited Systems, 22nd, Seattle, WA, July 13-16, 1992 refs volume and resources (electrical power, heat rejection, crew time, (SAE PAPER 921241) Copyright launch constraints), location remoteness, isolation, and Controlled Ecological Life Support System (CELSS) technology microgravity, while minimizing detriment to other nonrelated Space is critical to the Space Exploration Initiative. NASA's Kennedy Station operations. Design implications resulting from phased Space Center has been performing CELSS research for several Space Station build-up are also described. General and specific years, developing data related to CELSS design. We have topics involve selected component and installations designs, developed OCAM (Object-oriented CELSS Analysis and Modeling), development testing and simulation activities, and system design a CELSS modeling tool, and have used this tool to evaluate CELSS integration into Space Station elements. Implications introduced concepts, using this data. In using OCAM, a CELSS is broken by CHeCS relationships to the Space Transportation System are down into components, and each component is modeled as a also presented. Author (revised) combination of containers, converters, and gates which store, process, and exchange carbon, hydrogen, and oxygen on a daily A93-41423* National Aeronautics and Space Administration, basis. Multiple crops and plant types can be simulated. Resource Washington, DC. recovery options modeled include combustion, leaching, enzyme A FEASIBILITY STUDY OF HAND KINEMATICS FOR EVA treatment, aerobic or anaerobic digestion, and mushroom and fish ANALYSIS USING MAGNETIC RESONANCE IMAGING growth. Results include printouts and time-history graphs of total REUBEN D. DICKENSON (Vanderbilt Univ., Nashville, TN), system mass, biomass, carbon dioxide, and oxygen quantities; CHRISTINE H. LORENZ (Vanderbilt Medical Center, Nashville, TN), energy consumption; and manpower requirements. The STEVEN W. PETERSON, ALVIN M. STRAUSS, and JOHN A. MAIN contributions of mass, energy, and manpower to system cost have (Vanderbilt Univ., Nashville, TN) Jul. 1992 11 p. SAE, been analyzed to compare configurations and determine International Conference on Environmental Systems, 22nd, Seattle, appropriate research directions. Author (revised) WA, July 13-16, 1992 Research supported by NASA refs (SAE PAPER 921253) Copyright A93-41418 A new method for analyzing the kinematics of joint motion using magnetic resonance imaging (MRI) is described. The THE EFFECTS OF A REDUCED PRESSURE SCENARIO ON reconstruction of the metacarpalphalangeal joint of the left index THE COLUMBUS APM ENVIRONMENTAL CONTROL SYSTEM EUGENIO GARGIOLI and CESARE LOBASCIO (Alenia Spazio finger into a 3D graphic display is shown. From the reconstructed volumetric images, measurements of the angles of movement of S.p.A., Turin, Italy) Jul. 1992 11 p. SAE, International Conference on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 the applicable bones are obtained and processed by analyzing refs the screw motion of the joint. Landmark positions are chosen at (SAE PAPER 921247) Copyright distinctive locations of the joint at fixed image threshold intensity levels to ensure repeatability. The primarily 2D planar motion of The results are reported of a study to identify the contraints this joint is then studied using a method of constructing coordinate and problems in the Columbus APM operations at reduced pressure. The effects of reduced pressure on the Environmental systems using three or more points. A transformation matrix based on a world coordinate system describes the location and orientation Control System are considered as regards avionics air cooling, ventilation requirements and crew comfort, and subfloor cooling. of the local target coordinate system. The findings show the applicability of MRI to joint kinematics for gaining further knowledge The impact on components and materials is addressed, including heat exchanger performances, humidity removal, fan performance, of the hand-glove design for EVA. AIAA flammability, and the selection of materials. AIAA A93-41424* National Aeronautics and Space Administration. Marshall Space Flight Center, Huntsville, AL. A93-41419* National Aeronautics and Space Administration. DEVELOPMENT OF A TEST PROTOCOL FOR EVALUATING Lyndon B. Johnson Space Center, Houston, TX. EVA GLOVE PERFORMANCE SPACE STATION FREEDOM FOOD MANAGEMENT ELAINE M. HINMAN (NASA, Marshall Space Flight Center, TROY N. WHITEHURST, JR. (Boeing Defense & Space Group, Huntsville, AL) Jul. 1992 20 p. SAE, International Conference Seattle, WA) and CHARLES T. BOURLAND (NASA, Johnson Space on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 Center, Houston, TX) Jul. 1992 7 p. SAE, International refs Conference on Environmental Systems, 22nd, Seattle, WA, July (SAE PAPER 921254) Copyright 13-16, 1992 refs Testing gloved hand performance involves work from several (SAE PAPER 921248) Copyright disciplines. Evaluations performed in the course of reenabling a This paper summarizes the specification requirements for the disabled hand, designing a robotic end effector or master controller, Space Station Food System, and describes the system that is or hard-suit design have all yielded relevant information, and, in being designed and developed to meet those requirements. Space most cases, produced performance test methods. Most times, these Station Freedom will provide a mix of frozen, refrigerated, test methods have been primarily oriented toward their parent rehydratable, and shelf stable foods. The crew will pre-select discipline. For space operations, a comparative test which would preferred foods from an approved list, to the extent that proper provide a way to quantify pressure glove and end effector nutrition balance is maintained. A galley with freezers, refrigerators, performance would be useful in dividing tasks between humans trash compactor, and combination microwave and convection and robots. Such a test would have to rely heavily on sensored ovens will improve crew efficiency and productivity during the long measurement, as opposed to questionnaires, to produce relevant Space Station Freedom (SSF) missions. Author data. However, at some point human preference would have to

298 54 MAN/SYSTEM TECHNOLOGY AND LIFE SUPPORT be taken into account. This paper presents a methodology for Houston, TX) Jul. 1992 14 p. SAE, International Conference evaluating gloved hand performance which attempts to respond on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 to these issues. Glove testing of a prototype glove design using refs this method is described. Author (revised) (SAE PAPER 921258) Copyright A lightweight, flexible thermal micrometeoroid garment (TMG) A93-41425* National Aeronautics and Space Administration, design for enhanced space suit micrometeoroid/debris (M/D) Washington, DC. protection is described. It will consist of an outer layer comprised POWER ASSIST EVA GLOVE DEVELOPMENT of orthofabric, multilayers of aluminized Mylar, and a layer of silicone JOHN A. MAIN, STEVEN W. PETERSON, and ALVIN M. STRAUSS rubber loaded with micron sized particles of tungsten. The shield (Vanderbilt Univ., Nashville, TN) Jul. 1992 17 p. SAE, layers would fragment and/or vaporize the M/D projectile while International Conference on Environmental Systems, 22nd, Seattle, the backup sheet would stop the resultant debris cloud. AIAA WA, July 13-16, 1992 Research supported by NASA refs (SAE PAPER 921255) Copyright The design of the EVA glove is examined, emphasizing the A93-41431 development of a more flexible metacarpophalangeal (MCP) joint SYSTEM INTEGRATION AND VERIFICATION APPROACH FOR for the EVA glove. The analysis of the EVA glove MCP joint is THE ENVIRONMENTAL CONTROL SYSTEM OF THE reviewed and the glove design process is recapitulated. COLUMBUS ATTACHED PRESSURISED MODULE Experimental tests of the glove are summarized. AIAA MASSIMO BRAGHIN and RUGGERO VENERI (Alenia Spazio S.p.A., Turin, Italy) Jul. 1992 9 p. SAE, International Conference A93-41426 on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 DEVELOPMENT OF THE HERMES EVA SPACE SUIT GLOVE (SAE PAPER 921261) Copyright DAVID A. NICE (Aerazur, Issy-les-Moulineaux, France), A test approach selected for the functional and performance JEAN-LOUIS THONNARD, and LEON PLAGHKI (Louvain, Univ. verification of the Environmental Control System (ECS) of the Catholique, Louvain-la-Neuve, Belgium) Jul. 1992 23 p. SAE, Attached Pressurized Module (APM) is described. While the ECLSS International Conference on Environmental Systems, 22nd, Seattle, is tested as an integrated subsystem by using load simulators WA, July 13-16, 1992 Research supported by ESA and Dassault and a boiler plate, the thermal control subsystem is tested as an Aviation refs integrated engineering model subsystem only after APM EM (SAE PAPER 921256) Copyright integration completion. AIAA The development phase of the Hermes EVA (Extra Vehicular Activity) Space Suit Glove began with a review of EVA Glove literature and a parallel study of hand biomechanics. The glove A93-41434 had three principal layers; Bladder, Restraint and Thermal PROCESS CONTROL WATER QUALITY MONITOR FOR Micrometeoroid Protection, (TMP). Range of motion, strength, SPACE STATION FREEDOM • DEVELOPMENT UPDATE tactile perception, dexterity, fatigue and comfort were assessed E. L. JEFFERS and J. NOVOTNY (Astro International Corp., through the test program. The testing revealed a decrease in Houston, TX) Jul. 1992 23 p. SAE, International Conference performance. Thermal contact testing was performed with the glove on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 interfaced to a U.S. Shuttle EMU (Extravehicular Mobility Unit). Research supported by Boeing Defense and Space Group refs Further evaluation was performed with the glove interfaced to a (SAE PAPER 921264) Copyright Soviet Orlan DMA suit. The testing identified a number of glove The monitoring system being designed for the Space Station improvements. Author Freedom's water reclamation system (called the Process Control Water Quality Monitor, PCWQM) is an untended continuous process A93-41427 water quality monitor which measures conductivity, pH, total organic DEVELOPMENT OF A 500 HPA SHOULDER JOINT FOR THE carbon (TOC), temperature, and the residual iodine biocide EUROPEAN EVA SPACE SUIT SYSTEM concentration in the effluent. This paper describes the PCWQM Y. OLLIVIER, X. LABOURDETTE (Dassault Aviation, St.-Cloud, system, the measurement methodology used, and the solid phase France), M. DIENER (Dornier GmbH, Friedrichshafen, Germany), calibration standards. A development test unit containing all major and V. MENENDEZ (Zodiac Espanola, S.A., Figueras, Spain) Jul. PCWQM components began integrated testing in May 1992. The 1992 13 p. SAE, International Conference on Environmental testing evaluates functional compatibility, materials compatibility, Systems, 22nd, Seattle, WA, July 13-16,1992 Research supported and prototype sensor performance. Results of these evaluations by ESA refs are presented. AIAA (SAE PAPER 921257) Copyright This paper synthesizes the shoulder joint development activities performed in the framework of the European EVA Space Suit A93-41435 System program. The shoulder joint belongs to the CONTINUOUS MONITORING OF EFFLUENT IODINE LEVELS anthropomorphic enclosure encompassing the crewmember, OF SPACE STATION WATER USING SOLID STATE protecting him against the space environment while ensuring him TECHNOLOGY adequate mobility, dexterity, and visibility. A conceptual trade-off DALE R. DOUGHERTY, JOHN NOVOTNY, E. L. JEFFERS (Astro selected two candidates likely to fulfill the stringent shoulder joint International Corp., Houston, TX), and TOM POORMAN Jul. requirements: an all-soft joint and a hybrid 'rolling convolute'. 1992 11 p. SAE, International Conference on Environmental Representative pressurized breadboards were designed, Systems, 22nd, Seattle, WA, July 13-16, 1992 refs manufactured, and tested. The tests addressed both intrinsic (SAE PAPER 921265) Copyright performance, via torque/flexion hysteresis curves, and ergonomic Space Station Freedom's potable water recycling system will characteristics, via a 'man in the loop' evaluation, involving a suit use iodine biocide. A process control water quality monitor will demonstrator. Tests results completed the trade-off, thus enabling continually measure potable water parameters, including the 2.0 the industrial team to formulate recommendations and propose to 6.0 mg/l iodine concentration range. The iodine sensor will be further development studies. Author (revised) a photometric flow cell that measures iodine's 465 nm radiative absorption band and reports iodine concentration. The expanded A93-41428* National Aeronautics and Space Administration. ECLSS Preliminary Operational System Test included prototype Lyndon B. Johnson Space Center, Houston, TX. iodine sensors. A solid state iodine sensor will meet power, weight, ENHANCED SOFTGOODS STRUCTURES FOR SPACESUIT reliability, and maintainability requirements associated with the MICROMETEOROID/DEBRIS PROTECTIVE SYSTEMS station's redesign. This paper discusses solid state photometric BRIAN REMINGTON, DAVID CADOGAN (ILC Dover, Frederica, iodine measurement theory and engineering considerations and DE), and JOSEPH KOSMO (NASA, Johnson Space Center, presents preliminary LED-based sensor test results. Author

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A93-41436* National Aeronautics and Space Administration. optimized. This paper reports the status of a study to evaluate Lyndon B. Johnson Space Center, Houston, TX. CE's capability with regard to inorganic and carboxylate anions, THE DEVELOPMENT AND TESTING OF A VOLATILE alkali and alkaline earth cations, and transition metal cations. ORGANICS CONCENTRATOR FOR USE IN MONITORING Preliminary results indicate that CE has an impressive selectivity SPACE STATION WATER QUALITY and trace sensitivity, although considerable methods development ITAMAR BODEK, DANIEL J. EHNTHOLT, THOMAS J. STOLKI remains to be performed. Author (Arthur D. Little, Inc., Cambridge, MA), RUDY TRABANINO, LLOYD HINSDALE, JOHANNA WEBB (McDonnell Douglas Space Systems, A93-41439* National Aeronautics and Space Administration. Huntington Beach, CA), and RICHARD L. SAUER (NASA, Johnson Marshall Space Flight Center, Huntsville, AL. Space Center, Houston, TX) Jul. 1992 10 p. SAE, International THE ANALYTICAL CONTROL PROGRAM FOR THE NASA Conference on Environmental Systems, 22nd, Seattle, WA, July SPACE STATION FREEDOM ENVIRONMENTAL CONTROL 13-16, 1992 refs AND LIFE SUPPORT SYSTEM (ECLSS) WATER RECOVERY (SAE PAPER 921266) Copyright TEST The Volatile Organics Concentrator (VOC) system, designed to JAMES D. TATARA and SILVIA MINTON (ION Electronics, attach to a gas chromatograph/mass spectrometer (GC/MS) for Huntsville, AL) Jul. 1992 14 p. SAE, International Conference the analyses of volatile organic compounds in water on Space on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 Station Freedom, is described. Organic volatiles are collected and Research supported by NASA refs concentrated in the VOC by means of two primary solid sorbent (SAE PAPER 921269) Copyright tubes and desorbed into the GC/MS system. The paper describes NASA-Marshall has striven to maximize quality assurance and the results of testing the VOC breadboard using a GC/MS system. quality control measures in the course of Water Recovery Test Evaluations performed on 39 organic compounds recovered from (WRT) development for the Space Station Freedom ECLSS. The water samples were compared with data for these compounds WRT was subjected to an independent analytical control program using direct injection/GC/MS and purge and trap/GC/MS that is governed by the Analytical Control Test Plan and the procedures. The results demonstrate that the VOC/GC/MS Microbiological Methods for Water Recovery Testing Plan. Attention system's detection limits for the 39 compounds analyzed are is given to analysis results for volatiles, sodium, and conductivity. comparable to those of the EPA Method 524.2, and for many AIAA compounds reaching a factor of 5 lower. AIAA A93-41440 A93-41437 THE APPLICATION OF FILTRATION TECHNOLOGY WITHIN MEASUREMENT OF FREE AND DISSOLVED GAS CONTENT THE WATER PROCESSOR ON BOARD SPACE STATION OF WATER SAMPLES ON SPACE STATION FREEDOM FREEDOM RANDOLPH W. SCHWEICKART (McDonnell Douglas Space PAUL I. KEYSER, GLENN W. HOWARD, JR. (Pall Corp., Glen Systems, Huntington Beach, CA) and DAMON C. SMITH (Lockheed Cove, NY), JOHN W. STEELE, and ROBERT W. MARSH (Hamilton Missiles and Space Co., Inc., Sunnyvale, CA) Jul. 1992 10 p. Standard, Windsor Locks, CT) Jul. 1992 9 p. SAE, International SAE, International Conference on Environmental Systems, 22nd, Conference on Environmental Systems, 22nd, Seattle, WA, July Seattle, WA, July 13-16, 1992 refs 13-16, 1992 refs (SAE PAPER 921267) Copyright (SAE PAPER 921270) Copyright A linear displacement aerometer has been developed for the Space Station Freedom uses a semi-closed loop recirculating measurement of the volume percent of free and dissolved gas in waste water system to regenerate potable water. A specific series water samples. This paper discusses the design and testing of of depth and membrane filters can be employed prior to the waste the prototype linear displacement aerometer that was incorporated water holding tank to eliminate bacteria at the earliest portion of into the Optical Water Quality Analyzer (OWQA) breadboard, an the Water Processor. Several advantages accrue by using a cold instrument that is being developed to monitor the quality of water sterilizing method for microbial control. This methodology i) reduces samples on Space Station Freedom. Consumption of liquids the weight and power requirements needed for a heat sterilizer containing excessive amounts of free or dissolved gas in and exchanger, and ii) significantly reduces biocorrosion and biofilm microgravity can potentially cause gastrointestinal discomfort. The associated problems. A series of six filters and a two component OWQA aerometer will determine the free and dissolved gas resin bed was used to process a mixture of laundry water, shower contents of water samples from the Space Station processed water water, and urine distillate in a ratio of 63:28:9 by volume. The distribution system so that potential health impacts may be final effluent was free of bacteria when grown on R2A agar. assessed prior to consumption. Author Gravimetric analysis was performed on 100 ml of downstream effluent from four filters and compared to the raw water. The A93-41438* National Aeronautics and Space Administration. proposed filtration scheme throughout the entire Water Processor Lyndon B. Johnson Space Center, Houston, TX. will contain eleven filters including a final filter sized at 0.04 micron EVALUATION OF CAPILLARY ELECTROPHORESIS FOR absolute. Author IN-FLIGHT IONIC CONTAMINANT MONITORING OF SSF POTABLE WATER A93-41441* National Aeronautics and Space Administration. PAUL D. MUDGETT, JOHN R. SCHULTZ (Krug Life Sciences, Lyndon B. Johnson Space Center, Houston, TX. Houston, TX), and RICHARD L. SAUER (NASA, Johnson Space AN ASSESSMENT OF WASTE PROCESSING/RESOURCE Center, Houston, TX) Jul. 1992 12 p. SAE, International RECOVERY TECHNOLOGIES FOR LUNAR/MARS LIFE Conference on Environmental Systems, 22nd, Seattle, WA, July APPLICATIONS 13-16, 1992 refs CHARLES E. VEROSTKO (NASA, Johnson Space Center, Houston, (SAE PAPER 921268) Copyright TX), NIGEL J. C. PACKHAM (Lockheed Engineering and Sciences Until 1989, ion chromatography (1C) was the baseline technology Co., Houston, TX), and DONALD H. HENNINGER (NASA, Johnson selected for the Specific Ion Analyzer, an in-flight inorganic water Space Center, Houston, TX) Jul. 1992 15 p. SAE, International quality monitor being designed for Space Station Freedom. Recent Conference on Environmental Systems, 22nd, Seattle, WA, July developments in capillary electrophoresis (CE) may offer significant 13-16, 1992 refs savings of consumables, power consumption, and weight/volume (SAE PAPER 921271) Copyright allocation, relative to 1C technology. A thorough evaluation of CE's NASA's future manned missions to explore the solar system analytical capability, however, is necessary before one of the two are by nature of long duration, mandating extensive regeneration techniques is chosen. Unfortunately, analytical methods currently of life support consumables from wastes generated in space-based available for inorganic CE are unproven for NASA's target list of habitats. Long-duration exploration missions would otherwise be anions and cations. Thus, CE electrolyte chemistry and methods prohibitive due to the number and frequency of energy-intensive to measure the target contaminants must be first identified and resupply missions from Earth. Resource recovery is therefore a

300 54 MAN/SYSTEM TECHNOLOGY AND LIFE SUPPORT critical component of the controlled ecological life support system A93-41444* National Aeronautics and Space Administration. (CELSS). In order to assess resource recovery technologies for Lyndon B. Johnson Space Center, Houston, TX. CELSS applications, the Crew and Thermal Systems Division at POST-TREATMENT OF RECLAIMED WASTE WATER BASED NASA-Johnson Space Center convened a three-day workshop to ON AN ELECTROCHEMICAL ADVANCED OXIDATION assess potential resource recovery technologies for application in PROCESS a space-based CELSS. This paper describes the methodology of CHARLES E. VEROSTKO (NASA, Johnson Space Center, Houston, assessing and ranking of these technologies. Recommendations TX), OLIVER J. MURPHY, G. D. HITCHENS, CARLOS E. SALINAS, and issues are identified. Evaluations focused on the processes and TOM D. ROGERS (Lynntech, Inc., Bryan, TX) Jul. 1992 for handling and treatment of inedible plant biomass, human waste, 13 p. SAE, International Conference on Environmental Systems, and human generated trash. Technologies were assessed on the 22nd, Seattle, WA, July 13-16, 1992 refs basis of safety, reliability, technology readiness, and performance (SAE PAPER 921275) Copyright characteristics. Author (revised) The purification of reclaimed water is essential to water reclamation technology life-support systems in lunar/Mars habitats. An electrochemical UV reactor is being developed which generates oxidants, operates at low temperatures, and requires no chemical expendables. The reactor is the basis for an advanced oxidation A93-41442 process in which electrochemically generated ozone and hydrogen ANAEROBIC TREATMENT OF ORGANIC WASTES FROM peroxide are used in combination with ultraviolet light irradiation CONTROLLED ECOLOGICAL LIFE SUPPORT SYSTEMS to produce hydroxyl radicals. Results from this process are DOUGLAS W. WILLIAMS, ROBERT KULL (California Polytechnic presented which demonstrate concept feasibility for removal of State Univ., San Luis Obispo), and STEVEN H. SCHWARTZKOPF organic impurities and disinfection of water for potable and hygiene (Lockheed Missiles and Space Co., Inc., Sunnyvale, CA) Jul. reuse. Power, size requirements, Faradaic efficiency, and process 1992 11 p. SAE, International Conference on Environmental reaction kinetics are discussed. At the completion of this Systems, 22nd, Seattle, WA, July 13-16,1992 Research supported development effort the reactor system will be installed in JSC's by Lockheed Missiles and Space Co., Inc refs regenerative water recovery test facility for evaluation to compare (SAE PAPER 921272) Copyright this technique with other candidate processes. Author (revised) This paper describes the results of a project involving an anaerobic digestion system used in treating the human and A93-41445* National Aeronautics and Space Administration. vegetative wastes from a Controlled Ecological Life Support System Lyndon B. Johnson Space Center, Houston, TX. (CELSS). The anaerobic digester biologically breaks down the A HYBRID REGENERATIVE WATER RECOVERY SYSTEM FOR organic matter in the wastes into a mixture of methane gas and LUNAR/MARS LIFE SUPPORT APPLICATIONS carbon dioxide, while significantly reducing the BOD (biological CHARLES E. VEROSTKO, MARYBETH A. EDEEN (NASA, Johnson oxygen demand) of the wastewater. A standard waste was Space Center, Houston, TX), and NIGEL J. C. PACKHAM formulated consisting of a mixture of swine waste (the surrogate (Lockheed Engineering and Sciences Co., Houston, TX) Jul. for human feces and urine), green wastes (primarily lettuce), and 1992 10 p. SAE, International Conference on Environmental paper wastes. The equipment used for this project was a 2.7 Systems, 22nd, Seattle, WA, July 13-16, 1992 refs cubic meter digester tank filled with plastic media and heated to (SAE PAPER 921276) Copyright an average temperature of 35 C. The digester was run over period Long-duration manned space missions will require integrated of 200 days and loaded on the average of five days per week. biological and physicochemical processes for recovery of resources The results over this test period showed a 94 percent reduction from wastes. This paper discusses a hybrid regenerative biological in BOD and a 98 percent reduction in suspended solids in the and physicochemical water recovery system designed and built at wastewater. Biogas production was approximately 1 cubic meter NASA's Crew and Thermal Systems Division at Johnson Space of biogas per kg of BOD added to the digester per day. This Center. The system is sized for a four-person crew and consists biogas contained an average of 62 percent methane. of a two-stage, aerobic, trickling filter bioreactor; a reverse osmosis Author (revised) system; and a photocatalytic oxidation system. The system was designed to accommodate high organic and inorganic loadings and a low hydraulic loading. The bioreactor was designed to oxidize organics to carbon dioxide and water; the reverse osmosis system A93-41443* National Aeronautics and Space Administration. reduces inorganic content to potable quality; and the photocatalytic Marshall Space Flight Center, Huntsville, AL. oxidation unit removes residual organic impurities (part per million CATALYTIC OXIDATION FOR TREATMENT OF ECLSS AND range) and provides in situ disinfection. The design and PMMS WASTE STREAMS performance of the hybrid system for producing potable/hygiene JAMES R. AKSE, JOHN THOMPSON, BRYAN SCOTT, CLIFFORD water is described. Aspects of the system such as closure, JOLLY (Umpqua Research Co., Myrtle Creek, OR), and DONALD automation and integration are discussed and preliminary results L. CARTER (NASA, Marshall Space Flight Center, Huntsville, AL) presented. Author (revised) Jul. 1992 18 p. SAE, International Conference on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 refs A93-41446 (Contract NAS8-38038; NAS8-38490) IMMOBILIZED CELL BIOREACTORS FOR WATER (SAE PAPER 921274) Copyright RECLAMATION - PROCESS STABILITY AND EFFECT OF Catalytic oxidation was added to the baseline multifiltration REACTOR DESIGN technology for use on the Space Station Freedom in order to GLENN E. PETRIE, BERIT G. DISMER, EDWARD F. ZINGER convert low-molecular weight organic waste components such as (Allied-Signal Research and Technology, Des Plaines, IL), and alcohols, aldehydes, ketones, amides, and thiocarbamides to CO2 MAURENA S. NACHEFF-BENEDICT (Allied-Signal Aerospace, at low temperature (121 C), thereby reducing the total organic Torrance, CA) Jul. 1992 12 p. SAE, International Conference carbon (TOG) to below 500 ppb. The rate of reaction for the on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 catalytic oxidation of aqueous organics to CO2 and water depends Research supported by Allied-Signal Aerospace and Allied-Signal primarily upon the catalyst, temperature, and concentration of Engineered Materials refs reactants. This paper describes a kinetic study conducted to (SAE PAPER 921277) Copyright determine the impact of each of these parameters upon the reaction Immobilized cell bioreactor (ICB) technology is being rate. The results indicate that a classic kinetic model, the investigated under a multiyear, company-funded program to Langmuir-Hinshelwood rate equation for heterogeneous catalysis, evaluate its applicability as a primary water processor for treatment can accurately represent the functional dependencies of this rate. of wastewater streams in a regenerative life support system (RLSS). AIAA Two aspects of the ongoing ICB research are described: (1)

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performance stability over an extended time period, and (2) new Support System (CELLS) to be built on the lunar surface or just reactor designs. Two packed-bed bioreactors were operated over beneath it: the ionizing radiation and the danger of meteoroid 7 months at a hydraulic retention time (HRT) of 24 hours and penetration. The analysis defines the degree of risk associated exhibited consistent performance throughout this period in terms with each hazard, specifically with regard to the feasibility of using of total organic carbon degradation, urea degradation, and solids an inflatable surface structure for CELLS application. It is shown production. However, it is desirable to lower the required HRT, by that chronic exposure to galactic cosmic rays does not present a increasing the overall processing rate, in order to minimize size hindrance to the concept of constructing a plant growth subsystem and weight of an ICB for a life support system. Two alternate on the surface of the moon. However, the analysis indicated that, scale bioreactor designs were investigated and their effect on the even for a small plant growth system such as that anticipated for HRT determined. A greater than fourfold decrease in HRT a four-person crew, there is at least a 1 percent chance of a compared with previous bioreactors is reported. Author (revised) small meteoroid strike. AIAA

A93-41449 A93-41452* National Aeronautics and Space Administration. John ENVIRONMENTAL CONTROL OF THE MINI PRESSURIZED F. Kennedy Space Center, Cocoa Beach, FL. LOGISTIC MODULE ADVANCED LIFE SUPPORT SYSTEMS IN LUNAR AND CESARE LOBASCIO, ANGELO DENARO, and RENATO D'AURIA MARTIAN ENVIRONMENTS UTILIZING A HIGHER PLANT (Alenia Spazio S.p.A., Turin, Italy) Jul. 1992 14 p. SAE, BASED ENGINEERING PARADIGM International Conference on Environmental Systems, 22nd, Seattle, DENNIS CHAMBERLAND (NASA, Kennedy Space Center, Cocoa WA, July 13-16, 1992 Beach, FL) Jul. 1992 11 p. SAE, International Conference on (SAE PAPER 921281) Copyright Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 The Mini Pressurized Logistic Module (MPLM)is designed to refs transport supplies and return cargo requiring a pressurized (SAE PAPER 921286) Copyright environment to and from the Space Station Freedom (SSF) via The paper describes a higher-plant-based engineering paradigm the National Space Transportation System (NSTS) Shuttle. The for advanced life support in a Controlled Ecological Life Support MPLM provides accommodation for a number of cargo racks, System (CELSS) on the surface of the moon or Mars, called the including two Freezer/Refrigerators (F/Rs) and one subsystem CELSS Breadboard Project, designed at John F. Kennedy Space rack. The maintenance of the habitable conditions for the crew Center. Such a higher-plant-based system would use the plants and the control of the MPLM thermal environment are carried out for a direct food source, gas exchange, water reclamation, and by the Environmental Control and Life Support System (ECLSS) plant residuals in a complex biological resource recovery scheme. and the Thermal Control System (TCS). The ECLSS and TCS The CELSS Breadboard Project utilizes a 'breadboard' approach functional concepts are tailored to the peculiarities of the MPLM of developing independent systems that are evaluated design, based on mass and volume minimization, maximum autonomously and are later interconnected. Such a scheme will simplification, and exploitation of the resources available at the enable evaluation of life support system methodologies tested for SSF interface. This paper provides an overview of the ECLSS their efficiency in a life support system for habitats on the moon and TCS design features and components, describing the results or Mars. AIAA of the main tradeoffs performed by Alenia Spazio in the definition phase of the Phase B MPLM baseline (Mid-Term Review). A93-41453* National Aeronautics and Space Administration. Author (revised) Ames Research Center, Moffett Field, CA. CONSUMABLES AND WASTES ESTIMATIONS FOR THE A93-41450 FIRST LUNAR OUTPOST EFFECTS OF AIR BUBBLE CONTAMINATION IN RONALD L. A. THEIS, MARK G. BALLIN (NASA, Ames Research RECIRCULATING WATER LOOP Center, Moffett Field, CA), and MARTHA F. EVERT (Lockheed ROBERTO ORLANDO and MARINO FERRARA (Microtecnica Engineering & Sciences Co., Houston, TX) Jul. 1992 12 p. S.p.A., Turin, Italy) Jul. 1992 8 p. SAE, International Conference SAE, International Conference on Environmental Systems, 22nd, on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 Seattle, WA, July 13-16, 1992 refs (SAE PAPER 921282) Copyright (SAE PAPER 921287) Copyright Long life in space of the Columbus recirculating water transport The First Lunar Outpost mission is a design reference mission loop indicates probability that air bubble contamination will for the first human return to the moon. This paper describes a inadvertently be added to the loop during service revision, or repair set of consumables and waste material estimations made on the procedures. This paper describes the results of tests run to simulate basis of the First Lunar Outpost mission scenario developed by the effects of bubble contamination on the operation in zero gravity the NASA Exploration Programs Office. The study includes the of a recirculating water loop. All major components of the loop definition of a functional interface framework and a top-level set were installed with their water inlet and outlet connections at the of consumables and waste materials to be evaluated, the top to prevent bubbles from being separated and stored in the compilation of mass flow information from mission developers components. In this way the bubbles were encouraged to recirculate supplemented with information from the literature, and the analysis in the loop in the manner expected in space with zero g operation. of the resulting mass flow information to gain insight about the Maximum air injection without adverse pump operation was possibility of material flow integration between the moon outpost determined. A brief trade-off of prospective bubble trap concepts elements. The results of the study of the details of the piloted is presented, and a preliminary investigation of a hydrophobic mission and the habitat are used to identify areas where integration membrane bubble separator for this application is discussed. of consumables and wastes across different mission elements Author could provide possible launch mass savings. AIAA

A93-41451 A93-41463* National Aeronautics and Space Administration. HAZARD AND RISK ASSESSMENT FOR SURFACE Lyndon B. Johnson Space Center, Houston, TX. COMPONENTS OF A LUNAR BASE CONTROLLED DEVELOPMENT OF A REGENERABLE METAL OXIDE SHEET ECOLOGICAL LIFE SUPPORT SYSTEM MATRIX CO2 REMOVAL SYSTEM S. SCHWART2KOPF (Lockheed Missiles and Space Co., Inc., TIMOTHY A. NALETTE, THOMAS P. FILBUM (Hamilton Standard, Sunnyvale, CA) Jul. 1992 11 p. SAE, International Conference Windsor Locks, CT), and ROBERT J. CUSICK (NASA, Johnson on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 Space Center, Houston, TX) Jul. 1992 8 p. SAE, International refs Conference on Environmental Systems, 22nd, Seattle, WA, July (SAE PAPER 921285) Copyright 13-16, 1992 Results are presented of an analysis of the two greatest (Contract NAS9-17822) potential hazards for the lunar-base Controlled Ecological Life (SAE PAPER 921298) Copyright

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NASA-Johnson has guided the development of a nonventing The chemicals produced by the microbial processes involved Metal Oxide Regenerable EMU CO2 Removal Subsystem (MORES) in the 'biofilms' which form on the surfaces of manned spacecraft which employs a catalyzed, Ag-based metal oxide to achieve CO2 water reclamation systems encompass both metals and organic removal during EVA, while requiring no supplemental cooling. poisons; both are potential hazards to astronaut health and the Regeneration is then easily obtained by means of cabin air, in a growth of the plants envisioned for closed-cycle life support simple hot-air process. The MORES technology has been systems. Image analysis is here shown to be a very useful technique demonstrated in the case of a full size EMU contaminant control for the study of biofilm formation on candidate water-processor cartridge employing a conventional packed bed, as well as an materials for Space Station Freedom. The biodeterioration of improved sheet matrix configuration. AIAA materials exposed to biofilms can be swiftly evaluated by means of electrochemical impedance spectroscopy. AIAA A93-41464* National Aeronautics and Space Administration. Lyndon B. Johnson Space Center, Houston, TX. A93-41474* National Aeronautics and Space Administration. PORTABLE LIFE SUPPORT SYSTEM REGENERATIVE Lyndon B. Johnson Space Center, Houston, TX. CARBON DIOXIDE AND WATER VAPOR REMOVAL BY USE OF SORPTION TECHNOLOGY FOR TREATMENT OF METAL OXIDE ABSORBENTS PREPROTOTYPE HARDWARE HUMIDITY CONDENSATE FOR POTABLE WATER DEVELOPMENT AND TESTING SUNDARA R. M. AJJARAPU and J. M. SYMONS (Houston Univ., JOAN M. HART, JOSEPH B. BORGHESE (Allied-Signal Aerospace, TX) Jul. 1992 20 p. SAE, International Conference on Torrance, CA), CRAIG H. CHANG (Allied-Signal Research and Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 Technology, Des Plaines, IL), and ROBERT J. CUSICK (NASA, refs Johnson Space Center, Houston, TX) Jul. 1992 12 p. SAE, (Contract NAG9-284) International Conference on Environmental Systems, 22nd, Seattle, (SAE PAPER 921312) Copyright WA, July 13-16, 1992 refs This research focused on the testing of the original potable (Contract NAS9-17900) water processor aboard Space Station Freedom that was to (SAE PAPER 921299) Copyright produce potable water from the humidity condensate and additional NASA-Johnson has acquired a preprototype/full-scale metal water generated by carbon dioxide reduction. Humidity condensate oxide CO2 and humidity remover (MOCHR), together with its was simulated by an influent water model 'Ersatz'. The humidity regeneration module. Tests conducted prior to delivery by the condensate was treated with multifiltration (MF) beds that consisted MOCHR's manufacturer have demonstrated the concurrent removal of a train of sorption beds (referred to as 'Unibed') designed to of H2O and CO2 at rates, and under conditions, that are applicable remove specific contaminants. For the complete simulated MF to EVA Portable Life Support Systems. AIAA system runs tested for 100 bed volumes (BV) (volume processed/total column volume), 0.6 percent of the TOC was A93-41472* National Aeronautics and Space Administration. removed by the SAC/IRN 77 (Strong Acid Cation exchange resin), Lyndon B. Johnson Space Center, Houston, TX. 39.6 percent of the total organic carbon (TOC) was removed by BIOFILM FORMATION AND CONTROL IN A SIMULATED the WBA/IRA 68 (Weak Base Anion exchange resin), 13.2 percent SPACECRAFT WATER SYSTEM - THREE YEAR RESULTS of the TOC was removed by activated carbon adsorption (580-26), JOHN R. SCHULTZ, DAVID T. FLANAGAN, REBEKAH J. BRUCE, and the remaining sorbent media acted as polishing units to remove PAUL D. MUDGETT, SANDRA E. CARR, JEFFREY A. RUTZ, M. an additional 1.6 percent of the TOC at steady state. At steady H. HULS (Krug Life Sciences, Inc., Houston, TX), RICHARD L state, 45 percent of the influent TOC passed through the MF SAUER, and DUANE L. PIERSON (NASA, Johnson Space Center, bed. Author Houston, TX) Jul. 1992 15 p. SAE, International Conference on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 refs A93-41475* National Aeronautics and Space Administration. (SAE PAPER 921310) Copyright Marshall Space Flight Center, Huntsville, AL. Two simulated spacecraft water systems are being used to DETERMINATION OF ORGANIC CARBON AND IONIC evaluate the effectiveness of iodine for controlling microbial ACCOUNTABILITY OF VARIOUS WASTE AND PRODUCT contamination within such systems. An iodine concentration of WATERS DERIVED FROM ECLSS WATER RECOVERY TESTS about 2.0 mg/L is maintained in one system by passing ultrapure AND SPACELAB HUMIDITY CONDENSATE water through an iodinated ion exchange resin. Stainless steel DONALD L. CARTER (NASA, Marshall Space Flight Center, coupons with electropolished and mechanically-polished sides are Huntsville, AL), HAROLD COLE, MARK HABERCOM (Boeing Co., being used to monitor biofilm formation. Results after three years Missiles and Space Div., Huntsville, AL), and GUY GRIFFITH of operation show a single episode of significant bacterial growth (Sverdrup Technology, Inc., Tullahoma, TN) Jul. 1992 26 p. in the iodinated system when the iodine level dropped to 1.9 SAE, International Conference on Environmental Systems, 22nd, mg/L. This growth was apparently controlled by replacing the Seattle, WA, July 13-16, 1992 refs iodinated ion exchange resin, thereby increasing the iodine level. (SAE PAPER 921313) Copyright The second batch of resin has remained effective in controlling The development of a closed-loop water recovery system for microbial growth down to an iodine level of 1.0 mg/L. SEM indicates Space Station Freedom involves many technical challenges that the iodine has impeded but may have not completely eliminated associated with contaminant removal. Attention is presently given the formation of biofilm. Metals analyses reveal some corrosion in to the characterization of contaminants constituting total organic the iodinated system after 3 years of continuous exposure. carbon (TOC), and to the Hubaux and Vos (1970) statistical model Significant microbial contamination has been present continuously for low level TOC that has been employed. A tabulation is given in a parallel noniodinated system since the third week of for TOC accountability in the case of both potable and hygiene operation. Author waters. AIAA

A93-41473 National Aeronautics and Space Administration. A93-41478* National Aeronautics and Space Administration. Marshall Space Flight Center, Huntsville, AL. Lyndon B. Johnson Space Center, Houston, TX. BIODETERIORATION OF MATERIALS IN WATER REGENERABLE MICROBIAL CHECK VALVE - LIFE CYCLE RECLAMATION SYSTEMS TESTS RESULTS TIM FORD, JAMES S. MAKI, and RALPH MITCHELL (Harvard JAMES E. ATWATER, RICHARD R. WHEELER, JR., J. T. Univ., Cambridge, MA) Jul. 1992 7 p. SAE, International OLIVADOTI (Umpqua Research Co., Myrtle Creek, OR), RICHARD Conference on Environmental Systems, 22nd, Seattle, WA, July L. SAUER (NASA, Johnson Space Center, Houston, TX), and 13-16, 1992 refs DAVID T. FLANAGAN (Krug Life Sciences, Inc., Houston, TX) (Contract NCC8-17; NCC2-628) Jul. 1992 12 p. SAE, International Conference on Environmental (SAE PAPER 921311) Copyright Systems, 22nd, Seattle, WA, July 13-16, 1992 refs

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(Contract NAS9-18361) space missions. This paper presents results of a developmental (SAE PAPER 921316) Copyright program focused on the use of a Life cycle regeneration testing of the Microbial Check Valve liquid-sorbent/membrane-contactor (LSMC) system for removal of (MCV) that is used on the Shuttle Orbiter to provide microbial CO2 and water vapor from air. In this system, air from the spacecraft control of potable water is currently in progress. Four beds are cabin atmosphere is circulated through one side of a hollow-fiber being challenged with simulated reclaimed waters and repeatedly membrane contactor. On the other side of the membrane contactor regenerated. Preliminary results indicate that contaminant systems is flowed a liquid sorbent, which absorbs the CO2 and water exhibit unique regeneration periodicities. Cyclic throughput vapor from the feed air. The liquid sorbent is then heated to diminishes with increasing cumulative flow. It is considered to be desorb the CO2 and water vapor. The CO2 is subsequently feasible to design a regenerable MCV system which will function removed from the system as a concentrated gas stream, whereas without human intervention and with minimal resupply penalty for the water vapor is condensed, producing a water stream. A the 30 year life of the Space Station. AIAA breadboard system based on this technology was designed and constructed. Tests showed that the LSMC breadboard system can A93-41480 produce a CO2 stream and a liquid-water stream. Details are GRAY WATER RECYCLING WITH A UNIQUE VAPOR presented on the operation of the system, as well as the effects COMPRESSION DISTILLATION (VCD) DESIGN on performance of variations in feed conditions. Author (revised) M. A. FRIEDMAN, T. E. STYCZYNSKI, S. H. SCHWARTZKOPF (Lockheed Missiles & Space Co., Inc., Sunnyvale, CA), B. W. A93-41484* National Aeronautics and Space Administration. TLEIMAT, and M. C. TLEIMAT Jul. 1992 10 p. SAE, International Ames Research Center, Moffett Field, CA. Conference on Environmental Systems, 22nd, Seattle, WA, July A NOVEL MEMBRANE DEVICE FOR THE REMOVAL OF 13-16, 1992 refs WATER VAPOR AND WATER DROPLETS FROM AIR (SAE PAPER 921318) Copyright ROD RAY, DAVID D. NEWBOLD, SCOTT B. MCCRAY, DWAYNE This paper describes the design and test of a gray water T. FRIESEN (Bend Research, Inc., OR), and MARK KLISS (NASA, recycling system based on VCD using a patented evaporator. The Ames Research Center, Moffett Field, CA) Jul. 1992 10 p. system has previously been tested using sea water and agricultural SAE, International Conference on Environmental Systems, 22nd, runoff as the feed, but gray water had never been tested. The Seattle, WA, July 13-16, 1992 refs work covered in this paper evaluated the utility and performance (Contract NAS2-13345) potential of VCD in recycling gray water in partial- and full-gravity (SAE PAPER 921322) Copyright environments. The gray water recycling test used a defined gray One of the key challenges facing NASA engineers is the water simulant as the input to the VCD system. Engineering data development of systems for separating liquids and gases in were taken and samples of the product distilled water, the waste microgravity environments. In this paper, a novel membrane-based brine, and original feed were collected as the operating parameters phase separator is described. This device, known as a water of the system were varied. Results show that this is an extremely recovery heat exchanger (WRHEX), overcomes the inherent efficient recycling system that produces excellent quality distilled deficiencies of current phase-separation technology. Specifically, water with recovery efficiencies of over 95 percent. Depending on the WRHEX cools and removes water vapor or water droplets the operating conditions, the energy consumption varied from 32 from feed-air streams without the use of a vacuum or centrifugal to 64 Watt-hours/kg (120 to 240 W-hr/gal) of condensate force. As is shown in this paper, only a low-power air blower and produced. Author (revised) a small stream of recirculated cool water is required for WRHEX operation. This paper presents the results of tests using this novel A93-41482 membrane device over a wide range of operating conditions. The MEMBRANE TECHNOLOGY FOR ZERO GRAVITY LIFE data show that the WRHEX produces a dry air stream containing SUPPORT SYSTEMS no entrained or liquid water - even when the feed air contains ALAN D. WILLIAMS and JEFFREY J. FASZCZA (Hamilton water droplets or mist. An analysis of the operation of the WRHEX Standard, Windsor Locks, CT) Jul. 1992 8 p. SAE, International is presented. Author (revised) Conference on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 refs (SAE PAPER 921320) Copyright A93-41485 Membrane technology development for both gas separation RECOVERING POTABLE WATER FROM WASTEWATER IN and pervaporation separation processes aimed at maximizing SPACE PLATFORMS BY LYOPHILIZATION membrane selectivity while maintaining high permeation rates is PETER J. HOLLAND, CAROLYN L. MILLER, DONALD M. BIRD, addressed. Current technology can be extended to develop new JENNY E. YUNG, and DORAL E. SANDLIN (U.S. Air Force membrane materials for space life support applications in three Academy, Colorado Springs, CO) Jul. 1992 11 p. SAE, areas, namely, thin film composites, immobilized liquid membranes, International Conference on Environmental Systems, 22nd, Seattle, and volatile rejection membranes. It is concluded that the WA, July 13-16, 1992 refs state-of-the-art membrane technology in these three areas is (SAE PAPER 921323) Copyright applicable to zero gravity life support systems including CO2 The USAFA research on lyophilization of urine and the NASA removal and water purification. AIAA standard wastewater cocktail is reviewed. Bacteriological results show that normal flora from the urinary tract does not survive lyophilization. Formation of capsules do not protect the host A93-41483* National Aeronautics and Space Administration. bacterium from the environmental stresses exerted by lyophilization. Lyndon B. Johnson Space Center, Houston, TX. Physicochemical results reveal that NASA Space Station Freedom OPERATION OF A BREADBOARD standards were met or exceeded in all tested parameters except LIQU1D-SORBENT/MEMBRANE-CONTACTOR SYSTEM FOR that of ammonia-nitrogen in the product water generated from the REMOVING CARBON DIOXIDE AND WATER VAPOR FROM raw blended urine. Lyophilization recovered about 97 and 95 AIR percent of the water from humane urine and the wastewater SCOTT B. MCCRAY, ROD RAY, DAVID D. NEWBOLD, DOUGLAS L MILLARD, DWAYNE T. FRIESEN (Bend Research, Inc., OR), cocktail, respectively. AIAA and SANDRA FOERG (NASA, Johnson Space Center, Houston, TX) Jul. 1992 10 p. SAE, International Conference on A93-41493 Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 RECENT REGENERATIVE ECLSS TECHNOLOGY (Contract NAS9-18348) DEVELOPMENTS IN EUROPE (SAE PAPER 921321) Copyright H. PREISS (Dornier GmbH, Friedrichshafen, Germany), G. TAN, Processes to remove and recover carbon dioxide (CO2) and and C. SAVAGE (ESTEC, Noordwijk, Netherlands) Jul. 1992 water vapor from air are essential for successful long-duration 10 p. SAE, International Conference on Environmental Systems,

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22nd, Seattle, WA, July 13-16, 1992 refs return-to-flight of STS-26 in September 1988 which resulted in (SAE PAPER 921332) Copyright improved crew compartment habitability and less potential for The status of the preliminary breadboarding based on a steam equipment malfunction. AIAA desorbed solid amine concentrator and a Sabatier reactor is discussed. Test results on a five cell fixed alkaline electrolyzer for regenerative fuel cell applications are reported. Possible application A93-41505 of vacuum desorbed solid amine for regenerative CO2 control in TEST OF THE SHUTTLE EXTENDED DURATION ORBITER HERMES and COLUMBUS is addressed. AIAA (EDO) WASTE COLLECTION SUBSYSTEM (WCS) DONALD W. RETHKE (Hamilton Standard, Windsor Locks, CT) A93-41497 Jul. 1992 14 p. SAE, International Conference on Environmental LIFE SUPPORT AND HABITABILITY MANUAL ESA PSS-03-406 Systems, 22nd, Seattle, WA, July 13-16, 1992 refs ROBIN C. HUTTENBACH (Nelson Space Services, Ltd., London, (SAE PAPER 921346) Copyright United Kingdom) Jul. 1992 16 p. SAE, International Conference A new concept for human waste collection, compaction, and on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 storage has been developed to accommodate the planned longer Research supported by ESA refs flight durations required for the Shuttle. The new commode features (SAE PAPER 921338) Copyright brushless dc motor driven fan/separators for urine collection, The paper describes some of the features of a reference manual individual disposable bags for fecal collection with mechanized to be issued by the European Space Agency that will form part of compaction, and in-flight removable canisters that allow natural a set of standards covering the subjects of environmental control, biodegradation of the stored solid waste. Results of the EDO life support, habitability, and human factors. The Manual contains WCS commode development and evaluation tests performed in information on the general requirements of life support and the NASA JSC Houston show that the unit operates properly to habitability and the missions that will drive its associated collect liquid and solid waste. AIAA technologies. It is formatted as a series of individual data sheets that can be updated regularly and which are designed to accommodate inputs from other organizations and individuals. It A93-41506* National Aeronautics and Space Administration. also includes details of promising experimental work and theoretical Lyndon B. Johnson Space Center, Houston, TX. concepts, as well as historical reviews that will help to guide the SPACE SHUTTLE ORBITER OXYGEN PARTIAL PRESSURE selection of technologies and the design of new systems. The SENSING AND CONTROL SYSTEM IMPROVEMENTS paper presents examples from the Manual, which highlight aspects ROBERT F. FRAMPTON (Carleton Technologies, Inc., Orchard of a systems approach to life support. Trade-off methods that Park, NY), DENNIS M. HOY (NASA, Johnson Space Center, can be used to evaluate competing technologies and their Houston, TX), KEVIN J. KELLY (Rockwell International Corp., Seal combinations at sub-system and systems level are also Beach, CA), and JAMES J. WALLESHAUSER (Carleton described. Author (revised) Technologies, Inc., Orchard Park, NY) Jul. 1992 15 p. SAE, International Conference on Environmental Systems, 22nd, Seattle, A93-41503* National Aeronautics and Space Administration. WA, July 13-16, 1992 refs Lyndon B. Johnson Space Center, Houston, TX. (SAE PAPER 921347) Copyright PERFORMANCE EVALUATION OF CANDIDATE SPACE SUIT A program aimed at developing a new PPO2 oxygen sensor ELEMENTS FOR THE NEXT GENERATION ORBITAL EMU and a replacement amplifier for the Space Shuttle Orbiter is PHILIP R. WEST and STEPHANIE V. TRAUSCH (NASA, Johnson described. Experimental design methodologies used in the test Space Center, Houston, TX) Jul. 1992 15 p. SAE, International and modeling process made it possible to enhance the Conference on Environmental Systems, 22nd, Seattle, WA, July effectiveness of the program and to reduce its cost. Significant 13-16, 1992 refs cost savings are due to the increased lifetime of the basic sensor (SAE PAPER 921344) Copyright cell, the maximization of useful sensor life through an increased The AX-5 all metallic, multibearing technologies developed at amplifier gain adjustment capability, the use of streamlined the Ames Research Center and the Mk III fabric and metallic production processes for the manufacture of the assemblies, and technologies developed at the Johnson Space Center were the refurbishment capability of the replacement sensor. AIAA evaluated using the current Space Shuttle space suit technologies as a baseline. Manned evaluations were performed in the Weightless Environment Training Facility and KC-135 zero-gravity A93-41507* National Aeronautics and Space Administration. aircraft. Joint torque, range, cycle life, and environmental protection Lyndon B. Johnson Space Center, Houston, TX. characteristics were analyzed during unmanned tests. Both SHUTTLE ORBITER ENVIRONMENTAL CONTROL AND LIFE numerical results and test subject comments on performance are SUPPORT SYSTEM - FLIGHT EXPERIENCE presented. AIAA H. E. WINKLER (NASA, Johnson Space Center, Houston, TX) Jul. 1992 8 p. SAE, International Conference on Environmental A93-41504* National Aeronautics and Space Administration. Systems, 22nd, Seattle, WA, July 13-16, 1992 refs Lyndon B. Johnson Space Center, Houston, TX. (SAE PAPER 921348) Copyright SPACE SHUTTLE CREW COMPARTMENT This paper describes the overall design of the Shuttle Orbiter DEBRIS-CONTAMINATION Environmental Control and Life Support System (ECLSS). The JERRY R. GOODMAN and LEOPOLDO J. VILLARREAL (NASA, Orbiter ECLSS consists of six major subsystems which accomplish Johnson Space Center, Houston, TX) Jul. 1992 12 p. SAE, the functions of providing a habitable pressurized cabin atmosphere International Conference on Environmental Systems, 22nd, Seattle, and removing gaseous contaminants, controlling the temperature WA, July 13-16, 1992 of the cabin and vehicle components within acceptable ranges, (SAE PAPER 921345) Copyright providing fire detection and suppression capability, maintaining a Remedial actions undertaken to reduce debris during manned supply of potable water, collecting and removing metabolic waste flights and ground turnaround operations at Kennedy Space Center materials, and providing utilities and access for extravehicular and Palmdale are addressed. They include redesign of selected activity. The operational experience is summarized for the 45 space ground support equipment and Orbiter hardware to reduce flights accomplished to date during which the Orbiter ECLSS has particularization/debris generation; development of new detachable been demonstrated to perform reliably, and has proved to have filters for air-cooled avionics boxes; application of tape-on screens the flexibility to meet a variety of mission needs. Significant flight to filter debris; and implementation of new Orbiter maintenance problems are described, along with the design or procedure and turnaround procedures to clean filters and the crew changes which were implemented to resolve the problems. compartment. Most of these steps were implemented before the Author

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A93-41509 requirements for a detailed reverse-osmosis model. AIR HANDLING AND ATMOSPHERE CONDITIONING Author (revised) SYSTEMS FOR MANNED SPACECRAFT - A DESIGN AND PERFORMANCE DATA SURVEY A93-41512 CHARLES E. MARTIN and ARTHUR K. MCCORMICK, III HIGH-RECOVERY LOW-PRESSURE REVERSE OSMOSIS (McDonnell Douglas Space Systems, Huntington Beach, CA) Jul. CAL C. HERRMANN (Bionetics Corp., Moffett Field, CA) Jul. 1992 28 p. SAE, International Conference on Environmental 1992 11 p. SAE, International Conference on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 refs Systems, 22nd, Seattle, WA, July 13-16, 1992 refs (SAE PAPER 921350) Copyright (SAE PAPER 921353) Copyright As the complexity of manned spacecraft increases, close Membrane performance parameters have been obtained for consideration of Environmental Control and Life Support (ECLS) high water recovery operation in the pressure range up to 1.4 systems design becomes important. Mission design topics and MPascals (200 psig) for system modeling. Simple equations can flight performance data for a subset of the overall ECLS system, be fitted to these measurements, from which RO system the Air Handling and Atmosphere Conditioning (AH&AC) system, performance can be predicted or simulated as part of a model of are presented to aid in designing systems for future manned system performance. A single-pump configuration with feedback missions. Included are such topics as crew habitable volumes, air has been found useful in reaching high brine osmotic pressures circulation velocities, atmospheric pressures, electrical component in continuous-flow operation. Enhanced brine concentration as well and metabolic cooling, ventilation fan designs, and contaminant as an enhanced fraction of product/feed water recovery can be removal systems. The condensed information in this paper obtained by recycling a second-stage permeate of intermediate represents the first step in a much larger internal study with the quality. For spaceflight recycling of hygiene water this permits goal of optimizing the design and efficiency of physical/chemical lower pressure-vessel ratings, or higher water recovery, or both. life support systems, using flight data and 'lessons learned' to Author support this goal. Author A93-41513 A93-41510* National Aeronautics and Space Administration. COMPUTER MODELING OF THE VARIABLE PRESSURE Ames Research Center, Moffett Field, CA. GROWTH CHAMBER USING THE CASE/A SIMULATION WATER RECLAMATION TECHNOLOGY DEVELOPMENT FOR PACKAGE FUTURE LONG RANGE MISSIONS CARL D. MCFADDEN (McDonnell Douglas Space Systems, Houston, TX) and ADAM M. MILLER (McDonnell Douglas Space MICHAEL T. FLYNN, KARL AMO, T. M. HIGHTOWER, and JOHN FISHER (NASA, Ames Research Center, Moffett Field, CA) Jul. Systems, Huntington Beach, CA) Jul. 1992 8 p. SAE, International Conference on Environmental Systems, 22nd, Seattle, 1992 11 p. SAE, International Conference on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 refs WA, July 13-16, 1992 refs (SAE PAPER 921351) Copyright (SAE PAPER 921354) Copyright A computer simulation of the variable pressure growth chamber This paper covers the development of computer simulation (VPGC) located at the NASA Johnson Space Center has been models of the Vapor Compression Distillation (VCD) process, the developed using an expanded version of the Computer-Aided Super Critical Water Oxidation (SCWO) process, and two versions Systems Engineering and Analysis (CASE/A) simulation package. of a Vapor Phase Catalytic Ammonia Reduction (VPCAR) process. The VPGC is a pressure chamber that has been outfitted to support These process level models have combined into two Integrated the growth of approximately 10.6 sq m of plants in an enclosed Water Reclamation Systems (IWRS). Results from these integrated environment of approximately 27 cu m. CASE/A is a models, in conjunction with other data sources, have been used to develop a preliminary comparison of the two systems. Also physical/chemical system-level simulation package originally developed to model the life support systems of Space Station discussed in this paper is the development of a Vapor Phase Freedom. The expanded version of CASE/A extends the simulation Catalytic Ammonia Reduction teststand and the development of a package by including biological components, primarily plant growth new urine analog for use with the teststand and computer models. Author algorithms. The configuration, modeling methods and verification of the CASE/A Variable Pressure Growth Chamber model are described. Performance estimates generated from the model are A93-41511* National Aeronautics and Space Administration. compared to data from recent lettuce growth experiments in the Lyndon B. Johnson Space Center, Houston, TX. VPGC. Author (revised) MODELING OF MEMBRANE PROCESSES FOR AIR REVITALIZATION AND WATER RECOVERY A93-41514 National Aeronautics and Space Administration. Ames KEVIN E. LANGE (Lockheed Engineering & Sciences Co., Houston, Research Center, Moffett Field, CA. TX), SANDRA L FOERG, and LIESE A. DALL-BAUMAN (NASA, PLANT CANOPY TRANSPIRATION IN BIOREGENERATIVE Johnson Space Center, Houston, TX) Jul. 1992 14 p. SAE, LIFE SUPPORT SYSTEMS - THE LINK BETWEEN International Conference on Environmental Systems, 22nd, Seattle, MECHANISTIC AND EMPIRICAL MODELS WA, July 13-16, 1992 refs ROBERT J. SIRKO (McDonnell Douglas Space Systems, (SAE PAPER 921352) Copyright Huntington Beach, CA), ANN C. MCCORMACK (NASA, Ames Gas-separation and reverse-osmosis membrane models are Research Center, Moffett Field, CA), and MARYBETH A. EDEEN being developed in conjunction with membrane testing at NASA (NASA, Johnson Space Center, Houston, TX) Jul. 1992 10 p. JSC. The completed gas-separation membrane model extracts SAE, International Conference on Environmental Systems, 22nd, effective component permeabilities from multicomponent test data, Seattle, WA, July 13-16, 1992 refs and predicts the effects of flow configuration, operating conditions, (SAE PAPER 921355) Copyright and membrane dimensions on module performance. Variable feed- A model of water transpiration in a plant canopy that combines and permeate-side pressures are considered. The model has been two approaches is presented. The first approach is to account for applied to test data for hollow-fiber membrane modules with underlying physical processes, while the second is to empirically simulated cabin-air feeds. Results are presented for a membrane incorporate transpiration data now being generated at the Johnson designed for air drying applications. Extracted permeabilities are Center Variable Pressure Growth Chamber. The two approaches, used to predict the effect of operating conditions on water physical modeling and data analysis, make it possible to produce enrichment in the permeate. A first-order reverse-osmosis model a model that is more robust than either the standard first-principles has been applied to test data for spiral wound membrane modules model or a straightforward empirical model. It is shown that the with a simulated hygiene water feed. The model estimates an present transpiration model is able to efficiently capture the dynamic effective local component rejection coefficient under behavior of the plant canopy over the entire range of environmental pseudosteady-state conditions. Results are used to define parameters now envisioned to be important in an operating

306 54 MAN/SYSTEM TECHNOLOGY AND LIFE SUPPORT controlled ecological life support system (CELSS). Examples of WA, July 13-16, 1992 refs the use of this model in assessing plant canopy dynamics and (Contract NAGW-2356) CELSS design options are also presented. AIAA (SAE PAPER 921358) Copyright Activities of the Center for Space Environmental Health (CSEH), A93-41515* National Aeronautics and Space Administration. one of several NSCORTs supported by NASA in order to advance Lyndon B. Johnson Space Center, Houston, TX. knowledge in environmental health in space habitats, are reviewed. PLANT GROWTH MODELING AT THE JSC VARIABLE Research in environmental health will define the standards or PRESSURE GROWTH CHAMBER - AN APPLICATION OF requirements needed to protect human health. This information EXPERIMENTAL DESIGN will affect mission plans and the design of space habitats. This ADAM M. MILLER (McDonnell Douglas Space Systems, Huntington reseach will study unique contaminant stresses and lead to risk Beach, CA), MARYBETH EDEEN (NASA, Johnson Space Center, models for human health and performance. AIAA Houston, TX), and ROBERT J. SIRKO (McDonnell Douglas Space Systems, Huntington Beach, CA) Jul. 1992 11 p. SAE, A93-41518 International Conference on Environmental Systems, 22nd, Seattle, BIOMASS PRODUCTIVITY AND SUSTAINABILITY OF A WA, July 13-16, 1992 refs BIOREGENERATIVE LIFE-SUPPORT SYSTEM (SAE PAPER 921356) Copyright GARY A. MITCHELL, LOUIS A. SHERMAN, PAUL M. HASEGAWA, This paper describes the approach and results of an effort to RAYMOND A. BRESSAN, THOMAS K. HODGES, S. S. NIELSEN, characterize plant growth under various environmental conditions PHILIP E. NELSON, and MICHAEL R. LADISCH (Purdue Univ., at the Johnson Space Center variable pressure growth chamber. West Lafayette, IN) Jul. 1992 9 p. SAE, International Conference Using a field of applied mathematics and statistics known as design on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 of experiments (DOE), we developed a test plan for varying (SAE PAPER 921359) Copyright environmental parameters during a lettuce growth experiment. The Energy budgets for future Controlled Ecological Life-Support test plan was developed using a Box-Behnken approach to DOE. Systems (CELSS) must balance not only with respect to primary As a result of the experimental runs, we have developed empirical productivity (i.e., photosynthesis) vs utilization steps (human models of both the transpiration process and carbon dioxide maintenance plus preparative and recycling processes), but also assimilation for Waldman's Green lettuce over specified ranges of with respect to necessary and desired nonlife-support activities of environmental parameters including carbon dioxide concentration, crews (e.g., exploration, research). Present objectives of the light intensity, dew-point temperature, and air velocity. This model NSCORT program at Purdue University include identification of also predicts transpiration and carbon dioxide assimilation for critical paths for biomass conversion to desired forms with different ages of the plant canopy. Author energetics and rate-constant properties that are compatible with life-support sustainability within a CELSS Physico-chemical recycling systems working in conjunction with bioregenerative ones A93-41516* National Aeronautics and Space Administration. likely will be required to keep time constants of critical processes Ames Research Center, Moffett Field, CA. within reasonable limits. Author TESTS CHARACTERIZING BIOPROCESSOR HARDWARE FOR ANALYTICAL MODELING A93-41519 S. GUSTAVINO (McDonnell Douglas Space Systems, Huntington CONTAMINANT DISTRIBUTION AND ACCUMULATION IN Beach, CA) and A. MCCORMACK (NASA, Ames Research Center, WATER RECYCLE SYSTEMS Moffett Field, CA) Jul. 1992 8 p. SAE, International Conference JOANN SILVERSTEIN, JON R. SCHULZ, ROBERT BARKLEY, on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 GAIL M. BRION, and CHARLES HURST (Colorado Univ., refs Boulder) Jul. 1992 10 p. SAE, International Conference on (SAE PAPER 921357) Copyright Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 The tests outlined in this paper were used to characterize the refs hardware components of the Salad Machine, a small (SAE PAPER 921360) Copyright NASA-developed bioprocessor. The data from these tests are Water contaminant distribution research conducted as part of presented, and the methods by which this data can be integrated the activities of the Center For Space Environmental Health, a into system mathematical models are briefly discussed. The NASA Specialized Center of Research and Training, is reviewed. subsystems and physical processes discussed include the lighting The research is based on a scaled-down physical model of a system, the air loop (condensing heat exchanger and the blower), water recycle system to analyze and model four 'indicator' heat transfer to the surroundings, and leakage. Through this effort contaminants: viruses and bacteria, nitrogen species, and selected it was learned that in the development of a test protocol, care organic and inorganic compounds. The water recycle test bed should be taken to order the tests such that environmental encompasses individual water treatment processes linked in a parameters, particularly humidity, require as few large adjustments closed loop, and spiked with chemical and biological contaminants. as possible. Sensor calibration and installation take a substantial A systems approach was used to define experiments and data amount of time, which should be built into the test schedule. Two which can be used to characterize the long-term, overall properties were particularly hard to quantify: the air flow rate and performance of the test bed. AIAA the energy from the lighting system entering into the growth volume. Flow rate can be measured using the appropriate device for the A93-41521 system configuration and airflow. Lighting system radiation level GENERATION OF IODINE DISINFECTION BY-PRODUCTS was measured using three methods. The results of these methods (IDP'S) IN A WATER RECYCLE SYSTEM varied substantially, putting off conclusive quantification of this ROBERT BARKLEY, CHARLES HURST, ANDREW DUNHAM, value. Author (revised) JOANN SILVERSTEIN, and GAIL M. BRION (Colorado Univ., Boulder) Jul. 1992 9 p. SAE, International Conference on A93-41517* National Aeronautics and Space Administration, Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 Washington, DC. refs NASA SPECIALIZED CENTER FOR RESEARCH AND (SAE PAPER 921362) Copyright TRAINING (NSCORT) IN SPACE ENVIRONMENTAL HEALTH Iodine is being considered for disinfection of recycled hygiene THOMAS W. CLARKSON, MARK J. UTELL (Rochester Univ., NY), and potable water in Space Station Freedom. Like chlorine, the GEORGE W. MORGENTHALER (Colorado Univ., Boulder), RALPH halogen iodine can form disinfection by-products (DBPs) when EBERHARDT (Martin Marietta Civil Space & Communications, used as a disinfectant in waters with dissolved or colloidal organic Denver, CO), and ROBERT RABIN (Center for Space and compounds. Recycled shower and laundry wastewater, urine, and Advanced Technology, Fairfax, VA) Jul. 1992 11 p. SAE, condensate from the space cabin atmosphere all have large International Conference on Environmental Systems, 22nd, Seattle, amounts of dissolved and colloidal organic compounds and may

307 54 MAN/SYSTEM TECHNOLOGY AND LIFE SUPPORT generate iodinated DBPs which can be toxic to humans. We have A93-41542* National Aeronautics and Space Administration. investigated the formation of iodinated DBPs (IDP's) in model Lyndon B. Johnson Space Center, Houston, TX. compounds typical of shower wastewater and condensate. The FIRST ENTRY OPERATIONS FOR SPACECRAFT selection of these model compounds and flask experiments to STEVEN WILSON, THOMAS LIMERO (Krug Life Sciences, Inc., test for IDP formation have been described. Methods for reaction, Houston, TX), and JOHN JAMES (NASA, Johnson Space Center, extraction, and analysis for IDPs also have been developed. We Houston, TX) Jul. 1992 9 p. SAE, International Conference have tentatively identified likely organic precursors from recycled on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 water and several iodinated organic compounds formed during refs the reaction with iodine. As we increase the complexity of the (SAE PAPER 921384) Copyright water matrix, eventually studying recycled shower wastewater, the First entry procedures implemented in the industrial setting are flask experiment data will allow understanding of the reactions of considered to identify those applicable to the situation on the iodine disinfectant with the organic compounds found in space SSF. Particular attention is given to consequences when these water recycle systems. Author (revised) procedures are not followed. Operational scenarios for nominal first entry procedures intended to verify air quality before the crew A93-41534 enters the module are outlined. Components of the Environmental SHIELDING STRATEGIES FOR HUMAN EXPLORATION Health System will provide necessary monitoring capability to MISSIONS protect crew health and safety during the planned first entry BENTON C. CLARK (Martin Marietta Planetary Sciences Lab., procedures of the man-tended capability phase of the SSF program. Denver, CO) Jul. 1992 8 p. SAE, International Conference It is apparent that first-entry scenarios have drawn heavily upon on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 industry experience, tempered with the specific characteristics of refs the space flight environment. AIAA (SAE PAPER 921376) Copyright Space mission shielding strategies intended to protect aircraft A93-41544* National Aeronautics and Space Administration. crews from the galactic and solar flare radiation environments are Ames Research Center, Moffett Field, CA. reviewed. Particular attention is given to galactic cosmic ray hazards DEFINING CONTAMINATION CONTROL REQUIREMENTS FOR for Mars and lunar missions, and solar particle events during NON-HUMAN RESEARCH ON SPACE STATION FREEDOM interplanetary Mars and moon flights. AIAA BARBARA J. CORBIN (NASA, Ames Research Center, Moffett Field, CA) and GLENN A. FUNK (GE Government Services, Moffett A93-41539* National Aeronautics and Space Administration. Field, CA) Jul. 1992 10 p. SAE, International Conference on Lyndon B. Johnson Space Center, Houston, TX. Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 ASDA - ADVANCED SUIT DESIGN ANALYZER COMPUTER refs PROGRAM (SAE PAPER 921386) Copyright GRANT C. BUE, BRUCE C. CONGER, JOHN V. IOVINE (Lockheed The use of non-human biological specimens for life sciences Engineering & Sciences Co., Houston, TX), and CHI-MIN CHANG research on Space Station Freedom has generated concerns about (NASA, Johnson Space Center, Houston, TX) Jul. 1992 12 p. spacecraft internal contamination, crew safety and hardware utility. SAE, International Conference on Environmental Systems, 22nd, Various NASA organizations convened to discuss the concerns Seattle, WA, July 13-16, 1992 refs and determine how they should be addressed. This paper will (SAE PAPER 921381) Copyright present the issues raised at this meeting, the process by which An ASDA model developed to evaluate the heat and mass safety concerns were identified, and the means by which transfer characteristics of advanced pressurized suit design contamination control requirements for all biological payloads were concepts for low pressure or vacuum planetary applications is recommended for incorporation into Space Station Freedom safety presented. The model is based on a generalized 3-layer suit that requirements. The microbiological, toxicological and particulate uses the Systems Integrated Numerical Differencing Analyzer '85 contamination criteria for long-term spaceflight will be based on in conjunction with a 41-node FORTRAN routine. The latter realistic assessment of risk and hardware will be designed to meet simulates the transient heat transfer and respiratory processes of established contamination criteria while facilitating crew operations, a human body in a suited environment. The user options for the thereby meeting the needs of the investigator. Author suit encompass a liquid cooled garment, a removable jacket, a CO2/.H2O permeable layer, and a phase change layer. AIAA A93-41545* National Aeronautics and Space Administration, Washington, DC. A93-41541 POTENTIAL HEALTH EFFECTS OF FUME PARTICLES ON THE SPACE STATION CONDENSING HEAT EXCHANGER BIOFILM CREW OF SPACECRAFTS FORMATION AND CONTROL EVALUATION JURAJ FERIN and GUNTER OBERDORSTER (Rochester Univ., ROBERT W. MARSH, NORMAN A. GRABOWSKI, and JOHN W. NY) Jul. 1992 6 p. SAE, International Conference on STEELE (Hamilton Standard, Windsor Locks, CT) Jul. 1992 10 Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 p. SAE, International Conference on Environmental Systems, refs 22nd, Seattle, WA, July 13-16, 1992 refs (Contract NAGW-2356; NIH-ES-01247; NIH-ES-04872) (SAE PAPER 921383) Copyright (SAE PAPER 921387) Copyright The Space Station Temperature and Humidity Control The effect of the size of polymer (e.g., Teflon) particles in Condensing Heat Exchangers will be utilized to remove and collect fumes inhaled by spacecraft personnel on the condition of the atmospheric water vapor generated by the metabolic and hygienic lung tissue and on the recovery of the exposed subjects was activity of crew members. The porous hydrophilic coating within investigated in rats receiving a single intrapulmonary instillation, the heat exchangers will be continually moist and in contact with or repeated inhalation exposures to either TiO2 particles with a steady flow of cabin air which makes them susceptible to microbial primary particle diameter 20 nm, or TiO2 particles with primary growth. This paper summarizes the findings from an ongoing study particle diameter 250 nm. It was found that rats exposed to to evaluate biofilm formation characteristics and microbial control 20-nm-diam particles showed a dramatically higher toxicity and techniques for the Space Station Condensing Heat Exchangers slower recovery compared to the group exposed to the (CHX). This ongoing study examines whether the CHX's are 250-nm-diam particles, due to a larger extent of penetration of susceptible to performance degrading microbial colonization with the interstitium of the lung by the finer particles. AIAA microbial challenge testing under simulated system environmental conditions. Furthermore, the three candidate microbial control A93-41547 National Aeronautics and Space Administration. Ames approaches of periodic heating, periodic drying, and incorporation Research Center, Moffett Field, CA. of an antimicrobial agent, into the hydrophilic coating are DESIGN AND EVALUATION OF A PAYLOAD TO SUPPORT evaluated. Author (revised) PLANT GROWTH ONBOARD COMET 1

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A. HOEHN (Colorado Univ., Boulder), M. H. KLISS (NASA, Ames manipulating live animals, e.g., rats, served as a containment facility Research Center, Moffett Field, CA), M. W. LUTTGES, M. C. for fixatives, and was proposed for use to conduct in-flight ROBINSON, and L. S. STODIECK (Colorado Univ., Boulder) Jul. maintenance during connector pin repair. The cabinet has a front 1992 10 p. SAE, International Conference on Environmental door large enough to allow installation of a full-size microscope Systems, 22nd, Seattle, WA, July 13-16, 1992 refs in-flight and is outfitted with a side window to allow delivery of (Contract NAGW-1197) items into the cabinet without exposure to the spacelab (SAE PAPER 921389) Copyright atmosphere. Additional support subsystems include inside cabinet The paper describes the design and the operation principles mounting, surgical glove fine manipulations capability, and ac or of the Plant Module for Autonomous Space Support (P-MASS), dc power supply for experiment equipment, as will be demonstrated designed to provide life support for a variety of plants, algae, and during Spacelab J. The GPWS, integrated and maintained in a bacteria in low earth orbit during the maiden flight of COMET-1, double flight-rack, interfaces to spacelab systems including water scheduled for 1993. During flight (scheduled to continue for 30 cooling, avionics and cabin air, and power. Verification has been days), both color video images and collected environmental data completed for multiple spacelab scenarios including SLS-2, SL-J, (including light intensity, temperature, relative humidity, CO2 and and SLS-3. Author (revised) O2 concentrations, soil moisture, and nutrients released) will be downlinked to earth several times a day. These data will also be A93-41553 stored within the payload and retrieved from it after reentry and DESIGN AND PRELIMINARY TESTING OF A MEMBRANE recovery. AIAA BASED WATER RECYCLING SYSTEM FOR EUROPEAN MANNED SPACE MISSIONS A93-41548 J. M. BARREAU, T. BOUET (Carrar, France), P. AMBLARD, X. A MATRIX-BASED POROUS TUBE WATER AND NUTRIENT BOUISSON, C. GUIZARD, C. GAVACH, A. LARBOT, and R. A. DELIVERY SYSTEM BINOT (ESTEC, Noordwijk, Netherlands) Jul. 1992 10 p. SAE, R. C. MORROW, R. J. BULA, T. W. TIBBITTS, and W. R. DINAUER International Conference on Environmental Systems, 22nd, Seattle, (Wisconsin Univ., Madison) Jul. 1992 7 p. SAE, International WA, July 13-16, 1992 refs Conference on Environmental Systems, 22nd, Seattle, WA, July (Contract ESA-9254/90/NL/FG) 13-16, 1992 refs (SAE PAPER 921396) Copyright (SAE PAPER 921390) Copyright Results are presented of a development work based on a A system for providing nutrients and water to plants, while study by Madsen et al. (1990) which identified a basic core maintaining good aeration at the roots and preventing water from technology system essentially based on membrane technologies escaping in reduced gravity was developed on the basis of porous and capable of providing recovery of water from moderately tubes embedded in a rooting matrix. Nutrient solution circulated contaminated waste waters like hygiene water and condensation through the porous tubes moves into the rooting matrix by capillary water. Attention is given to the detailed design ol a breadboard action. The system was successfully tested in short-term of a core system consisting of three successive membrane units: microgravity and will be flown aboard Space Shuttle. AIAA ultrafiltration on a mineral membrane, reverse osmosis and electrodialysis, and an oxidation step. Experimental testing for the A93-41549* National Aeronautics and Space Administration. selection of individual components and for the definition of Lyndon B. Johnson Space Center, Houston, TX. operating procedures have been performed. Feasibility REGENERATIVE LIFE SUPPORT SYSTEMS TEST BED demonstration tests on the complete core configuration are being PERFORMANCE - LETTUCE CROP CHARACTERIZATION performed using real shower water and condensation water from DANIEL J. BARTA, MARYBETH A. EDEEN (NASA, Johnson Space a cold room. Microbiologically, the stabilizing agent has a total Center, Houston, TX), and BRADLEY D. ECKHARDT (Lockheed bacteriocide effect, and no living microorganisms were detected Engineering & Sciences Co., Houston, TX) Jul. 1992 9 p. in the stabilization tank after 24 hr in contact with 0.2 percent of SAE, International Conference on Environmental Systems, 22nd, oxonia. Checking was performed downstream, and confirms the Seattle, WA, July 13-16, 1992 refs absence of viable microorganisms in the other parts of the (SAE PAPER 921391) Copyright system. AIAA System performance in terms of human life support requirements was evaluated for two crops of lettuce (Lactuca sative cv. Waldmann's Green) grown in the Regenerative Life Support A93-41554 Systems Test Bed. Each crop, grown in separate pots under EXPERIMENTAL AND THEORETICAL STUDY ON MEMBRANE identical environmental and cultural conditions, was irrigated with DISTILLATION USING THERMOPERVAPORATION half-strength Hoagland's nutrient solution, with the frequency of NOBUO HAMANO, KENJI MITANI (Hitachi, Ltd., Space Systems irrigation being increased as the crop aged over the 30-day crop Div., Yokohama, Japan), HIDEAKI KUROKAWA, TOSHIO SAWA tests. Averaging over both crop tests, the test bed met the (Hitachi, Ltd., Energy Research Lab., Japan), and AKIRA ASHIDA requirements of 2.1 person-days of oxygen production, 2.4 (Hitachi, Ltd., Space Systems Div., Tokyo, Japan) Jul. 1992 7 person-days of CO2 removal, and 129 person-days of potential p. SAE, International Conference on Environmental Systems, potable water production. Gains in the mass of water and O2 22nd, Seattle, WA, July 13-16, 1992 refs produced and CO2 removed could be achieved by optimizing (SAE PAPER 921397) Copyright environmental conditions to increase plant growth rate and by Water recycling systems have been studied at Hitachi using optimizing cultural management methods. AIAA thermopervaporation technology for space use for about 10 years. According to the studies this method is a good candidate for space application from the viewpoint of good water quality, system A93-41552* National Aeronautics and Space Administration. Ames Research Center, Moffett Field, CA. compactness and microgravity adaptability. In this paper we discuss (1) fundamental characteristics, (2) temperature distribution, and THE GENERAL PURPOSE WORK STATION, A SPACIOUS (3) effect of volatile substances of membrane distillation by the MICROGRAVITY WORKBENCH thermopervaporation method from both theoretical and BONNIE P. DALTON, GREG K. SCHMIDT, and P. D. SAVAGE (NASA, Ames Research Center, Moffett Field, CA) Jul. 1992 experimental points of view. Author (revised) 11 p. SAE, International Conference on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992 A93-41555 (SAE PAPER 921394) Copyright HERMES ECLSS - MAIN REQUIREMENTS AND TECHNICAL The General Purpose Work Station (GPWS) is a laboratory SOLUTIONS multiuse facility, as demonstrated during the Spacelab Life Sciences REINHARD SCHAEFER, STEPHEN LUCK, and GERHARD 1 (SLS-1) flight. The unit provided particulate containment under HAUSER (Dornier GmbH, Friedrichshafen, Germany) Jul. 1992 varying conditions, served as an effective work space for 14 p. SAE, International Conference on Environmental Systems,

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22nd, Seattle, WA, July 13-16, 1992 refs N93-27100*# Orbital Technologies Corp., Madison, Wl. (SAE PAPER 921400) Copyright 1991 NASA LIFE SUPPORT SYSTEMS ANALYSIS WORKSHOP Some of the principal aspects of the development work carried Final Report, 1991 out recently in the Hermes ECLSS are presented. For various PEGGY L. EVANICH (National Aeronautics and Space constituent hardware items of the ECLSS, the technical constraints Administration, Washington, DC.), THOMAS M. CRABB, and which are at the origin of the development work are described. CHARLES F. GARTRELL (General Research Corp., Vienna, VA.) The design concepts which have been identified and investigated 1 Mar. 1992 112 p Workshop held in Milwaukee, Wl, 24-27 to fulfill the constraints are discussed, and the technical solution Jun. 1991 which has been selected is presented. For some hardware items (Contract NASW-4470) (e.g., cabin fan and toilet assembly), for which the initial design (NASA-CR-4466; NAS 1.26:4466) Avail: CASI HC A06/MF A02 selection has been supported by breadboard tests, the rationale The 1991 Life Support Systems Analysis Workshop was behind such tests and the major test results are presented. sponsored by NASA Headquarters' Office of Aeronautics and AIAA Space Technology (OAST) to foster communication among NASA, industrial, and academic specialists, and to integrate their inputs and disseminate information to them. The overall objective of systems analysis within the Life Support Technology Program of A93-41564* National Aeronautics and Space Administration. OAST is to identify, guide the development of, and verify designs Lyndon B. Johnson Space Center, Houston, TX. which will increase the performance of the life support systems SETTING SPACECRAFT MAXIMUM ALLOWABLE on component, subsystem, and system levels for future human CONCENTRATIONS FOR 1 HOUR OR 24 HOUR space missions. The specific goals of this workshop were to report CONTINGENCY EXPOSURES TO AIRBORNE CHEMICALS on the status of systems analysis capabilities, to integrate the HECTOR D. GARCIA, THOMAS F. LIMERO (Krug Life Sciences, chemical processing industry technologies, and to integrate Inc., Houston, TX), and JOHN T. JAMES (NASA, Johnson Space recommendations for future technology developments related to Center, Houston, TX) Jul. 1992 6 p. SAE, International systems analysis for life support systems. The workshop included Conference on Environmental Systems, 22nd, Seattle, WA, July technical presentations, discussions, and interactive planning, with 13-16, 1992 refs time allocated for discussion of both technology status and (SAE PAPER 921410) Copyright time-phased technology development recommendations. Key Since the early years of the manned space program, NASA personnel from NASA, industry, and academia delivered inputs has developed and used exposure limits called Spacecraft and presentations on the status and priorities of current and future Maximum Allowable Concentrations (SMACs) to help protect systems analysis methods and requirements. Author astronauts from airborne toxicants. Most of these SMACS are based on an exposure duration of 7 days, since this is the duration N93-27101*# Orbital Technologies Corp., Madison, Wl. Of a 'typical' mission. A set of 'contingency SMACs' is also being 1992 NASA LIFE SUPPORT SYSTEMS ANALYSIS WORKSHOP developed for scenarios involving brief (1-hour or 24- hour) Final Report, 1992 exposures to relatively high levels of airborne toxicants from PEGGY L. EVANICH (National Aeronautics and Space event-related 'contingency' releases of contaminants. The Administration, Washington, DC.), THOMAS M. CRABB, and emergency nature of contingency exposures dictates the use of CHARLES F. GARTRELL (General Research Corp., Vienna, VA.) different criteria for setting exposure limits. The NASA JSC 1 Dec. 1992 84 p Workshop held in Houston, TX, 12-14 May Toxicology Group recently began a program to document the 1992 rationales used to set new SMACs and plans to review the older, (Contract NASW-4470) 7-day SMACs. In cooperation with the National Research Council's (NASA-CR-4467; NAS 1.26:4467) Avail: CASI HC A05/MF A01 Committee on Toxicology, a standard procedure has been The 1992 Life Support Systems Analysis Workshop was developed for researching, setting, and documenting SMAC sponsored by NASA's Office of Aeronautics and Space Technology values. Author (revised) (OAST) to integrate the inputs from, disseminate information to, and foster communication among NASA, industry, and academic specialists. The workshop continued discussion and definition of A93-41565* National Aeronautics and Space Administration. key issues identified in the 1991 workshop, including: (1) modeling Lyndon 8. Johnson Space Center, Houston, TX. and experimental validation; (2) definition of systems analysis THE ROLE OF ENVIRONMENTAL HEALTH SYSTEM AIR evaluation criteria; (3) integration of modeling at multiple levels; QUALITY MONITORS IN SPACE STATION CONTINGENCY and (4) assessment of process control modeling approaches. OPERATIONS Through both the 1991 and 1992 workshops, NASA has continued THOMAS F. LIMERO, STEVE WILSON, SUSAN PERLOT (Krug to seek input from industry and university chemical process Life Sciences,. Inc., Houston, TX), and JOHN JAMES (NASA, modeling and analysis experts, and to introduce and apply new Johnson Space Center, Houston, TX) Jul. 1992 8 p. SAE, systems analysis approaches to life support systems. The workshop International Conference on Environmental Systems, 22nd, Seattle, included technical presentations, discussions, and interactive WA, July 13-16, 1992 refs planning, with sufficient time allocated for discussion of both (SAE PAPER 921414) Copyright technology status and technology development recommendations. This paper describes the Space Station Freedom (SSF) Key personnel currently involved with life support technology Environmental Health System's air-quality monitoring strategy and developments from NASA, industry, and academia provided input instrumentation. A two-tier system has been developed, consisting to the status and priorities of current and future systems analysis of first-alert instruments that warn the crew of airborne methods and requirements. Author contamination and a volatile organic analyzer that can identify volatile organic contaminants in near-real time. The strategy for N93-27121# Federal Aviation Agency, Oklahoma City, OK. Civil air quality monitoring on SSF is designed to provide early detection Aeromedical Inst. so that the contamination can be confined to one module and so COMPARISON OF PORTABLE CREWMEMBER PROTECTIVE that crew health and safety can be protected throughout the BREATHING EQUIPMENT (CPBE) DESIGNS Final Report contingency event. The use of air-quality monitors in fixed and BRUCE WILCOX, JR., GARNET MCLEAN, and HARVEY portable modes will be presented as a means of following the ENGLAND, JR. Apr. 1993 11 p Sponsored by FAA Office of progress of decontamination efforts and ensuring acceptable air Aviation Medicine, Washington, DC quality in a module after an incident. The technology of each (DOT/FAA/AM-93/6) Avail: CASI HC A03/MF A01 instrument will be reviewed briefly; the main focus of this paper, Crewmemeber protective breathing equipment (CPBE) however, will be the use of air-quality monitors before, during, presently certified for transport category aircraft employ 3 types and after contingency incidents. Author (revised) of oxygen production systems: chlorate candle, potassium

310 54 MAN/SYSTEM TECHNOLOGY AND LIFE SUPPORT superoxide, and compressed oxygen. CPBE performance was Station Evolution. Volume 2: Data Management evaluated to expose significant differences based on this distinction. System/Environmental Control and Life Support Systems p 343-365 CPBE tests employing humans were conducted in accordance 1990 with FAA Technical Standard Order C-116. All CPBE were tested Avail: CASI HC A03/MF A04; 1 functional color page for oxygen production, carbon dioxide concentration, internal Viewgraphs on Environmental Control and Life Support System temperature, moisture, and breathing resistance for 15 minutes at (ECLSS) evolution are presented. The Space Station Freedom ground level (1,300 ft) and cabin altitude (8,000 ft), while subjects ECLSS will have to accommodate the changes to Freedom as it exercised. All CPBE produced a mean oxygen level of at least 59 evolves over the design life of 30 years or more. Requirements percent and maintained carbon dioxide level below 5 percent at will change as pressurized modules are added, crew numbers ground level. Differences in internal temperature and humidity were increase, and as the tasks to be performed change. This evolution found. Performance at altitude generally paralleled these findings. will result in different demands on the ECLSS and the numbers Oxygen and carbon dioxide levels provide little discrimination about ECLSS will have to adapt. Technologies other than the baselined the relative merits of particular CPBE. However, differences in the ones may be better able to perform the various tasks and wearability of CPBE, based on internal temperature, humidity, and technological advances will result in improved life support hardware weight, were dependent on the type of CPBE oxygen production having better performance, increased reliability, reduced power system. Author consumption, weight, and volume, greater autonomy, and fewer resupply requirements. A preliminary study was performed to look N93-27177 Technion - Israel Inst. of Tech., Haifa. Faculty of at alternative technologies for life support and evaluate them for Aerospace Engineering. their integration requirements. Derived from text VISUAL FIELD INFORMATION IN NAP-OF-THE-EARTH FLIGHT BY TELEOPERATED HELMET-MOUNTED DISPLAYS N93-27720*# McDonnell-Douglas Space Systems Co., Huntsville, ARTHUR J. GRUNWALD, S. KOHN, and S. J. MERHAV In AL. Israel Society of Aeronautics and Astronautics, 32nd Annual TECHNOLOGIES FOR ECLSS EVOLUTION Conference on Aviation and Astronautics p 78-97 20 Feb. 1992 BRYCE L DIAMANT In NASA, Washington, Technology for Copyright Avail: Israel Society of Aeronautics and Astronautics, Space Station Evolution. Volume 2: Data Management c/o Faculty of Engineering, Tel-Aviv Univ., Ramat Aviv 69978, System/Environmental Control and Life Support Systems p 367-493 Israel 1990 The human ability to derive control-oriented visual field (Contract NAS8-36407) information from teleoperated helmet-mounted displays in Avail: CASI HC A05/MF A04; 1 functional color page nap-of-the-earth flight is investigated. The visual field with these Viewgraphs and discussion on technologies for Environmental types of display originates from a forward-looking infrared radiation Control and Life Support System (ECLSS) evolution are presented. camera, gimbal-mounted at the front of the aircraft and slaved to Topics covered include: atmosphere revitalization including CO2 the pilot's line-of-sight, to obtain wide-angle coverage. Although removal, CO2 reduction, 02 generation, and trace contaminant these displays are proved to be effective in Apache and Cobra control; water recovery and management including urine helicopter night operations, they demand very high pilot proficiency processing, hygiene water processing, and potable water and work load. Experimental work presented in this paper has processing; and waste management. ECLSS technology shown that part of the difficulties encountered in vehicular control schematics, process diagrams, and fluid interfaces are included. by means of these displays can be attributed to the narrow viewing CASI aperture and head/camera slaving system phase lags. Both of these shortcomings will impair visuo-vestibular coordination when N93-27721*# Texas A&M Univ., College Station. Space Research voluntary head rotation is present. This might result in errors in Center. estimating the control-oriented visual field information vital in ALTERNATIVE PROCESSES FOR WATER RECLAMATION vehicular control, such as the vehicle yaw rate or the anticipated AND SOLID WASTE PROCESSING IN A flight path, or might even lead to visuo-vestibular conflicts (motion PHYSICAL/CHEMICAL BIOREGENERATIVE LIFE SUPPORT sickness). Since, under these conditions, the pilot will tend to SYSTEM minimize head rotation, the full wide-angle coverage of the TOM D. ROGERS In NASA, Washington, Technology for Space helmet-mounted display, provided by the line-of-sight slaving Station Evolution. Volume 2: Data Management system is not always fully utilized. ISA System/Environmental Control and Life Support Systems p 495-515 1990 N93-27718*# National Aeronautics and Space Administration. Avail: CASI HC A03/MF A04; 1 functional color page Marshall Space Flight Center, Huntsville, AL. Viewgraphs on alternative processes for water reclamation and ENVIRONMENTAL CONTROL AND LIFE SUPPORT SYSTEM solid waste processing in a physical/chemical-bioregenerative life CHARLES RAY and ALAN ADAMS In NASA, Washington, support system are presented. The main objective is to focus Technology for Space Station Evolution. Volume 2: Data attention on emerging influences of secondary factors (i.e., waste Management System/Environmental Control and Life Support composition, type and level of chemical contaminants, and effects Systems p 317-341 1990 of microorganisms, primarily bacteria) and to constructively address Avail: CASI HC A03/MF A04; 1 functional color page these issues by discussing approaches which attack them in a Viewgraphs on the Environmental Control and Life Support direct manner. Derived from text System (ECLSS) for the space station are presented. The ECLSS is divided into six subsystems: temperature and humidity control N93-27722*# Wyle Labs., Inc., Huntsville, AL. (THC), atmosphere control and supply (ACS), atmosphere INCREASED FIRE AND TOXIC CONTAMINANT DETECTION revitalization (AR), fire detection and suppression (FDS), water RESPONSIBILITY BY USE OF DISTRIBUTED, ASPIRATING recovery management (WRM), and waste management (WM). SENSORS Topics covered include: ECLSS subsystem functions; ECLSS WALLACE W. YOUNGBLOOD In NASA, Washington, Technology distributed system; ECLSS functional distribution; CO2 removal; for Space Station Evolution. Volume 2: Data Management CO2 reduction; oxygen generation; urine processor; and potable System/Environmental Control and Life Support Systems p 517-541 water recovery. CASI 1990 Avail: CASI HC A03/MF A04; 1 functional color page N93-27719*# National Aeronautics and Space Administration. Viewgraphs of increased fire and toxic contaminant detection Marshall Space Flight Center, Huntsville, AL. responsivity by use of distributed, aspirating sensors for space ENVIRONMENTAL CONTROL AND LIFE SUPPORT SYSTEM station are presented. Objectives of the concept described are EVOLUTION (1) to enhance fire and toxic contaminant detection responsivity PAUL WIELAND In NASA, Washington, Technology for Space in habitable regions of space station; (2) to reduce system weight

311 54 MAN/SYSTEM TECHNOLOGY AND LIFE SUPPORT

and complexity through centralized detector/monitor systems; (3) N93-27788*# National Aeronautics and Space Administration. to increase fire signature information from selected locations in a Lyndon B. Johnson Space Center, Houston, TX. space station module; and (4) to reduce false alarms. MAN-SYSTEMS DISTRIBUTED SYSTEM FOR SPACE STATION Derived from text FREEDOM J. L. LEWIS In NASA, Washington, Technology for Space Station N93-27723*# National Aeronautics and Space Administration. Evolution. Volume 3: EVA/Manned Systems/Fluid Management Marshall Space Flight Center, Huntsville, AL. System p 33-56 1990 THE ECLSS ADVANCED AUTOMATION PROJECT EVOLUTION Avail: CASI HC A03/MF A03; 1 functional color page AND TECHNOLOGY ASSESSMENT Viewgraphs on man-systems distributed system for Space BRANDON S. DEWBERRY, JAMES R. CARNES (Boeing Co., Station Freedom are presented. Topics addressed include: Huntsville, AL), BRENDA D. LUKEFAHR (Alabama Univ., description of man-systems (definition, requirements, scope, Huntsville.), JOHN S. ROGERS (Alabama Univ., Huntsville.), subsystems, and topologies); implementation (approach, tools); DANIEL M. ROCHOWIAK (Alabama Univ., Huntsville.), JAMES W. man-systems interfaces (system to element and system to system); MCKEE (Alabama Univ., Huntsville.), and BRIAN L. BENSON prime/supporting development relationship; selected accomplish- (Alabama Univ., Huntsville.) In NASA, Washington, Technology ments; and technical challenges. CASI for Space Station Evolution. Volume 2: Data Management System/Environmental Control and Life Support Systems p 543-565 N93-27789*# National Aeronautics and Space Administration, 1990 Washington, DC. Avail: CASI HC A03/MF A04; 1 functional color page EVA/MANNED SYSTEMS Viewgraphs on Environmental Control and Life Support System JAMES P. JENKINS In its Technology for Space Station Evolution. (ECLSS) advanced automation project evolution and technology Volume 3: EVA/Manned Systems/Fluid Management System p assessment are presented. Topics covered include: the ECLSS 59-68 1990 advanced automation project; automatic fault diagnosis of ECLSS Avail: CASI HC A02/MF A03; 1 functional color page subsystems descriptions; in-line, real-time chemical and microbial Viewgraphs on extravehicular activity/manned systems are fluid analysis; and object-oriented, distributed chemical and presented. Objectives of crewstation design include (1) microbial modeling of regenerative environmental control systems development of human-computer interface technology and description. CASI graphical presentations, including multi-dimensional visual and aural displays; (2) provide a technology base for autonomous vision and other perceptual systems, virtual workstation technology, and N93-27724*# National Aeronautics and Space Administration. computational vision systems; and (3) develop databases and Marshall Space Flight Center, Huntsville, AL. models of human strength, motion, and body positions in MARSHALL SPACE FLIGHT CENTER ECLSS TECHNOLOGY microgravity environments. Extravehicular technology is ACTIVITIES addressed. CASI PAUL WIELAND In NASA, Washington, Technology for Space Station Evolution. Volume 2: Data Management N93-27790"# Hamilton Standard, Windsor Locks, CT. Space System/Environmental Control and Life Support Systems p 567-598 and Sea Systems. 1990 EVOLUTION OF SPACE STATION EMU PLSS TECHNOLOGY Avail: CASI HC A03/MF A04; 1 functional color page RECOMMENDATIONS Viewgraphs on Environmental Control and Life Support System RICHARD C. WILDE In NASA, Washington, Technology for Space (ECLSS) technology activities are presented. Topics covered Station Evolution. Volume 3: EVA/Manned Systems/Fluid include: analytical development; ECLSS modeling approach; Management System p 69-111 1990 example of water reclamation modeling needs; and hardware Avail: CASI HC A03/MF A03; 1 functional color page development and testing. CASI Viewgraphs on extravehicular mobility unit (EMU) portable life support system (PLSS) technology recommendations are N93-27725*# National Aeronautics and Space Administration. presented. Topics covered include: oxygen supply storage; oxygen Lyndon B. Johnson Space Center, Houston, TX. supply regulators; carbon dioxide control; prime movers; crew JSC ECLSS R/T PROGRAM OVERVIEW comfort; heat rejection; power sources; controls; display devices; A. F. BEHREND In NASA, Washington, Technology for Space and sensor technology. CASI Station Evolution. Volume 2: Data Management System/Environmental Control and Life Support Systems p 599-619 N93-27791*# McDonnell-Douglas Space Systems Co., Huntington 1990 Beach, CA. Avail: CASI HC A03/MF A04; 1 functional color page EVOLVING EVA SYSTEM CAPABILITY FOR THE EVOLVING Viewgraphs on Johnson Space Center Environmental Control SPACE STATION FREEDOM REQUIREMENTS and Life Support System (ECLSS) research and technology HOWARD SLADE In NASA, Washington, Technology for Space program overview are presented. Topics covered include: Station Evolution. Volume 3: EVA/Manned Systems/Fluid advancements in electrochemical CO2 removal; supercritical water Management System p 113-119 1990 waste oxidation; electrooxidation for post-treatment of reclaimed Avail: CASI HC A02/MF A03; 1 functional color page water; and photocatalytic post-treatment of reclaimed water. Viewgraphs on evolving extravehicular activity (EVA) system CASI capability for the evolving Space Station Freedom requirements are presented. Topics covered include: pre-scrub 1989 baseline; N93-27787*# National Aeronautics and Space Administration. approach shift resulting from scrub 1989; considerations for Lyndon B. Johnson Space Center, Houston, TX. alternative selection; EVA supply options; and key technologies EXTRAVEHICULAR ACTIVITY SYSTEM for evolution of EVA system life support. CASI MICHAEL N. ROUEN In NASA, Washington, Technology for Space Station Evolution. Volume 3: EVA/Manned Systems/Fluid N93-27792*# National Aeronautics and Space Administration. Management System p 5-31 1990 Langley Research Center, Hampton, VA. Avail: CASI HC A03/MF A03; 1 functional color page EVA AND TELEROBOT INTERACTION Viewgraphs and discussion on the extravehicular activity system KELLI F. WILLSHIRE In NASA, Washington, Technology for for space station evolution are presented. The following topics Space Station Evolution. Volume 3: EVA/Manned Systems/Fluid are addressed: (1) EVAS program status; (2) definition of EVAS Management System p 121-139 1990 baseline; (3) baseline functional requirements; (4) definition of Avail: CASI HC A03/MF A03; 1 functional color page evolutionary EVAS; (5) evolutionary EVAS functional requirements; We are about to enter into a new era - that of astronauts and (6) technology status. CASI working hand in hand with telerobots in space. This has been

312 54 MAN/SYSTEM TECHNOLOGY AND LIFE SUPPORT done to some degree with astronauts and the Space Station MMS is a combination of one or more human beings and one or Shuttle's Remote Manipulator Arm. However, for the Space Station more physical components that are integrated through the common Freedom, not only will astronauts be working with the RMS type purpose of achieving some objective. The human operator interacts system but also with smaller, more dexterous systems such as with the system through the Man-Machine Interface (MMI). CASI the Flight Telerobotic Servicer (FTS). Because EVA time is a premium resource, the most effective use of the astronauts and N93-27847*# Vanderbilt Univ., Nashville, TN. the telerobot will be required. There may be some tasks for which EVA GLOVE RESEARCH TEAM Annual Report it is most efficient to have both the EVA astronaut and the telerobot ALVIN M. STRAUSS, STEVEN W. PETERSON, JOHN A. MAIN, working together. This type of close integration has not occurred RUEBEN D. DICKENSON, BOBBY L. SHIELDS, and CHRISTINE before and brings up many issues. Most of these issues are related H. LORENZ (Vanderbilt Univ. Hospital, Nashville, TN.) Jul. 1992 to technology: communication must be infallible, new control 83 p systems and devices may be required, enhanced telerobot safety (Contract NAGW-2546) systems may be necessary. IVA operations may also be affected (NASA-CR-193014; NAS 1.26:193014) Avail: CASI HC A05/MF by the combined EVA telerobot tasks. There is also the issue of A01 how the EVA astronaut and the telerobot work on separate tasks The goal of the basic research portion of the extravehicular but at the same time. For both situations, research and activity (EVA) glove research program is to gain a greater development of at least some new technology is required; understanding of the kinematics of the hand, the characteristics enhanced communication both by voice and data, sophisticated of the pressurized EVA glove, and the interaction of the two. collision detection systems, more responsive controls and displays. Examination of the literature showed that there existed no These new systems or system enhancements may require acceptable, non-invasive method of obtaining accurate knowledge base systems for their operation. Some of the important biomechanical data on the hand. For this reason a project was issues, types of tasks, the FTS capabilities, the technology that is initiated to develop magnetic resonance imaging as a tool for needed to address those issues, and the possible impact on Space biomechanical data acquisition and visualization. Literature reviews Station Freedom are reviewed. Author (revised) also revealed a lack of practical modeling methods for fabric structures, so a basic science research program was also initiated N93-27793*# Lockheed Missiles and Space Co., Sunnyvale, in this area. CA. Astronautics Div. SIMPLIFIED AID FOR CREW RESCUE (SAFR) H. THOMAS FISHER In NASA, Washington, Technology for N93-27848*# Vanderbilt Univ., Nashville, TN. Space Station Evolution. Volume 3: EVA/Manned Systems/Fluid A FEASIBILITY STUDY OF HAND KINEMATICS FOR EVA Management System p 141-163 1990 ANALYSIS USING MAGNETIC RESONANCE IMAGING Avail: CASI HC A03/MF A03; 1 functional color page RUEBEN D. DICKENSON, CHRISTINE H. LORENZ (Vanderbilt Viewgraphs and discussion of a Crew Emergency Rescue Univ. Hospital, Nashville, TN.), STEVEN W. PETERSON, ALVIN System (CERS) are presented. Topics covered include: functional M. STRAUSS, and JOHN A. MAIN In its EVA Glove Research description; operational description; interfaces with other Team 11 p Jul. 1992 Presented at the 22nd International subsystems/elements; simplified aid for crew rescue (SACR) Conference on Environmental Systems, Seattle, WA, 13-16 Jul. characteristics; potential resource requirements; logistics, repair, 1992 and resupply; potential performance improvements; and automation Avail: CASI HC A03/MF A01 impact. CASI A new method of analyzing the kinematics of joint motion is developed. Magnetic Resonance Imaging (MRI) offers several N93-27794*# National Aeronautics and Space Administration. distinct advantages. Past methods of studying anatomic joint motion Lyndon B. Johnson Space Center, Houston, TX. have usually centered on four approaches. These methods are EVOLVING TECHNOLOGIES FOR SPACE STATION FREEDOM x-ray projection, goniometric linkage analysis, sonic digitization, COMPUTER-BASED WORKSTATIONS and landmark measurement of photogrammetry. Of these four, DEAN G. JENSEN and MARIANNE RUDISILL In NASA, only x-ray is applicable for in vivo studies. The remaining three Washington, Technology for Space Station Evolution. Volume 3: methods utilize other types of projections of inter-joint EVA/Manned Systems/Fluid Management System p 165-179 measurements, which can cause various types of error. MRI offers 1990 accuracy in measurement due to its tomographic nature (as Avail: CASI HC A03/MF A03; 1 functional color page opposed to projection) without the problems associated with x-ray Viewgraphs on evolving technologies for Space Station dosage. Once the data acquisition of MR images was complete, Freedom computer-based workstations are presented. The the images were processed using a 3D volume rendering human-computer computer software environment modules are workstation. The metacarpalphalangeal (MCP) joint of the left index described. The following topics are addressed: command and finger was selected and reconstructed into a three-dimensional control workstation concept; cupola workstation concept; Japanese graphic display. From the reconstructed volumetric images, experiment module RMS workstation concept; remote devices measurements of the angles of movement of the applicable bones controlled from workstations; orbital maneuvering vehicle free flyer; were obtained and processed by analyzing the screw motion of remote manipulator system; Japanese experiment module exposed the MCP joint. Landmark positions were chosen at distinctive facility; Japanese experiment module small fine arm; flight locations of the joint at fixed image threshold intensity levels to telerobotic servicer; human-computer interaction; and ensure repeatability. The primarily two dimensional planar motion workstation/robotics related activities. CASI of this joint was then studied using a method of constructing coordinate systems using three (or more) points. A transformation N93-27795*# National Aeronautics and Space Administration. matrix based on a world coordinate system described the location Marshall Space Flight Center, Huntsville, AL. and orientation of a local target coordinate system. Future research MAN-SYSTEMS INTEGRATION AND THE MAN-MACHINE involving volume rendering of MRI data focusing on the internal INTERFACE kinematics of the hand's individual ligaments, cartilage, tendons, JOSEPH P. HALE In NASA, Washington, Technology for Space etc. will follow. Its findings will show the applicability of MRI to joint kinematics for gaining further knowledge of the hand-glove Station Evolution. Volume 3: EVA/Manned Systems/Fluid Management System p 181-192 1990 (power assisted) design for extravehicular activity (EVA). Derived from text Avail: CASI HC A03/MF A03; 1 functional color page Viewgraphs on man-systems integration and the man-machine interface are presented. Man-systems integration applies the N93-27849'# Vanderbilt Univ., Nashville, TN. systems' approach to the integration of the user and the machine A PRELIMINARY STRUCTURAL ANALYSIS OF SPACE-BASED to form an effective, symbiotic Man-Machine System (MMS). A INFLATABLE TUBULAR FRAME STRUCTURES

313 54 MAN/SYSTEM TECHNOLOGY AND LIFE SUPPORT

JOHN A. MAIN, STEVEN W. PETERSON, and ALVIN M. of the project were: to consolidate the currently separate databases STRAUSS In its EVA Glove Research Team 7 p Jul. 1992 related to pilot certification and aviation accidents and incidents; Avail: CASI HC A02/MF A01 and to use this consolidated database to statistically examine the The use of inflatable structures has often been proposed for relationships that exist among chronological age, accidents, and aerospace and planetary applications. The advantages of such other factors. Although the study was primarily directed at pilots structures include low launch weight and easy assembly. The use who fly for FAR Part 121 air carriers who are subject to the Age of inflatables for applications requiring very large frame structures 60 Rule, additional analyses were conducted for other categories intended for aerospace use are proposed. In order to consider of pilots to take advantage of additional data available for active using an inflated truss, the structural behavior of the inflated frame pilots beyond the age of 60, and to further examine the influence must be examined. The statics of inflated tubes as beams was of confounding factors. Derived from text discussed in the literature, but the dynamics of these elements has not received much attention. In an effort to evaluate the N93-27858*# National Aeronautics and Space Administration. vibration characteristics of the inflated beam a series of free Marshall Space Flight Center, Huntsville, AL. vibration tests of an inflated fabric cantilevers were performed. ENVIRONMENTAL CONTROL AND LIFE SUPPORT SYSTEMS Results of the tests are presented and models for system behavior CHARLES D. RAY In NASA, Washington, Technology for Space posed. Author (revised) Station Evolution. Executive Summary and Overview p 85-101 1990 N93-27850*# Vanderbilt Univ., Nashville, TN. Avail: CASI HC A03/MF A03; 1 functional color page POWER ASSIST EVA GLOVE DEVELOPMENT Viewgraphs on Environmental Control and Life Support Systems JOHN A. MAIN, STEVEN W. PETERSON, and ALVIN M. (ECLSS) for Space Station Freedom are presented. Topics covered STRAUSS In its EVA Glove Research Team 17 p Jul. 1992 include: crew generated wastes processing and reclamation; water Presented at the 22nd International Conference on Environmental reclamation - pre- and post-treatment; simplified waste water Systems, Seattle, WA, 13-16 Jul. 1992 processing; improved trace contaminant removal; and real time Avail: CASI HC A03/MF A01 microbial analysis. CASI Structural modeling of the EVA glove indicates that flexibility in the metacarpophalangeal (MCP) joint can be improved by N93-27859*# National Aeronautics and Space Administration. selectively lowering the elasticity of the glove fabric. Two strategies Ames Research Center, Moffett Field, CA. are used to accomplish this. One method uses coil springs on EXTRAVEHICULAR ACTIVITY TECHNOLOGY DISCIPLINE the back of the glove to carry the tension in the glove skin due BRUCE W. WEBBON In NASA, Washington, Technology for to pressurization. These springs carry the loads normally borne Space Station Evolution. Executive Summary and Overview p by the glove fabric, but are more easily deformed. An active system 103-117 1990 was also designed for the same purpose and uses gas filled Avail: CASI HC A03/MF A03; 1 functional color page bladders attached to the back of the EVA glove that change the Viewgraphs on extravehicular activity technology discipline for dimensions of the back of the glove and allow the glove to bend Space Station Freedom are presented. Topics covered include: at the MCP joint, thus providing greater flexibility at this joint. A extravehicular mobility unit; airlock and EMU support equipment; threshold control scheme was devised to control the action of the tools, mobility aids, and workstations; and telerobotic work aids joint actuators. Input to the controller was provided by thin resistive interfaces. CASI pressure sensors placed between the hand and the pressurized glove. The pressure sensors consist of a layer of polyester film that has a thin layer of ink screened on the surface. The resistivity N93-27860*# National Aeronautics and Space Administration. of the ink is pressure dependent, so an extremely thin pressure Ames Research Center, Moffett Field, CA. sensor can be fabricated by covering the ink patch with another MANNED SYSTEMS TECHNOLOGY DISCIPLINE layer of polyester film and measuring the changing resistance of REMUS BRETOI In NASA, Washington, Technology for Space the ink with a bridge circuit. In order to sense the force between Station Evolution. Executive Summary and Overview p 119-140 the hand and the glove at the MCP joint, a sensor was placed on 1990 the palmar face of the middle finger. The resultant signal was Avail: CASI HC A03/MF A03; 1 functional color page used by the controller to decide whether to fill or exhaust the Viewgraphs on manned systems technology discipline for Space bladder actuators on the back of the glove. The information from Station Freedom are presented. Topics covered include: the sensor can also be used to evaluate the effectiveness of a crew-systems interfaces and interactions; crew training; on-board given control scheme or glove design since the magnitude of the systems maintenance and support; habitability and environment; measured pressures gives some idea of the torque required to and computational human factors. CASI bend a glove finger at the MCP joint. Tests of this actuator, sensor, and control system were conducted in an 57.2 kPa glove box by N93-27927# Search Technology, Inc., Norcross, GA. performing a series of 90 degree finger bends with a glove without SPECIFICATION OF ADAPTIVE AIDING SYSTEMS Final an MCP joint assembly, a glove with the coil spring assembly, Report, 30 Mar. - 30 Nov. 1990 and with the four fingered actuated glove. The tests of these ROBERT C. ANDES, JR. and WILLIAM B. ROUSE Jul. 1992 three glove designs confirm the validity of the model. Author 72 p (Contract F33615-88-C-3612) N93-27851# Hilton Systems, Inc., Cherry Hill, NJ. (AD-A263071; STI-TR-8925-001; NAWCADWAR-92086-60) AGE 60 PROJECT: CONSOLIDATED DATABASE Avail: CASI HC A04/MF A01 EXPERIMENTS Final Report Designers' decision making in specifying adaptive aiding EDWIN J. KAY (Lehigh Univ., Bethlehem, PA.), REGINA M. systems is considered. A study of design decisions in specifying HARRIS, ROBERT S. VOROS (Lehigh Univ., Bethlehem, PA.), aiding for a fighter aircraft mission scenarios is discussed. The DONALD J. HILLMAN (Lehigh Univ., Bethlehem, PA.), DIANE T. requisite background knowledge required for the design of aiding HYLAND (Lehigh Univ., Bethlehem, PA.), and JAMES D. systems and inherent complexity of situations to which adaptive DEIMLER Mar. 1993 96 p aiding is applicable is quite broad. Considering these facts, the (Contract DTFA02-90-90125) initial analysis of aiding designer's decision processes focused on (HS-TR-8025-3C(R2)) Avail: CASI HC A05/MF A01 identification and validation of solutions currently used in the design Statistical analysis on historical data was conducted to process. Results indicate a high degree of consistency on the investigate the relationship between pilot age and accident rates. part of individual designers. However, there were substantial The ultimate long-term aim of the Age 60 Project was to enhance variations among designers in terms of both decisions made and aviation safety by increasing understanding about the relationships information used to make the decisions. The implications of these among pilot age, experience, and accident rates. The specific aims results for development of design tools, as well as the types of

314 54 MAN/SYSTEM TECHNOLOGY AND LIFE SUPPORT research studies whose results would be valued by designers, are hours accumulated at sea. During the 1980s, the basic SPE water considered. DTIC electrolyzer cell structure developed for the Navies was incorporated into several demonstrations for NASA's Space Station N93-27967*# Bechtel National, Inc., San Francisco, CA. Program. Among these were: the SPE regenerative fuel cell for OXYGEN PRODUCTION ON THE LUNAR MATERIALS electrical energy storage; the SPE water electrolyzer for metabolic PROCESSING FRONTIER oxygen production; and the high pressure SPE water electrolyzer BARBARA H. ALTENBERG In Arizona Univ., Proceedings of the for reboost propulsion reactant production. In the 1990s, one Lunar Materials Technology Symposium 14 p Feb. 1992 emphasis will be the development of SPE water electrolyzers for Avail: CASI HC A03/MF A03 the Lunar Outposts Currently defined potential Lunar Outpost During the pre-conceptual design phase of an initial lunar applications for the SPE water electrolyzer include: SPE water oxygen processing facility, it is essential to identify and compare electrolyzers for metabolic oxygen and potable water production the available processes and evaluate them in order to ensure the from reclaimed water; and SPE water electrolyzers operating at success of such an endeavor. The focus of this paper is to provide high pressure as part of stationary and mobile surface energy an overview of materials processing to produce lunar oxygen as storage systems. Author (revised) one part of a given scenario of a developing lunar occupation. More than twenty-five techniques to produce oxygen from lunar N93-27978*# Lockheed Engineering and Sciences Co., Houston, materials have been identified. While it is important to continue TX. Life Support Development Lab. research on any feasible method, not all methods can be ASSESSMENT OF THE STATE OF THE ART IN LIFE implemented at the initial lunar facility. Hence, it is necessary SUPPORT ENVIRONMENTAL CONTROL FOR SEI during the pre-conceptual design phase to evaluate all methods CHARLES H. SIMONDS and GARY P. NOYES In Arizona Univ., and determine the leading processes for initial focus. Researchers Proceedings of the Lunar Materials Technology Symposium 14 p have developed techniques for evaluating the numerous proposed Feb. 1992 methods in order to suggest which processes would be best to Avail: CASI HC A03/MF A03 go to the Moon first. As one section in this paper, the recent This paper defines the types of technology that would be used evaluation procedures that have been presented in the literature in a lunar base for environmental control and life support system are compared and contrasted. In general, the production methods and how it might relate to in situ materials utilization (ISMU) for for lunar oxygen fall into four categories: thermochemical, reactive the Space Exploration Initiative (SEI). There are three types of solvent, pyrolytic, and electrochemical. Examples from two of the interaction between ISMU and the Environmental Control and Life four categories are described, operating characteristics are Support System (ECLSS): (1) ISMU can reduce cost of water, contrasted, and terrestrial analogs are presented when possible. oxygen, and possibly diluent gasses provided to ECLSS-a corollary In addition to producing oxygen for use as a propellant and for to this fact is that the availability of indigenous resources can life support, valuable co-products can be derived from some of dramatically alter life support technology trade studies; (2) ISMU the processes. This information is also highlighted in the description can use ECLSS waste systems as a source of reductant carbon of a given process. Author (revised) and hydrogen; and (3) ECLSS and ISMU, as two chemical processing technologies used in spacecraft, can share technology, N93-27976*# Arizona Univ., Tucson. Environmental Research thereby increasing the impact of technology investments in either Lab. area. Author (revised) CLOSED ECOLOGICAL SYSTEMS: FROM TEST TUBES TO EARTH'S BIOSPHERE N93-27979*# AiResearch Mfg. Co., Los Angeles, CA. ROBERT J. FRYE and GEORGE MIGNON In its Proceedings of DUST PROTECTION FOR ENVIRONMENTAL CONTROL AND the Lunar Materials Technology Symposium 19 p Feb. 1992 LIFE SUPPORT SYSTEMS IN THE LUNAR ENVIRONMENT Avail: CASI HC A03/MF A03 SUSAN FUHS and JEFFREY HARRIS (Lockheed Corp., Houston, Artificially constructed closed ecological systems (CES) have TX.) In Arizona Univ., Proceedings of the Lunar Materials been researched both experimentally and theoretically for over 25 Technology Symposium 12 p Feb. 1992 years. The size of these systems have varied from less than one Avail: CASI HC A03/MF A03 liter to many thousands of cubic meters in volume. The diversity Lunar dust is pervasive, and requirements for dust protection of the included components has a similarly wide range from purely will affect both hardware design and operations planning for lunar aquatic systems to soil based systems that incorporate many surface systems. On Earth, mechanical problems caused by aspects of Earth's biosphere. While much has been learned about particulates include erosive and abrasive effects, clogging of the functioning of these closed systems, much remains to be mechanical equipment, and impairment of seals and bonds. In learned. In this paper, we compare and contrast the behavior of addition, dust tends to degrade the heat rejection properties of closed ecological systems of widely different sizes through an contaminated surfaces. All these effects have been observed on analysis of their atmospheric composition. In addition, we will the lunar surface as well. This paper discusses the potential compare the performance of relatively small CES with the behavior applicability of current dust protection methods to the problem of of Earth's biosphere. We address the applicability of small CES dust protection for the environmental control and life support as replicable analogs for planetary biospheres and discuss the (ECLS) systems of a lunar base, and highlights areas where use of small CES as an experimental milieu for an examination of development may be necessary. A review of dust problems the evolution of extra-terrestrial colonies. Author (revised) experienced during the Apollo missions and of additional, ground-based experience with lunar dust provides a baseline for N93-27977*# United Technologies Corp., Farmington, CT. identifying operations and areas where dust may be expected to Hamilton Standard Div. affect the ECLS systems. Current Earth-based methods of dust SPE WATER ELECTROLYZERS IN SUPPORT OF THE LUNAR protection are identified and the impact of differences between OUTPOST the Earth and lunar environments on these methods is evaluated. J. F. MCELROY In Arizona Univ., Proceedings of the Lunar Finally, integration of dust protection equipment with ECLS systems Materials Technology Symposium 20 p Feb. 1992 equipment is discussed. Author (revised) Avail: CASI HC A03/MF A03 During the 1970s, the SPE water electrolyzer, which uses ion N93-27985*# Boeing Defense and Space Group, Huntsville, AL. exchange membranes as its sole electrolyte, was developed for LUNAR BASE THERMAL MANAGEMENT/POWER SYSTEM nuclear submarine metabolic oxygen production. These ANALYSIS AND DESIGN developments included SPE water electrolyzer operation at up to JERRY R. MCGHEE In Arizona Univ., Proceedings of the Lunar 3,000 psia and at current densities in excess of 1,000 amps per Materials Technology Symposium 12 p Feb. 1992 square foot. The SPE water electrolyzer system is now fully qualified Avail: CASI HC A03/MF A03 for both the U.S. and U.K. Navies with tens of thousands of system A compilation of several lunar surface thermal management

315 54 MAN/SYSTEM TECHNOLOGY AND LIFE SUPPORT and power system studies completed under contract and IR&D is subsystems) were studied. Interface requirements with other presented. The work includes analysis and preliminary design of systems, such as ground test equipment, launch vehicle, earth all major components of an integrated thermal management orbit assembly facility, ground control station, manned lunar landing system, including loads determination, active internal acquisition and take-off vehicle, and lunar freight transport vehicle were also and transport equipment, external transport systems (active and studied. Construction methods, such as operations robots, passive), passive insulation, solar shielding, and a range of lunar construction procedures, and leveling mechanism after landing are surface radiator concepts. Several computer codes were utilized outlined. The results of the study of operation and maintenance in support of this study, including RADSIM to calculate radiation methods and system analysis are introduced. The functional exchange factors and view factors, RADIATOR (developed requirements, system concept, operation methods, including remote in-house) for heat rejection system sizing and performance analysis control, automation, automation, and development and operation over a lunar day, SURPWER for power system sizing, and plan for robots are outlined. Author (NASDA) CRYSTORE for cryogenic system performance predictions. Although much of the work was performed in support of lunar N93-28032# Ishikawajima-Harima Heavy Industries Co. Ltd., rover studies, any or all of the results can be applied to a range Tokyo (Japan). of surface applications. Output data include thermal loads MANNED LUNAR SURFACE SITE: CONCEPTUAL STUDY ON summaries, subsystem performance data, mass, and volume PRESSURIZED LUNAR SURFACE OPERATION ROVER estimates (where applicable), integrated and worst-case lunar day [YUUJIN GETSUMEN KYOTEN: YOATSUGATA GETSUMEN radiator size/mass and effective sink temperatures for several SAGYOU ROBA NO GAINEN KENTOU] concepts (shielded and unshielded), and external transport system YOUICHIROU NAKAMURA, KEIKO YASUDA, ISAO TATE, performance estimates for both single and two-phase (heat MASAHARU TAKADA, SHUUJI TAKAHASHI, and MICHIHIKO pumped) transport loops. Several advanced radiator concepts are HORIE In NASDA, Future Space Activity Workshop: Lunar Base presented, along with brief assessments of possible system benefits Workshop 1992 21 p 15 Jul. 1992 In JAPANESE and potential drawbacks. System point designs are presented for Avail: CASI HC A03/MF A06 several cases, executed in support of the contract and IR&D An overview of the conceptual study on pressurized manned studies, although the parametric nature of the analysis is stressed lunar rover to enable the safety operation of exploration crew is to illustrate applicability of the analysis procedure to a wide variety presented. Subjects of the operation of the rover were studied to of lunar surface systems. The reference configuration(s) derived determine its function and property requirements. Operation modes, from the various studies will be presented along with supporting including mission operation mode and system maintenance mode, criteria. A preliminary design will also be presented for the reference and operation profiles, including those for initial assembly and basing scenario, including qualitative data regarding TPS concerns manned missions, were studied to determine requirements from and issues. Author (revised) the operational aspects. The system and subsystem structures, including resource distribution and control methods, to meet the N93-28029# National Space Development Agency, Tokyo function and property requirements were studied. Two types of (Japan). configurations of the Remote Manipulator Systems (RMS's) were CONCEPTUAL STUDY ON MANNED LUNAR SURFACE SITE determined. Author (NASDA) [YUUJIN GETSUMEN KYOTEN NO GAINEN KENTOU] YUTAKA TAKANO In its Future Space Activity Workshop: Lunar N93-28033# Kawasaki Heavy Industries Ltd., Kobe (Japan). Base Workshop 1992 17 p 15 Jul. 1992 In JAPANESE MANNED LUNAR SURFACE SITE [YUUJIN GETSUMEN Avail: CASI HC A03/MF A06 KYOTEN] An overview of the conceptual study of a manned lunar surface TERUMITSU KAMATA and HIROYUKI TORII In NASDA, Future site, a small scale activity site for a small number of crew members Space Activity Workshop: Lunar Base Workshop 1992 17 p 15 is presented. The objectives of the manned lunar surface site are Jul. 1992 In JAPANESE as follows: (1) validating that human beings can conduct multiple Avail: CASI HC A03/MF A06 activities on the lunar surface; (2) validating the feasibility of Functions required for environment control system (mainly on outstanding development of scientific experiment and technology air conditioning and air regeneration equipment) for the purpose by human activities on the lunar surface; (3) validating the feasibility of calculating their weight and electric power requirement for of providing materials for space activity and further developing habitation module of manned lunar surface site were studied. production activities in space; (4) greatly promoting scientific Studies were conducted on subsystem performance requirements knowledge. about astronomy and space science by astronomical to satisfy the required functions and comparison of constituent and space science observation on the lunar surface; and (5) equipment for the environment control system were conducted to allowing a wide range of people to understand the prospects of select candidate equipment. Required electric power and weight space development. The design concept and missions of the were calculated and totaled to figure out the weight and electric manned lunar base are outlined. The system and its subsystems, power requirement of the environment control system. The above such as structure and mechanism, habitation, electric power, studies were conducted on air circulation, temperature and humidity thermal control, communication, control, logistics, flight and landing control, and particles and microorganisms removal of air subsystems are outlined. The construction and operation plans conditioning equipment and CO2 removal and toxic gas processing are presented. Author (NASDA) equipment for air regeneration. Author (NASDA)

N93-28031# Nippon Electric Co. Ltd., Tokyo (Japan). N93-28034# Ishikawajima-Harima Heavy Industries Co. Ltd., CONCEPTUAL STUDY OF MANNED LUNAR SURFACE SITE Tokyo (Japan). [YUUJIN GETSUMEN KYOTEN NO GAINEN KENTOU] LUNAR SURFACE EXPERIMENT SYSTEM [GETSUMEN TOSHIAKI OKUDAIRA, HARUKI AYATA, KIYOSHI TANAKA, JIKKEN SHISUTEMU] NOBUTAKA KATOU, and NAOKI YOSHIZAWA In NASDA, Future MASAKAZU TAKAMI, SEIKO HOSHI, and YURIKO OKA In Space Activity Workshop: Lunar Base Workshop 1992 22 p 15 NASDA, Future Space Activity Workshop: Lunar Base Workshop Jul. 1992 In JAPANESE 1992 22 p 15 Jul. 1992 In JAPANESE Avail: CASI HC A03/MF A06 Avail: CASI HC A03/MF A06 An overview of a study of a lunar surface site system which An overview of the study on experiment systems operated at does not necessitate Extravehicular Activity (EVA) and robotic manned lunar surface site is presented. Missions to be conducted support in starting the site is presented. Functional and performance at manned lunar surface site were selected by evaluating from requirements for the system, system configurations, system the view points of required resources (electric power, weight, and structure, weight and electric power allotments, and subsystems crew man hours), feasibility, operability, and especially significance (such as structures, habitat, electric power, thermal control, as the frontier base. Mission performance sites, such as pressurized communication control experiment, logistics, and flight and landing and exposed (located near habitation module or at remote location)

316 54 MAN/SYSTEM TECHNOLOGY AND LIFE SUPPORT environments, and system structures, including their ingredient ERICKSEN Feb. 1993 14 p subsystems, corresponding to them are outlined. Resource (Contract F33615-88-C-0014) allotment for the experiment system from the lunar surface site, (AD-A262616; AL-TR-1993-0008) Avail: CASI HC A03/MF A01 resources required for the missions, and mission crew time for This report contains two papers presented at the the experiment system were analyzed and the crew time required Helmet-Mounted Displays IV, International Symposium and for experiment operations at manned lunar base was determined. Exhibition on Optical Engineering and Photonics, held at Orlando, Approximate time required for conducting each mission was studied. FL on 20-24 April 1992. This symposium was sponsored by the A model mission operation and an example of lunar surface Society of Photo-Optical Instrumentation Engineers (SPIE). The experiment system operation (for pressurized environment and near papers describe the development and demonstration of two module experiments) are shown. Author (NASDA) helmet-mounted displays: a low-cost monochrome helmet display and a low-cost color helmet display, both with see-through optics. N93-28112# Mainstream Engineering Corp., Rockledge, FL. The present monochrome CRT display helmet design, through LIGHTWEIGHT PASSIVE MICROCLIMATE COOLING DEVICE demonstrations and system measurements, provided positive data Final Report, Aug. 1991 - Mar. 1992 as a research device. The color LCD helmet display system was CLYDE F. PARRISH and ROBERT P. SCARINGE Mar. 1993 successfully completed and although the resolution of the LCD 65 p matrix structure is not suited for the application of small text in (AD-A262262; NATICK-TR-93/014) Avail: CASI HC A04/MF the presentation, the high contrast and vivid colors produced by A01 the LCD, as well as the see-through function of the optics, provide The intermittent adsorption cooling concept has been the capability for a full field-of-regard visual simulation system which successfully demonstrated and has produced cooling rates in the can be used in conjunction with low-cost cockpit training devices. 300 W range. The design requirement of 300 W for 6 hours has DTIC not been demonstrated due' to system leaks. However, we demonstrated in laboratory experiments that were scaled to a much N93-28757# Chemical Warfare/Chemical and Biological Defense smaller size that we have produced 325 to 432 V of cooling. Information Analysis Center, Edgewood, MD. Laboratory experiments also showed the system could operate EVALUATION OF TEST METHODS AND REQUIREMENTS FOR for more than 8 hours, be started and stopped, when the system RESPIRATORY PROTECTION SYSTEMS 21 Final Report contained no leaks. The current prototype was constructed of T. L RAMIREZ, K. M. REED, M. R. PERRY, C. M. GROVE, and brass and copper for ease of fabrication. No consideration was D. E. MOLNAR Nov. 1992 73 p given to weight. We have examined alternate methods of (Contract DLA900-86-C-2045) construction of the backpack and cylinder assembly and thin (0.01 (AD-A262466; CBIAC-SS-335) Avail: CASI HC A04/MF A01 in.) stainless steel could be used. The stainless steel sheet stock The Joint Services Operational Requirements (JSOR) for vision, could be formed into a backpack bedding the sheets into fins, communications, respiration! thermal, personal support, which also serve to strengthen the backpack. Also, stainless steel compatibility, and psychological factors are presented in this could be used to lower the weight of the cylinders. With these summary. The body of the report provides the test methods used changes, the system weight including water and desiccant, is 23.8 with other pertinent information. The test equipment and cost of Ib. DTIC equipment are provided with recommendations for selection of the test and the equipment. The recommendation section provides N93-28464# Little (Arthur D.), Inc., Cambridge, MA. a synopsis of the findings and suggested equipment the advanced HYBRID OXYGEN SYSTEM Final Report, Sep. 1986 • Dec. protective systems integration laboratory may want to evaluate for 1991 use with advanced mask design. DTIC W. D. LEE Oct. 1992 197 p (Contract F33615-86-C-4505) N93-28850# Advisory Group for Aerospace Research and (AD-A262417; REPT-56913-10; AL-TR-1992-0014) Avail: CASI Development, Neuilly-Sur-Seine (France). Flight Mechanics HC A09/MF A03 Panel. Investigation of concepts for generating oxygen on-board COMBAT AUTOMATION FOR AIRBORNE WEAPON SYSTEMS: combat aircraft and development of a bleed air-driven refrigeration, MAN/MACHINE INTERFACE TRENDS AND TECHNOLOGIES liquefaction, and cryogenic storage system for oxygen were [L'AUTOMATISATION DU COMBAT AERIEN: TENDANCES ET undertaken in this study. A number of alternative approaches were TECHNOLOGIES POUR L'INTERFACE HOMME/MACHINE] examined while considering size, weight and power consumption. Apr. 1993 268 p Symposium held in Edinburgh, Scotland, An open-loop bleed. air-driven system was selected for design, 19-22 Oct. 1992 development, and testing. The bleed air-driven refrigeration unit (AGARD-CP-520; ISBN-92-835-0706-1) Copyright Avail: CASI achieved oxygen liquefaction temperatures of 90 deg K and HC A12/MFA03 liquefied and stored oxygen generated from a molecular sieve Recent advances in combat automation technologies offer oxygen generating system (MSOGS). The oxygen was stored in significant potential for improving overall mission effectiveness. cryogenic dewars, vaporized, and withdrawn from the system to Development of advanced situational awareness display concepts, simulate aircrew consumption. A heat exchanger flow reversing parallel distributed computer architecture, and tactical information valving system was used to sublime and blow out condensates fusion techniques have paved the way for new operational (water vapor and carbon dioxide) which normally collect in an capabilities and weapon system employment tactics. Harnessing open-loop refrigeration cycle operating from ambient air. The these innovative technologies is critically dependent upon collection of condensate in the cryogenic system represented the establishing an effective and intuitive pilot vehicle interface. The largest technological area to overcome, and the reverse cycle symposium addressed changing and possible future operational system overcame the problem. The laboratory demonstrator utilized scenarios, advanced technology concepts, application issues and a helium cycle cold head refrigeration unit in conjunction with a experimental development efforts and included sessions on: fusion, J-T valve to simulate a cryogenic expander to be used in the situation awareness, human capabilities and limitations, and design flight system. Further work to incorporate a cryogenic expander in and evaluation of integrated systems. place of the cold head and J-T valve is recommended. DTIC N93-28853# Elliott-Automation Space and Advanced Military N93-28479# General Electric Co., Gilbert, AZ. Government Systems Ltd., Camberley (England). Aerospace Systems Div. Services. PILOT DECISION AIDING FOR WEAPON DELIVERY: A NOVEL LOW-COST HELMET-MOUNTED DISPLAYS Final Technical APPROACH TO FIRE CONTROL CUEING USING PARALLEL Report, Apr. 1991 - Apr. 1992 COMPUTING ROGER W. LEINENWEVER, LEONARD G. BEST, and BRYCE J. A. R. BUFFETT and R. M. WIMBUSH In AGARD, Combat

317 54 MAN/SYSTEM TECHNOLOGY AND LIFE SUPPORT

Automation for Airborne Weapon Systems: Man/Machine Interface N93-28857# Dornier Luftfahrt G.m.b.H., Friedrichshafen Trends and Technologies 18 p Apr. 1993 (Germany). Flight Simulation Dept. Copyright Avail: CASI HC A03/MF A03 SYMBOLOGY FOR HEAD UP AND HEAD DOWN This paper describes the application of advanced technology, APPLICATIONS FOR HIGHLY AGILE FIGHTER AIRCRAFT: TO both hardware and software, to provide improved pilot IMPROVE SPATIAL AWARENESS, TRAJECTORY CONTROL, Man-Machine Interface (MMI) automation for the central function AND UNUSUAL ATTITUDE RECOVERY, PART 1 of an airborne weapon system, namely weapon release. The G. FISCHER and W. FUCHS In AGARD, Combat Automation specific scenario addressed is that of providing the pilot with for Airborne Weapon Systems: Man/Machine Interface Trends and decision aiding, in the form of firing cues, for the use of air-to-air Technologies 6 p Apr. 1993 missiles. The paper gives an overview of the need for Copyright Avail: CASI HC A02/MF A03 automation/decision aiding in air-to-air missile fire control, by The progressively increasing agility of modern fighter aircraft illustrating the way in which missile performance can vary greatly (a/c) with high onset and high sustained pitch and roll rates makes with the changes of engagement parameters which occur rapidly spatial orientation and awareness an even more demanding task in an air-to-air combat scenario. The high pilot workload in this for the operator. Pilots already complain about fast moving and type of scenario, and the future requirement for multiple twisting pitch bars in the HUD and the necessity to concentrate simultaneous missile firings, further support the need for automation almost their entire attention on maintaining spatial orientation. to provide pilots with simple, processed, predictive data on which Scaled and geared pitch bars relieved the problem to some extent to base their firing decisions. Derived from text but didn't solve it, at least according to our opinion. The above mentioned problems are aggravated with the introduction of advanced fighter a/c capable of even higher onset and angular N93-28855# Universitaet der Bundeswehr Muenchen, Neubiberg rates and flying at higher angles of attack (AoA) or even in the (Germany). Inst. fuer Systemdynamik und Flugmechanik. post-stall regime where the actual flight path in space and the PILOT INTENT AND ERROR RECOGNITION AS PART OF A a/c attitude may deviate to a great extent. In order to overcome KNOWLEDGE BASED COCKPIT ASSISTANT the problems mentioned above, a more stationary and more easily T. WITTIG and R. ONKEN In AGARD, Combat Automation for interpretable reference symbology, a circular arc segment, is used Airborne Weapon Systems: Man/Machine Interface Trends and to indicate pitch (theta) or flight path angle (gamma), whereas the Technologies 10 p Apr. 1993 roll angle (phi) is given by the angular relation between a/c Copyright Avail: CASI HC A02/MF A03 reference symbol and the center of the arc segment. A Pilot Intent and Error Recognition module as part of a Author (revised) knowledge based Cockpit Assistant System is presented, which is being developed at the University of the Armed Forces in Munich N93-28858# Rockwell International Corp., Los Angeles, CA. in cooperation with the Dornier company and implemented in a VIRTUAL INTERFACE APPLICATIONS FOR AIRBORNE flight simulator. The system mainly supports the pilot crew with WEAPONS SYSTEMS regard to the monitoring and planning task and provides assistance EMILY HOWARD In AGARD, Combat Automation for Airborne for a number of plan execution functions for the civil flight operation Weapon Systems: Man/Machine Interface Trends and under Instrument Flight Rules. During the whole flight, the Pilot Technologies 6 p Apr. 1993 Intent and Error Recognition module monitors pilot activities and Copyright Avail: CASI HC A02/MF A03 the flight status in order to detect deviations from the actual flight This paper addresses a class of control and display technology plan immediately. In this case, the current flight situation is that shall be referred to collectively as Virtual Interface (VI) evaluated, the pilot behavior is analyzed over a certain time period technology. The contents of this paper are presented in three and by use of both pilot intent or error is recognized. Pilot errors parts. Part 1 will describe what is meant by a 'virtual interface,' a lead to warning messages, and recognized pilot intent to a suite of control and display technology being developed for future modification of the flight plan. In this paper, a short survey is implementation in operational aircraft systems. The problem that given of the concept and the function of the Cockpit Assistant will be discussed is how the transition process between System. After that the structure of the Pilot Intent and Error development and operational status is particularly difficult for VI Recognition will be described in detail. At the end, the integration technology, given current applications. Part 2 will describe some of this module into the Cockpit Assistant System and the evaluation new applications of VI technology, based upon several programs in a flight simulator are presented. Derived from text that utilize embedded simulation for operational test and evaluation and training purposes. A review of the benefits of VI technology shows promise for accelerating the transition process at least N93-28856# Defence Research Agency, Bedford (England). toward these operational activities. Part 3 then will describe a Flight Dynamics and Simulation Div. new display concept, based on virtual interface technology, that THE DESIGN AND DEVELOPMENT OF THE NEW RAF was designed for one of these embedded simulation applications STANDARD HUD FORMAT and conclude with a discussion of plans for future development. J. R. HALL In AGARD, Combat Automation for Airborne Weapon Author (revised) Systems: Man/Machine Interface Trends and Technologies 11 p Apr. 1993 Sponsored by RAF N93-28859# General Dynamics Corp., Fort Worth, TX. Copyright Avail: CASI HC A03/MF A03 HEAD-STEERED SENSOR FLIGHT TEST RESULTS AND In poor weather and on instruments, the safe piloting of an IMPLICATIONS aircraft requires the display of basic flight information to the pilot L. N. LYDICK In AGARD, Combat Automation for Airborne Weapon in a manner that is instinctive, immediate, and unambiguous. Systems: Man/Machine Interface Trends and Technologies 7 p Head-up display formats have singularly failed in this regard over Apr. 1993 the years and are known to be a contributing factor in many Copyright Avail: CASI HC A02/MF A03 incidents involving lack of spatial awareness by the pilot. This A comprehensive flight test program of a head-steered paper describes the theory, experimental development, and flight FLIR/HMD night attack system was conducted between Aug. 1987 proving of the DRA Fast-Jet HUD Format (FJF). This format has and Jan. 1990. Seventy-five development and demonstration F-16B been designed to keep the pilot spatially aware under the most flights were flown. Approximately 90 percent of the flights were dynamic of flight maneuvers while retaining the flight-path conducted in night visual meteorological conditions. The remainder information so necessary for mission effectiveness during normal were conducted in daytime with the pilot's vision obscured by an tactical maneuvering and steady flight conditions. These include opaque visor cover to simulate night and to study laser eye low level night operations with FLIR and NVGs and highly dynamic, protection. Because the new FLIR/HMD systems were fully hard maneuvering flight in poor weather or on instruments either integrated with the F-16B fire control, navigation, communication, at low level or in the air-to-air role. Derived from text and display system, it was possible to achieve a considerable

318 54 MAN/SYSTEM TECHNOLOGY AND LIFE SUPPORT degree of tactical relevance in the tests. The night attack portion with virtual image displays; namely that the eyes may be of the testing was a subset of a broader series of tests to explore inappropriately accommodated (focused) when using virtual image advanced techniques for close air support (CAS). The work was displays. The possible consequences of these problems are industry sponsored by a number of corporations in a cooperative discussed. Author effort of about thirty million dollars. The tests and demonstrations culminated in operational test by (then) Tactical Air Command N93-28863# Texas Technological Univ., Lubbock. Dept. of pilots at Nellis Air Force Base, Nevada, and Fort Hood, Texas. Industrial Engineering. The night CAS systems evaluations were quite favorable and were HUMAN CAPABILITIES AND LIMITATIONS IN SITUATION planned for production until the remarkable end of the cold war AWARENESS reoriented (or perhaps gave pause to) planned introduction of the MICA R. ENDSLEY and CHERYL A. BOLSTAD (Monterey concepts to the fleet. In this paper, the author provides a summary Technologies, Inc., Gary, NC.) In AGARD, Combat Automation overview of the mission, a description of the systems, the lessons for Airborne Weapon Systems: Man/Machine Interface Trends and learned, and some thoughts about future system requirements. Technologies 10 p Apr. 1993 Author (revised) Copyright Avail: CASI HC A02/MF A03 Achieving high situation awareness (SA) is a major goal in the N93-28860# Defence Research Agency, Farnborough (England). design of aircraft systems. Efforts are currently underway by a Flight Systems Dept. number of individuals who are attempting to address this need THE QUEST FOR AN INTEGRATED FLYING HELMET through improvements in avionics system design, automation, and A. KARAVIS and D. N. JARRETT In AGARD, Combat Automation the pilot-vehicle interface (PVI). These efforts can be greatly for Airborne Weapon Systems: Man/Machine Interface Trends and enhanced through an understanding of human capabilities and Technologies 19 p Apr. 1993 limitations in achieving SA. This paper presents an identification Copyright Avail: CASI HC A03/MF A03 of those factors which underlie basic human SA capabilities, The addition of vision enhancement, display, and control including key information processing mechanisms, critical human functions to aviator's headgear is operationally attractive. The jets skills, and a discussion of external factors which act to hamper and helicopters that are currently under development call for SA. The implications of each of these issues for the design of headgear with a combination of these novel facilities. This paper systems, including PVI and automation efforts, are discussed. reviews the recent history of such helmet systems, which Author demonstrate admirably the inventiveness of the design teams. However, there are attendant perceptual and operational concerns N93-28864# Royal Air Force Inst. of Aviation Medicine, and the addition of extra components invariably compromises basic Farnborough (England). ergonomic qualities. A new design philosophy, which emphasizes OPERATOR AND AUTOMATION CAPABILITY ANALYSIS: functional integration rather than the incorporation of compatible PICKING THE RIGHT TEAM sub-systems, is emerging. This will be assisted significantly when R. M. TAYLOR and S. J. SELCON In AGARD, Combat Automation key optical and electro-optical technologies become mature. for Airborne Weapon Systems: Man/Machine Interface Trends and Author (revised) Technologies 17 p Apr. 1993 Copyright Avail: CASI HC A03/MF A03 N93-28861# Royal Air Force Inst. of Aviation Medicine, A review of the role of operator and automation capability Farnborough (England). Biodynamics Div. analysis in aircrew systems design is provided. The changing THE PHYSIOLOGICAL LIMITATIONS OF MAN IN THE HIGH G perceptions of human and machine functionality with increasing ENVIRONMENT machine capability, from early pilot-in-the-loop control, through to N. D. C. GREEN In AGARD, Combat Automation for Airborne the division and sharing of responsibilities for systems management Weapon Systems: Man/Machine Interface Trends and and mission problem solving, are charted. Concepts for the Technologies 8 p Apr. 1993 integration of human and machine resources in the performance Copyright Avail: CASI HC A02/MF A03 of physical and cognitive tasks, including decision-making, are The physiological limitations imposed upon man by the high-G discussed in the context of developments in machine intelligence. environment are discussed, with particular reference to the Operator capability and task analysis, and the modeling of human cardiovascular, respiratory, and musculo-skeletal systems. Anti-G performance, are seen to have developed from providing tools for technology has been developed specifically for agile fighter aircraft, system design, to giving critical support for real-time dynamic but it is apparent that if man is to have the capacity to tolerate function allocation in advanced adaptive systems. A model of any further increases in aircraft agility, a radically different approach cooperative teamwork, with the machine conceived of as an to G protection is required. The most effective physiological solution electronic-crew teaming resource, is proposed as broad framework is to change the orientation of the pilot such that his long axis is for thinking about future adaptive systems requirements. The results no longer in the plane of greatest acceleration, entailing major of a recent study of human-electronic crew teamwork with RAF cockpit redesign. This and other solutions are examined, and their Harrier and Tornado aircrew are reported. The results provide acceptability to aviators is considered. Author (revised) evidence for the validity of the teamwork model, and indicate directions for extending the capability for cooperative functioning N93-28862# British Aerospace Public Ltd. Co., Bristol (England). in future aircrew adaptive systems. Author (revised) Research Centre. OCULO-MOTOR RESPONSES AND VIRTUAL IMAGE N93-28865# Aerospace Medical Research Labs., DISPLAYS Wright-Patterson AFB, OH. Human Engineering Div. G. K. EDGAR, C. NEARY, I. CRAIG, and J. C. D. POPE In COGNITIVE INTERFACE CONSIDERATIONS FOR AGARD, Combat Automation for Airborne Weapon Systems: INTELLIGENT COCKPITS Man/Machine Interface Trends and Technologies 8 p Apr. ROBERT G. EGGLESTON In AGARD, Combat Automation for 1993 Airborne Weapon Systems: Man/Machine Interface Trends and Copyright Avail: CASI HC A02/MF A03 Technologies 16 p Apr. 1993 Virtual image displays are likely to become more prominent in Copyright Avail: CASI HC A03/MF A03 the cockpit, the most common examples being the head-up display The concept of an Intelligent Cockpit as a knowledge-based (HUD) and, more recently, the helmet-mounted display (HMD). aiding system is presented. It argues that, in order to maximally This paper describes a series of experiments highlighting some of support the air crew, user aiding in two areas is required: mission the advantages and disadvantages of displays of this type. The task aiding and interface useability aiding. These areas of aiding first experiments demonstrate that introducing perceived depth are discussed in relation to four different forms of an intelligent differences into displays may improve eye-tracking performance. cockpit. The central purpose, however, is to introduce the concept The second series of experiments illustrates some of the problems of a cognitive design requirement for aiding systems, and to suggest

319 54 MAN/SYSTEM TECHNOLOGY AND LIFE SUPPORT

its importance to design solutions expected to achieve crew aiding well beyond conventional aircraft stall limits. Such poststall in both the mission task and interface useability areas. Two maneuvering (PST) can dramatically increase an aircraft's turn arguments are made: (1) A deeper knowledge of human capabilities rate while simultaneously minimizing its turn radius, providing a and limitations is needed to generate effective cognitive design significant tactical advantage in close in air combat. Comparisons requirements for an aiding system; and (2) more cognitive design with all-digital (computer-in- the-loop) simulations under the same requirements are needed for an intelligent cockpit in comparison test conditions, however, show that the combat effectiveness of with a conventional one. Illustrations of possible cognitive design PST is consistently greater within the all-digital analyses than within requirements are presented in support of these arguments. Special the all-manned analyses. These comparisons are summarized and attention is given to requirements that derive from human whether pilots may require supplemental assistance in order to capabilities and limitations. Based on the general discussion, it is exploit the full potential of PST utility is considered. Through also concluded that an intelligent cockpit should be a separate analysis of both man- and computer-in-the-loop combat simulations, module from the traditional systems avionics, since it requires a requirements for pilot assistance were tentatively identified, along unique process architecture. Author (revised) with some of the methods applicable to meeting these requirements. These methods include expanded training, improved N93-28866# British Aerospace Public Ltd. Co., displays, and increased automation. The results of this analysis, Kingston-upon-Thames (England). Military Aircraft Div. based upon the studies available to date, are presented. Plans ERGONOMIC DEVELOPMENT OF DIGITAL MAP DISPLAYS for further analysis and validation studies are described. ADRIAN MARTEL and GEORGE A. WARD In AGARD, Combat Author (revised) Automation for Airborne Weapon Systems: Man/Machine Interface Trends and Technologies 8 p Apr. 1993 N93-28872# National Aerospace Lab., Amsterdam Copyright Avail: CASI HC A02/MF A03 (Netherlands). In the high workload environment of the cockpit, the importance OVERVIEW OF COCKPIT TECHNOLOGY RESEARCH AND of efficient transfer of information from visual displays to the pilot DEVELOPMENT PROGRAMS FOR IMPROVEMENT OF THE is of the highest priority. British Aerospace, Kingston, has developed MAN/MACHINE INTERFACE: REVIEW OF THE AGARD AVP a prototype Situational Awareness display which successfully SYMPOSIUM HELD IN MADRID, MAY 1992 combines tactical information with a digital map and aeronautical P. J. M. URLINGS and E. W. PIJPERS In AGARD, Combat information. The interface in terms of presentation and functionality Automation for Airborne Weapon Systems: Man/Machine Interface is designed to complement the process whereby visual information Trends and Technologies 12 p Apr. 1993 is cognitively integrated into mental models of Situational Copyright Avail: CASI HC A03/MF A03 Awareness by the user. The development of the display involved A review of the AGARD Avionics Panel (AVP) symposium on a comprehensive literature search on perception and cognition, 'Advanced Aircraft Interfaces: The Machine Side of the analysis of map representations, and an iterative evaluation Man-Machine Interface', held in May 1992 at Madrid is provided. whereby successive prototypes were developed and refined. The The theme of this symposium was limited to the 'machine-side' many visual design principles which were identified during this since a subsequent AGARD symposium at Edinburgh, Scotland, work which were successfully incorporated into this display and later that year was scheduled to cover the 'man-side' of the subject. which may in addition be of great benefit to other displays are The main findings of the Madrid symposium were summarized for detailed. Where displays are being radically revised, a holistic presentation in Edinburgh. The complete text of the papers of the redesign from first principles is preferable to simply adding new AVP symposium can be found in AGARD Conference Proceedings features. Author (revised) CP-521. Author (revised)

N93-28867# Wright Lab., Wright-Patterson AFB, OH. N93-28884# Army Research Inst. of Environmental Medicine, SYSTEM AUTOMATION AND PILOT-VEHICLE-INTERFACE Natick, MA. FOR UNCONSTRAINED LOW-ALTITUDE NIGHT ATTACK BIOPHYSICAL MODEL FOR HANDWEAR INSULATION T. O. CHURCH and W. S. BENNETT, II (General Dynamics Corp., TESTING Fort Worth, TX.) In AGARD, Combat Automation for Airborne W. R. SANTEE, L A. BLANCHARD, S. K. CHANG, and R. R. Weapon Systems: Man/Machine Interface Trends and GONZALEZ Mar. 1993 26 p Technologies 7 p Apr. 1993 (AD-A262926; USARIEMT7-93) Avail: CASI HC A03/MF A01 Copyright Avail: CASI HC A02/MF A03 Biophysical models of hands, feet, and full manikins are used Unconstrained low-altitude night attack is achievable today for direct measurement of clothing insulation. Thermal resistance through automation and integration of current technologies. Many values (m(sup 2)K/W) were measured with a weather resistant of these technologies are advanced avionic systems that still and simplified 7 zone hand model with upgraded controls and require additional development before they are production-ready. then compared to values from a 22 zone articulated copper model. However, their performance and synergistic benefits have been Insulation is calculated from the power demand required to maintain demonstrated. Additional efforts are still warranted to increase a selected surface temperature setpoint at known thermal gradient system safety, improve Situational awareness, decrease pilot between the surface setpoint and the environment. For the new workload, and provide a more effective weapon system. Author model, dry insulation values were 0.21 m(sup 2)K/W for the standard military trigger finger mitten and 0.12 m(sup 2)K/W for N93-28870# Rockwell International Corp., Los Angeles, CA. the light-duty shell. Values for the 22 section copper hand model REQUIREMENTS FOR PILOT ASSISTANCE IN A were 0.23 and 0.14 m(sup 2)K/W, respectively. Both hand models THRUST-VECTORING COMBAT AIRCRAFT provide replicable measurements of relative total handwear EMILY HOWARD and ROBERT E. BITTEN In AGARD, Combat insulation. DTIC Automation for Airborne Weapon Systems: Man/Machine Interface Trends and Technologies 15 p Apr. 1993 N93-28897# Oxford Univ. (England). Robotics Research (Contract N00019-88-C-0288) Group. Copyright Avail: CASI HC A03/MF A03 A MODULAR HEAD/EYE PLATFORM FOR REAL-TIME With the emergence of thrust-vectoring aircraft such as the REACTIVE VISION X-31 and F-22, new questions arise regarding the maximum IAN D. REID, PAUL M. SHARKEY, PHILIP F. MCLAUCHLAN, and potential of this technology for increasing air-to-air combat DAVID W. MURRAY 1992 12 p effectiveness. Recent dome-to-dome (man-in-the-loop) simulations (OUEL-1941/92; ETN-93-93877) Avail: CASI HC A03/MF A01 have demonstrated a significant increase in close-in air combat The design and implementation of a high speed reactive system effectiveness with the addition of thrust vector capability. Much of in which the primary sense is vision are presented. An architecture this increased effectiveness can be attributed to the ability of the for visual processing based around a configurable network of thrust-vectoring aircraft to continue maneuvering while operating general purpose processors is described. A purpose built, versatile,

320 54 MAN/SYSTEM TECHNOLOGY AND LIFE SUPPORT high quality engineered mount based on geared DC motors was prolonged, continuous exposure. Designing hardware to accomplish developed to facilitate rapid redirection of gaze. Performance this has traditionally required extensive testing to characterize and results for this device are presented. Results for a preliminary select appropriate control technologies. Data collected since the implementation of closed loop visual control using a brightest spot Apollo project can now be used in a computerized performance detector are given. ESA simulation to predict the performance and life of contamination control hardware to allow for initial technology screening, N93-28941# Army Research Lab., Aberdeen Proving Ground, performance prediction, and operations and contingency studies MD. to determine the most suitable hardware approach before specific A STUDY OF THE EFFECTS OF LENS FOCAL LENGTH ON design and testing activities begin. The program, written in REMOTE DRIVER PERFORMANCE Final Report FORTRAN 77, provides contaminant removal rate, total mass MONICA M. GLUMM, PATRICIA W. KILDUFF, and AMY S. removed, and per pass efficiency for each control device for MASLEY Nov. 1992 35 p discrete time intervals. In addition, projected cabin concentration (Contract DA PROJ. 1L1-62716-AH-70) is provided. Input and output data are manipulated using (AD-A263191; ARL-TR-25) Avail: CASI HC A03/MF A01 commercial spreadsheet and data graphing software. These results The effects of three lens focal lengths on remote driving can then be used in analyzing hardware design parameters such performance were measured. The three focal lengths and their as sizing and flow rate, overall process performance and program corresponding horizontal fields of view (FOV's) were 12 mm (29 economics. Test performance may also be predicted to aid test deg), 6 mm (55 deg), and 3.5 mm (94 deg). On-board driving design. Author performance (direct view) was also measured. The study was conducted on an indoor test course consisting of six segments: straightaways, right-hand turns, left-hand turns, serpentine, figure N93-29044*# National Aeronautics and Space Administration. 8, and obstacle avoidance. The findings are presented. DTIC Lyndon B. Johnson Space Center, Houston, TX. ANTHROPOMETRIC DATA FROM LAUNCH AND ENTRY SUITED TEST SUBJECTS FOR THE DESIGN OF A N93-28942# Edgerton, Germeshausen and Grier, Inc., Idaho Falls, ID. RECUMBENT SEATING SYSTEM LARA E. STOYCOS (Lockheed Engineering and Sciences Co., CRUCIAL ROLE OF DETAILED FUNCTION, TASK, TIMELINE, Houston, TX.) and GLEN K. KLUTE Jun. 1993 29 p LINK, AND HUMAN VULNERABILITY ANALYSES IN HRA (Contract NAS9-17900) T. G. RYAN, L. N. HANEY, and L T. OSTROM 1992 20 p (NASA-TM-104769; S-720; NAS 1.15:104769) Avail: CASI HC Presented at the Reliability and Maintainability Symposium, Atlanta, GA, 26-28 Jun. 1993 A03/MF A01 Returning space crews to Earth in a recumbent position requires (Contract DE-AC07-76ID-01570) the design of a new seating system. Current anthropometric data (DE93-001923; EGG-M-92402; CONF-930661-1) Avail: CASI HC are based on measurements taken while the subjects were unsuited A03/MF A01 and sitting. To be most accurate, it is necessary to design by This paper addresses one major cause for large uncertainties measurements of subjects in the launch and entry suit in a in human reliability analysis (HRA) results, that is, an absence of recumbent position. Since the design of the recumbent seating detailed function, task, timeline, link, and human vulnerability system must meet the requirements of both 5th percentile Japanese analyses. All too often this crucial step in the HRA process is female and 95th percentile American male crew members, a delta done in a cursory fashion using word of mouth or written procedures is reported rather than absolute measurements of the test subjects. which themselves may incompletely or inaccurately represent the This delta is the difference in the measurements taken with the human action sequences and human error vulnerabilities being subjects unsuited and sitting and those taken with the subjects analyzed. The paper examines the potential contributions these suited and recumbent. This delta, representative of the change detailed analyses can make in achieving quantitative and qualitative due to the suit, can be added to the existing Man-Systems HRA results which are as follows: (1) creditable, that is, minimize Integration Standards (NASA-STD-3000) anthropometric data to uncertainty; (2) auditable, that is, systematically linking quantitative project the measurements for 5th percentile Japanese female and results and qualitative information from which the results are 95th percentile American male crew members. A delta accounting derived; (3) capable of supporting root cause analyses on human for the spinal elongation caused by prolonged exposures to reliability factors determined to be major contributors to risk; and microgravity is added as well. Both unpressurized and pressurized (4) capable of repeated measures and being combined with similar suit conditions are considered. Background information, the test results from other analyses to examine HRA issues transcending protocol and procedure, analysis of the data, and recommendations individual systems and facilities. Based on experience analyzing are reported. Author (revised) test and commercial nuclear reactors, and medical applications of nuclear technology, an iterative process is suggested for doing detailed function, task, timeline, link and human vulnerability N93-29324*# National Aeronautics and Space Administration. analyses using documentation reviews, open-ended and structured Lyndon B. Johnson Space Center, Houston, TX. interviews, direct observations, and group techniques. Finally, the ANTHROPOMETRIC SURVEY OF THE ASTRONAUT paper concludes that detailed analyses done in this manner by APPLICANTS AND ASTRONAUTS FROM 1985 TO 1991 knowledgeable human factors practitioners, can contribute SUDHAKAR L. RAJULU (Lockheed Engineering and Sciences Co., significantly to the credibility, auditability, causal factor analysis, Houston, TX.) and GLENN K. KLUTE May 1993 96 p and combining goals of the HRA. DOE (Contract NAS9-17900) (NASA-RP-1304; S-718; NAS 1.61:1304) Avail: CASI HC N93-28977*# National Aeronautics and Space Administration. A05/MF A01 Marshall Space Flight Center, Huntsville, AL. The Anthropometry and Biomechanics Laboratory at the COMPUTERIZED ATMOSPHERIC TRACE CONTAMINANT Johnson Space Center has been collecting anthropometric data CONTROL SIMULATION FOR MANNED SPACECRAFT from astronaut applicants since 1977. These anthropometric J. L. PERRY Jun. 1993 171 p Sponsored by NASA, measurements had been taken from 473 applicants. Based on Washington the position they applied for, these applicants were classified as (NASA-TM-108409; NAS 1.15:108409) Avail: CASI HC A08/MF either mission specialists, payload specialists, pilots, or observers. A02 The main objective was to document the variations among these Buildup of atmospheric trace contaminants in enclosed volumes applicants and tabulate the percentile data for each anthropometric such as a spacecraft may lead to potentially serious health dimension. The percentile and the descriptive statistics data were problems for the crew members. For this reason, active control tabulated and graphed for the whole astronaut candidate methods must be implemented to minimize the concentration of population; for the male and female groups; for each subject atmospheric contaminants to levels that are considered safe for classification such as pilot, mission specialist, and payload

321 54 MAN/SYSTEM TECHNOLOGY AND LIFE SUPPORT specialist; and finally, for those who were selected as astronauts. Author (revised)

N93-29340# Mitre Corp., Bedford, MA. HEAD MOUNTED DISPLAYS FOR VIRTUAL REALITY PAUL J. HEZEL and HARRY VERON Feb. 1993 49 p (Contract F19628-89-C-0001) (AD-A263498; MTR-93B0000015) Avail: CASI HC A03/MF A01 One of the goals in the development of Virtual Reality (VR) is to achieve total immersion where one sees and interacts with objects in a virtual world in the same way that one sees and interacts with the objects of the real world. One becomes immersed in another world through the sense of sight. Thus the technique of displaying a virtual environment determines, in part, the degree to which one can become transported out of the real world and into the virtual world. The developers of VR have utilized the head mounted display (HMD) as a means of displaying the virtual environment to the user. The HMD is not new but has seen widespread use as an information display in military aircraft. In an HMD, displays and imaging optics mounted on a headset provide a virtual image in front of the eyes. In the VR domain, this design provides the user with a view of the virtual environment while blocking out the user's real environment. A tracking device allows the computer to present a viewpoint corresponding to the user's head position and orientation, thus enabling freedom of movement for the user within the virtual environment. These and other characteristics enhance the total immersion capabilities of the HMB. DTIC

55

SPACE BIOLOGY

Includes exobiology; planetary biology; and extraterrestrial life.

N93-28895*# Harvard Univ., Cambridge, MA. WIDE-BANDWIDTH HIGH-RESOLUTION SEARCH FOR EXTRATERRESTRIAL INTELLIGENCE Semiannual Status Report, 15 Dec. 1992-15 Jun. 1993 PAUL HOROWITZ 15 Jun. 1993 26 p (Contract NAGW-2872) (NASA-CR-193137; MAS 1.26:193137) Avail: CASI HC A03/MF A01 Research accomplished during the third 6-month period is summarized. Research covered the following: dual-horn antenna performance; high electron mobility transistors (HEMT) low-noise amplifiers; downconverters; fast Fourier transform (FFT) array; and backend 'feature recognizer' array. CASI

322 SUBJECT INDEX

AEROSPACE MEDICINE AND BIOLOGY / A Continuing Bibliography (Supplement 379) September 1993

Typical Subject Index Listing AERODYNAMIC STALLING AIR QUALITY Requirements for pilot assistance in a thrust-vectoring Microbiology operations and facilities aboard combat aircraft p 320 N93-28870 restructured Space Station Freedom AEROSPACE ENGINEERING [SAE PAPER 921213] p 296 A93-41389 I SUBJECT HEADING 1991 NASA Life Support Systems Analysis workshop First entry operations for spacecraft (NASA-CR-4466] p 310 N93-27100 [SAE PAPER 921384] p 308 A93-41542 1992 NASA Life Support Systems Analysis workshop AIR TO AIR MISSILES [NASA-CR-4467] p 310 N93-27101 Pilot decision aiding for weapon delivery: A novel NERVOUS SYSTEM AEROSPACE ENVIRONMENTS approach to (ire control cueing using parallel computing — Physiological analyses of the aflerents conliollmg Labels and visual cues to reproduce an earthlike p317 N93-28853 brain neurochemica! systems environment in space - Going ahead in designing Columbus AIR TRAFFIC CONTROL [AD-A253185] p 14 N93-11146 APM interior architecture Performance consequences of automation-induced [SAE PAPER 921193] p 295 A93-41371 'complacency' p 286 A93-39571 NASA Specialized Center for Research and Training AIRCRAFT ACCIDENTS (NSCORT) in space environmental health — TITLE Variations in time-to-incapacitation and blood cynanide [SAE PAPER 921358] p 307 A93-41517 values for rats exposed to two hydrogen cyanide gas AEROSPACE MEDICINE Hyperbaric treatment operations aboard Space Station concentrations [DOT/FAA/AM-93-8] p 283 N93-27158 Freedom [SAE PAPER 921142] p 292 A93-41328 Age 60 Project: Consolidated database experiments The subject heading Is a key to the subject content A systems approach to water recovery testing for space [HS-TR-8025-3C(R2>] p314 N93-27851 of the document. The title Is used to provide a descrip- life support - Initial biomedical results from the ECLSS AIRCRAFT CONTROL tion ol the subject matter. When the title Is Insuffi- Water Recovery Test and plans for testbed utilization A study of decision making and performance in rejected ciently descriptive of document content, a title [SAE PAPER 921210] p 295 A93-41386 takeorfs Crew Health Care Systems installations for Space [SAE PAPER 921134] p 287 A93-41322 extension is added, separated from the title by three Station Freedom AIRCRAFT EQUIPMENT hyphens. The accession number and the page num- [SAE PAPER 921249] p 298 A93-41420 Contact lenses in aviation - The Marine Corps ber are Included in each entry to assist the user In NASA Specialized Center for Research and Training experience p 289 A93-41172 locating the abstract In the abstract section. If appli- (NSCORT) in space environmental health New technologies for in-flight pasteless bioelectrodes cable, a report number Is also Included as an aid In [SAE PAPER 921358] p 307 A93-41517 p289 A93-41174 Index of international publications in aerospace Hybrid oxygen system Identifying the document. Under any one subject medicine heading, the accession numbers are arranged In [ AD-A262417 ] p 317 N93-28464 [AD-A262908] p 284 N93-28306 The design and development of the new RAF standard sequence. AEROSPACE SAFETY HUD format p318 N93-28856 EVA and telerobot interaction p 312 N93-27792 AIRCRAFT GUIDANCE AGE FACTOR Head-steered sensor flight test results and Age 60 Project: Consolidated database experiments implications p 318 N93-28859 [HS-TR-8025-3C(R2)l p314 N93-27851 AGING (BIOLOGY) The quest for an integrated flying helmet Influence of aging and practice on piloting tasks p319 N93-28860 p 286 A93-39708 Human capabilities and limitations in situation AIR CONDITIONING EQUIPMENT awareness p319 N93-28863 Manned lunar surface site p 316 N93-26033 AIRCRAFT INSTRUMENTS Lightweight passive microclimate cooling device Instrument-approach-plate design considerations for ABSORBENTS [AD-A262262] p 317 N93-28112 displaying radio frequencies p 289 A93-39574 Portable life support system regenerative carbon dioxide AIR DEFENSE The design and development of the new RAF standard and water vapor removal by metal oxide absorbents Requirements for pilot assistance in a thrust-vectoring HUD format p 318 N93-28856 preprototype hardware development and testing combat aircraft p 320 N93-28870 Cognitive interface considerations for intelligent [SAE PAPER 921299] p 303 A93-41464 AIR FILTERS cockpits p 319 N93-28865 Design of a Shuttle air and water prefilter for reduced Operation of a breadboard AIRCRAFT MANEUVERS gravity operation liquid-sorbent/membrane-contactor system for removing The design and development of the new RAF standard [SAE PAPER 921161] p 294 A93-41343 HUD format p 318 N93-28856 carbon dioxide and water vapor from air Evaluation and optimization of a flexible filtration system AIRCRAFT PILOTS [SAE PAPER 921321 ] p 304 A93-41483 for respiratory protection system 21 Influence of aging and practice on piloting tasks ACCELERATION STRESSES (PHYSIOLOGY) [AD-A262467] p 284 N93-28758 p286 A93-39708 Motion sickness induced by sinusoidal linear AIR FLOW Contact lenses in aviation - The Marine Corps acceleration in rats p 272 A93-39712 Tests characterizing bioprocessor hardware for experience p 289 A93-41172 analytical modeling ACCIDENT PRONENESS Prevalence of corrective lens wear in Royal Australian [SAE PAPER 921357] p 307 A93-41516 Accident proneness: A research review Air Force flight crews p 289 A93-41173 AIR LOCKS [DOT/FAA/AM-93/9] p 288 N93-28622 Age 60 Project: Consolidated database experiments Hyperbaric treatment operations aboard Space Station ACTIVATION [HS-TR-8025-3C(R2)J p314 N93-27851 Freedom Photobiological investigations on spores ol Head-steered sensor flight test results and [SAE PAPER 921142] p 292 A93-41328 streptomyces griseus implications p318 N93-28859 AIR POLLUTION [ESA-TT-1269] p 277 N93-29274 The quest for an integrated flying helmet Space Shuttle crew compartment p 319 N93-28860 ACTIVE CONTROL debris-contamination The physiological limitations of man in the high G Computerized atmospheric trace contaminant control [SAE PAPER 921345] p 305 A93-41504 environment p 319 N93-28861 simulation for manned spacecraft AIR PURIFICATION ALBUMINS [NASA-TM-108409] p 321 N93-28977 Space Shuttle crew compartment Amino acid sequences for the binding regions in serum ACTIVITY (BIOLOGY) debris-contamination albumin proteins 13 C NMR spectra of allosteric effectors of [SAE PAPER 921345] p 305 A93-41504 [NASA-CASE-MFS-28402-1] p 276 N93-289S2 hemoglobin Shuttle Orbiter Environmental Control and Life Support ALERTNESS [AD-A262979] p 284 N93-28293 System - Flight experience Identification of hazardous awareness states in ADAPTATION I SAE PAPER 921348 ] p 305 A93-41507 monitoring environments The prediction of the adaptation of circadian rhythms Air Handling and Atmosphere Conditioning systems for [SAE PAPER 921136] p 287 A93-41324 to rapid time zone changes p 278 A93-39714 manned spacecraft - A design and performance data The use of electrophysiological and cognitive variables The use of electrophysiological and cognitive variables survey in the assessment of degradation during periods of in the assessment of degradation during periods of [SAE PAPER 921350] p 306 A93-41509 sustained wakefulness sustained wakefulness Modeling of membrane processes for air revitalization (AD-A263033) p 283 N93-27923 [AD-A263033] p 283 N93-27923 and water recovery Method of encouraging attention by correlating video Specification of adaptive aiding systems [SAE PAPER 921352] p 306 A93-41511 game difficulty with attention level [AD-A263071] p 314 N93-27927 Manned lunar surface site p 316 N93-28033 [NASA-CASE-LAR-15022-1] p 288 N93-28128

A-1 ALGAE SUBJECT INDEX

ALGAE ATROPHY Performance and mood-state parameters during 30-day Process for selectively recovering algae and protozoa Aminohydroxybutane bisphosphonate and clenbuterol 6 deg head-down bed rest with exercise training [NASA-CASE-MFS-26124-1-NPO] p 276 N93-29174 prevent bone changes and retard muscle atrophy p281 A93-4I169 ALTITUDE ACCLIMATIZATION respectively in tail-suspended rats p 271 A93-39703 BINOCULAR VISION Interactions between Hb, Mg, OPG. ATP. and Cl Absence of a growth hormone effect on rat soleus Performance under dichoptic versus binocular viewing determine the change in Hb-O2 affinity at high altitude atrophy during a 4-day spaceflight p 272 A93-40548 conditions - Effects of attention and task requirements P279 A93-41117 Myosin and troponin changes in rat soleus muscle after p 287 A93-40772 Hypoxic ventilator/ responsiveness in Tibetan compared hindlimb suspension p 273 A93-41124 Visualization and modeling of factors influencing visibility with Han residents of 3,658 m p 280 A93-41120 in computer-aided crewstation design Growth factor involvement in tension-induced skeletal Minimal hypoxic pulmonary hypertension in normal [ SAE PAPER 921135 ] p 292 A93-41323 muscle growth Tibetans at 3.658 m p 280 A93-41121 BIOASSAY [NASA-CR-193023] p 282 N93-27113 ALTITUDE SICKNESS Characterization and classification of strains of High-altitude pulmonary edema with pulmonary ATTENTION Francisella tularensis isolated in the central Asian focus thromboembofism p 278 A93-39709 Cognitive predictors of vigilance p 287 A93-40771 of the Soviet Union and in Japan Long-lasting neuropsychological changes after a single Performance under dichoptic versus binocular viewing [FOA-B-40421-4.4] p 275 N93-28200 high altitude dimb p 278 A93-39713 conditions - Effects of attention and task requirements BIOCHEMISTRY Body fluid compartments, renal blood flow, and p 287 A93-40772 Characterization and classification of strains of hormones at 6,000 m in normal subjects Method of encouraging attention by correlating video Francisella tularensis isolated in the central Asian focus p281 A93-41125 game difficulty with attention level of the Soviet Union and in Japan AMINO ACIDS (NASA-CASE-LAR-15022-1) p 288 N93-28128 [FOA-B-40421-4.4] p 275 N93-28200 Amino acid sequences for the binding regions in serum ATTITUDE (INCLINATION) BIOCONVERSION albumin proteins Symbology for head up and head down applications for Introductions to the Proceedings of the Fourteenth [NASA-CASE-MFS-28402-1 ] p 276 N93-28952 highly agile fighter aircraft: To improve spatial awareness, Symposium on Biotechnology for Fuels and Chemicals AMMONIUM NITRATES trajectory control, and unusual attitude recovery, part 1 [DE93-006235J p 276 N93-28890 Development of the nitrogen fixation system for p318 N93-28857 BIODEGRADATION CELSS ATTITUDE INDICATORS Biodeterioration of materials in water reclamation [SAE PAPER 921238] p 297 A93-41411 Symbology for head up and head down applications for systems AMPHIBIA highly agile fighter aircraft: To improve spatial awareness, [SAE PAPER 921311 ] p 303 A93-41473 Altering the position of the first horizontal cleavage trajectory control, and unusual attitude recovery, part 1 BIODYNAMICS furrow of the amphibian (Xenopus) egg reduces embryonic p318 N93-28857 Development of the Hermes EVA Space Suit Glove survival p 272 A93-39717 AUTOMATIC CONTROL [SAE PAPER 921256] p 299 A93-41426 ANAEROBES The ECLSS advanced automation project evolution and Development of a 500 hPa shoulder joint for the Ferrous iron oxidation by anoxygenic phototrophic technology assessment p 312 N93-27723 European EVA Space Suit System bacteria p 271 A93-39280 [SAE PAPER 921257] p 299 A93-4I427 Combat Automation for Airborne Weapon Systems: Anaerobic treatment of organic wastes from Controlled EVA Glove Research Team Man/Machine Interface Trends and Technologies Ecological Life Support Systems [NASA-CR-193014] p 313 N93-27847 [AGARD-CP-520] p 317 N93-28850 [SAE PAPER 921272] p 301 A93-41442 Anthropometric survey of the astronaut applicants and Operator and automation capability analysis: Picking the ANGULAR VELOCITY right team p 319 N93-28864 astronauts from 1985 to 1991 Symbology for head up and head down applications for [NASA-RP-1304] p 321 N93-29324 System automation and pilot-vehicle-interface for highly agile fighter aircraft: To improve spatial awareness, unconstrained low-altitude night attack BIOELECTRIC POTENTIAL trajectory control, and unusual attitude recovery, part 1 New technologies for in-flight pasteless bioelectrodes p 320 N93-28867 p318 N93-28857 p289 A93-41174 AUTOMATIC PILOTS ANTHROPOMETRY BIOENGINEERING Performance consequences of automation-induced Hazard and risk assessment for surface components Anthropometric data from launch and entry suited test 'complacency' P 286 A93-39571 subjects for the design of a recumbent seating system of a lunar base Controlled Ecological Life Support An exploratory study of plan-view terrain displays for [NASA-TM-104769] p 321 N93-29044 System air carrier operations p 289 A93-39573 Anthropometric survey of the astronaut applicants and [SAE PAPER 921285] p 302 A93-41451 AUTOMATION astronauts from 1985 to 1991 Advanced life support systems in lunar and Martian Flight deck automation and pilot workload [NASA-RP-1304] p321 N93-29324 environments utilizing a higher plant based engineering [SAE PAPER 921132] p 291 A93-41320 ANTIBIOTICS Toward a flight deck automation philosophy for the paradigm Effects of refrigerating preinoculated Vitek cards on [SAE PAPER 921286] p 302 A93-41452 Boeing High Speed Civil Transport microbial physiology and antibiotic susceptibility [SAE PAPER 921133] p 291 A93-41321 BIOLOGICAL EFFECTS [SAE PAPER 921214] p 273 A93-41390 Gene transcription and electromagnetic fields AVIATION PSYCHOLOGY [DE93-010854] p 276 N93-28848 ANTIINFECTIVES AND ANTIBACTERIALS Influence of aging and practice on piloting tasks BIOLOGICAL EVOLUTION Relative resistance of biofilms and planktonic cells of p286 A93-39708 common molds and yeasts to antimicrobials Microfossils of the Early Archean Apex chert - New AVIONICS evidence of the antiquity of life p 272 A93-40308 [SAE PAPER 921212] p 273 A93-41388 Performance consequences of automation-induced ANTISEPTICS 'complacency' P 286 A93-39571 BIOLOGICAL MODELS (MATHEMATICS) Regenerate biocide delivery unit, volume 1 Mathematical model for the exchange of gases in the [NASA-CR-185701] p 274 N93-27122 lungs with special reference to carbon monoxide APPROACH B p271 A93-39707 The effect of geometric field of view and tunnel design Computer modeling of the Variable Pressure Growth for perspective flight-path displays BACTERIA Chamber using the CASE/A simulation package [SAE PAPER 921131) p 291 A93-41319 Ferrous iron oxidation by anoxygenic phototrophic [SAE PAPER 921354] p 306 A93-41513 ARCHITECTURE (COMPUTERS) bacteria P 271 A93-39280 Plant growth modeling at the JSC variable pressure Combat Automation for Airborne Weapon Systems: Microfossils of the Early Archean Apex chert - New growth chamber - An application of experimental design Man/Machine Interface Trends and Technologies evidence of the antiquity of life p 272 A93-40308 [SAE PAPER 921356] p 307 A93-41515 [AGAROCP-520] p317 N93-28850 Intracellular targeting of the Yersinia YopE cytotoxin in EVA Glove Research Team ARTIFICIAL INTELLIGENCE mammalian cells induces actin microfilament disruption [NASA-CR-193014] p 313 N93-27847 Operator and automation capability analysis: Picking the [FOA-B-40420-4.4] p 275 N93-27989 Comparative mutagenesis of human cells in vivo and right team p 319 N93-28864 Plasmid encoded virulence of Yersinia in vitro Cognitive interface considerations for intelligent [FOA-B-40419-4.4] p 275 N93-28199 [DE93-012269] p 276 N93-28651 cockpits p319 N93-28865 Characterization and classification of strains of Sudden loading and fatigue effects on the human ASTRONAUT LOCOMOTION Francisella tularensis isolated in the central Asian focus spine A study to explore locomotion patterns in partial gravity of the Soviet Union and in Japan [PB93-167526] p 286 N93-29199 environments [FOA-B-40421-4.4J p 275 N93-28200 BIOMASS [SAE PAPER 921157] p 293 A93-41340 Use of RNA hybridization in the diagnosis of a case of Introductions to the Proceedings of the Fourteenth ASTRONAUT TRAINING ulceroglandular tularemia Symposium on Biotechnology for Fuels and Chemicals NASA Specialized Center for Research and Training [FOA-B-40422-4.4] p 275 N93-28212 [DE93-006235] p 276 N93-28890 (NSCORT) in space environmental health Regulation of alternative CO2 fixation pathways in BIOMASS ENERGY PRODUCTION [SAE PAPER 921358] p 307 A93-41517 procaryotic and eucaryotic photosynthetic organisms Biomass productivity and sustainability of a ASTRONAUTS [DE93-012109] p276 N93-29181 bioregenerative life-support system Anthropometric survey of the astronaut applicants and BACTERICIDES [SAE PAPER 921359] p 307 A93-41518 astronauts from 1985 to 1991 Continuous monitoring of effluent iodine levels of Space BIOPHYSICS [NASA-RP-1304] p 321 N93-29324 Station water using solid state technology Gene transcription and electromagnetic fields ATMOSPHERIC COMPOSITION [SAE PAPER 921265) p 299 A93-41435 [DE93-010854] p 276 N93-28848 Biosphere 2 - Overview of system performance during BARORECEPTORS Biophysical model for handwear insulation testing the first nine months Response of genioglossus EMG activity to passive tilt [AD-A262926] p 320 N93-28884 [SAE PAPER 921129] p 291 A93-41317 in men P 279 A93-41118 BIOPROCESSING Pressure, composition, and temperature control of cabin BAROTRAUMA Tests characterizing bioprocessor hardware for atmosphere on Space Station Freedom Barotrauma in Boeing 737 cabin crew analytical modeling [SAE PAPER 921216] p 296 A93-41392 p 278 A93-39706 [SAE PAPER 921357] p 307 A93-41516 ATMOSPHERIC PRESSURE BED REST BIOREACTORS Pressure, composition, and temperature control of cabin Orthostatic intolerance during a 13-day bed rest does Immobilized cell bioreactors for water reclamation - atmosphere on Space Station Freedom not result from increased leg compliance Process stability and effect of reactor design [SAE PAPER 821216] p 296 A93-41392 p280 A93-41119 [SAE PAPER 921277] P 301 A93-41446

A-2 SUBJECTINDEX CLOSED ECOLOGICAL SYSTEMS

BIOSPHERE CANOPIES (VEGETATION) Response of genioglossus EMG activity to passive tilt Biosphere 2 - Overview of system performance during Plant canopy transpiration in bioregenerative life support in men p 279 A93-41118 the first nine months systems - The link between mechanistic and empirical CAROTID SINUS REFLEX [SAE PAPER 9211291 p 291 A93-41317 models Response of genioglossus EMG activity to passive tilt Closed ecological systems: From test tubes to Earth's [SAE PAPER 921355] p 306 A93-41514 in men p 279 A93-41118 biosphere p315 N93-27976 CANTILEVER BEAMS CATHODE RAY TUBES BIOTECHNOLOGY A preliminary structural analysis of space-based Low-cost helmet-mounted displays New technologies for in-flight pasteless bioelectrodes inflatable tubular frame structures p313 N93-27849 [AD-A262616] p317 N93-28479 p289 A93-41174 CAPILLARIES (ANATOMY) CELL DIVISION Immobilized cell bioreactors for water reclamation - Direct measurement of capillary blood pressure in the Altering the position of the first horizontal cleavage Process stability and effect of reactor design human lip p 279 A93-40550 furrow of the amphibian (Xenopus) egg reduces embryonic [SAE PAPER 9212771 p 301 A93-41446 CAPILLARY FLOW survival P 272 A93-39717 Evaluation of capillary electrophoresis for in-flight ionic Proceedings of a Workshop on Molecular Nuclear CELLS (BIOLOGY) contaminant monitoring of SSF potable water Medicine Comparative mutagenesis of human cells in vivo and [SAE PAPER 921268) p 300 A93-41438 [DE93-010828J p 285 N93-2883S CARBOHYDRATE METABOLISM in vitro [DE93-012269] P 276 N93-28651 BLOOD Influence of the Cold Buster (tm) sports bar on heat Toxicokinetics of inhaled bromotrifluoromethane (Halon debt, mobilization and oxidation of energy substrates CENTRAL NERVOUS SYSTEM 1301) in human subjects p 278 A93-39705 [AD-A262762] p 285 N93-28939 Secondary injury factors and preventative treatment 13 C NMR spectra of allosteric effectors of CARBON [PB93-176014] p283 N93-27409 hemoglobin Determination of organic carbon and ionic accountability CENTRIFUGAL FORCE [AD-A262979] p 284 N93-28293 of various waste and product waters derived from ECLSS The Centrifuge Facility Life Sciences Glovebox BLOOD PRESSURE water recovery tests and Spacelab humidity condensate configuration study Direct measurement of capillary blood pressure in the [SAE PAPER 921313] p 303 A93-41475 [SAE PAPER 921158] p 293 A93-41341 human lip p 279 A93-40550 CARBON DIOXIDE CENTRIFUGAL PUMPS BLOWERS Regulation of alternative CO2 fixation pathways in Effects of air bubble contamination in recirculating water Development of the carbon dioxide removal system procaryotic and eucaryotic photosynthetic organisms loop blower used on Space Station Freedom [DE93-012109] p 276 N93-29181 [SAE PAPER 921282] p 302 A93-41450 [SAE PAPER 921188] p 294 A93-41367 Growing wheat to maturity in reduced gas pressures CEREBRAL CORTEX BODY FLUIDS [NASA-CR-193245] p 277 N93-29216 Oxygen regime in the frontal cerebral cortex of monkeys Body fluid compartments, renal blood flow, and CARBON DIOXIDE CONCENTRATION during a two-week space flight p 272 A93-40773 hormones at 6,000 m in normal subjects Recent regenerative ECLSS technology developments CHEMICAL COMPOSITION p281 A93-41125 in Europe The development of an atmosphere composition monitor BODY TEMPERATURE [SAE PAPER 921332] p 304 A93-41493 for the Environmental Control and Life Support System Influence of the Cold Buster (tm) sports bar on heat Plant growth modeling at the JSC variable pressure [SAE PAPER 921149] p 292 A93-41333 debt, mobilization and oxidation of energy substrates growth chamber - An application of experimental design CHEMICAL EQUILIBRIUM [AD-A262762] p 285 N93-28939 [SAE PAPER 921356] p 307 A93-41515 Regenerable biocide delivery unit, volume 2 BOEING AIRCRAFT CARBON DIOXIDE REMOVAL [NASA-CR-185701-VOL-2] p 275 N93-27360 Toward a flight deck automation philosophy for the Development of the carbon dioxide removal system CHEMOTHERAPY Boeing High Speed CM Transport blower used on Space Station Freedom Secondary injury factors and preventative treatment [SAE PAPER 921133] p 291 A93-41321 [SAE PAPER 921188] p 294 A93-41367 [PB93-176014] p283 N93-27409 BOEING 737 AIRCRAFT Sabatier carbon dioxide reduction system for Space CIRCADIAN RHYTHMS Barotrauma in Boeing 737 cabin crew Station Freedom The prediction of the adaptation of circadian rhythms p 278 A93-39706 [SAE PAPER 921189] p 294 A93-41368 to rapid time zone changes p 278 A93-39714 BONES Comparative test data assessment and simplified math CIVIL AVIATION Aminohydroxybutane bisphosphonate and clenbuterol modelling for Sabatier CO2 reduction subsystem Toward a flight deck automation philosophy for the prevent bone changes and retard muscle atrophy [SAE PAPER 921228] p 296 A93-41402 Boeing High Speed Civil Transport respectively in tail-suspended rats p 271 A93-39703 Evaluation of the carbon dioxide removal assembly [SAE PAPER 921133] p 291 A93-41321 requirements for the Space Station Freedom in the Manned BOXES CLINICAL MEDICINE Glovebox design for Space Station Freedom Crew Tended Capability through Permanently Manned Capability New technology for the analysis of the results of an Health Care System configurations ultrasound experiment performed in aviation-medicine [SAE PAPER 921139] p 292 A93-41326 [SAE PAPER 921231] p 297 A93-41405 medical examination p 279 A93-40774 Development of a regenerate metal oxide sheet matrix BRAIN Hyperbaric treatment operations aboard Space Station CO2 removal system Analysis of neural systems involved in modulation of Freedom memory storage [SAE PAPER 921298] p 302 A93-41463 [SAE PAPER 921142] p 292 A93-41328 Portable life support system regenerative carbon dioxide [AD-A262418] p 283 N93-27654 DOKMA: A document oriented communication model BRAIN CIRCULATION and water vapor removal by metal oxide absorbents for medical applications as a basis of a role system in preprototype hardware development and testing Oxygen regime in the frontal cerebral cortex of monkeys the medical field during a two-week space flight p 272 A93-40773 [SAE PAPER 921299] p 303 A93-41464 [ETN-93-93799] P 284 N93-28469 Operation of a breadboard Cerebral blood velocity and other cardiovascular Proceedings of a Workshop on Molecular Nuclear liquid-sorbent/membtane-contactor system for removing responses to 2 days of head-down tilt Medicine p280 A93-41122 carbon dioxide and water vapor from air [DE93-010828] p 285 N93-28835 BRAIN DAMAGE [SAE PAPER 921321] p 304 A93-41483 CLOSED ECOLOGICAL SYSTEMS Technologies for ECLSS evolution Long-lasting neuropsychological changes after a single Recycling and source reduction for long duration space p311 N93-27720 high altitude climb p 278 A93-39713 habitation Secondary injury factors and preventative treatment JSC ECLSS R/T program overview [SAE PAPER 921121] p 290 A93-41313 [PB93-176014] p283 N93-27409 p312 N93-27725 Analysis of the Variable Pressure Growth Chamber using CARBON MONOXIDE BREATHING APPARATUS the CASE/ A simulation package Mathematical model for the exchange of gases in the Comparison of portable crewmember protective [SAE PAPER 921122] p 291 A93-41314 lungs with special reference to carbon monoxide breathing equipment (CPBE) designs Biosphere 2 - Overview of system performance during p 271 A93-39707 [DOT/FAA/AM-93/6] p 310 N93-27121 the first nine months BROADBAND AMPLIFIERS Variations of time-to-incapacitation and [SAE PAPER 921129] p 291 A93-41317 carboxyhemoglobin values in rats exposed to two carbon Wide-bandwidth high-resolution search for Crop interactions in polyculture and their implications extraterrestrial intelligence monoxide concentrations for CELSS design [DOT/FAA/AM-93/7] p 274 N93-27152 [NASA-CR-193137] p 322 N93-28895 I SAE PAPER 921197] p 295 A93-41373 CARBON MONOXIDE POISONING BROMINE COMPOUNDS A trade study method for determining the design Variations of time-to-incapacitation and Human performance and physiological function during parameter of CELSS subsystems carboxyhemoglobin values in rats exposed to two carbon a 24-hr exposure to 1 percent bromotrifluoromethane [SAE PAPER 921198] p 295 A93-41374 (Halon 1301) p 277 A93-39704 monoxide concentrations An approach to the functional optimization of the CELSS [DOT/FAA/AM-93/7] p 274 N93-27152 Test Facility CARCINOGENS [SAE PAPER 921199] P 295 A93-41375 Gene transcription and electromagnetic llelds European involvement in CELSS - Definition of a Closed [DE93-010854] p 276 N93-28848 Ecological Systems Test Bed CABIN ATMOSPHERES CARDIOVASCULAR SYSTEM [SAE PAPER 921200] p 295 A93-41376 Initial accomplishments of the Environmental Control Norepinephrine content in discrete brain areas and Functions simulation model of integrated regenerable and Life Support System (ECLSS) atmosphere neurohypophysial vasopressin in rats after a 9-d spaceflight life support system revitalization (AR) predevelopment operational system test (SLS-1) p273 A93-41167 [SAE PAPER 921201] p 295 A93-41377 (POST) for the Space Station Freedom (SSF) Effects of dynamic exercise on cardiovascular regulation Microbiological concerns and methodological [SAE PAPER 921186] p 294 A93-41365 during lower body negative pressure approaches related to bacterial water quality in Development of the carbon dioxide removal system p281 A93-41168 spaceflight blower used on Space Station Freedom The physiological limitations of man in the high G [SAE PAPER 921232] p 297 A93-41406 [SAE PAPER 921188] p 294 A93-41367 environment p 319 N93-28861 Development of the nitrogen fixation system for CAMERAS CAROTID SINUS BODY CELSS Dark cycle monitoring of biological specimens on Space Microgravity and orthostatic intolerance - Carotid [SAE PAPER 921238) p 297 A93-41411 Station Freedom hemodynamics and peripheral responses Concept of waste transferring mechanisms [SAE PAPER 921393] p 274 A93-41551 p 278 A93-39716 [SAE PAPER 921239] p 297 A93-41412

A-3 COATINGS SUBJECTINDEX

OCAM - A CELSS modeling tool: Description and results COLLOIDING CONTROL EQUIPMENT — Object-oriented Controlled Ecological Life Support Recovering potable water from wastewater in space 13 C NMR spectra of allosteric effectors of System Analysis and Modeling platforms by lyophilization hemoglobin [SAE PAPER 921241] p 298 A93-41413 | SAE PAPER 921323 ] p 304 A93-41485 [AD-A262979] p 284 N93-28293 Evaluation of capillary electrophoresis for in-flight ionic COLUMBUS SPACE STATION CONTROL SIMULATION contaminant monitoring of SSF potable water Effects of air bubble contamination in recirculating water Virtual interface applications for airborne weapons [SAE PAPER 921268] p 300 A93-41438 loop systems p 318 N93-28858 An assessment of waste processing/resource recovery [SAE PAPER 921282] p 302 A93-41450 Computerized atmospheric trace contaminant control technologies for lunar/Mars life applications Recent regenerative ECLSS technology developments simulation for manned spacecraft [SAE PAPER 921271] p 300 A93-41441 in Europe [NASA-TM-108409] p 321 N93-28977 Anaerobic treatment of organic wastes from Controlled (SAE PAPER 921332] p 304 A93-41493 CONTROL SYSTEMS DESIGN Ecological Life Support Systems COMBAT Pressure, composition, and temperature control of cabin [SAE PAPER 921272] p 301 A93-41442 Combat Automation for Airborne Weapon Systems: atmosphere on Space Station Freedom Biofilm formation and control in a simulated spacecraft Man/Machine Interface Trends and Technologies [SAE PAPER 921216] p 296 A93-41392 water system - Three year results [AGARD-CP-520] p317 N93-28850 Power assist EVA glove development [SAE PAPER 921310] p 303 A93-41472 COMBUSTION PRODUCTS p314 N93-27850 A novel membrane device for the removal of water vapor Variations in Ume-to-incapacitation and blood cynanide Lunar base thermal management/power system and water droplets from air values for rats exposed to two hydrogen cyanide gas analysis and design p 315 N93-27985 [SAE PAPER 921322] p 304 A93-41484 concentrations Plant canopy transpiration in bioregenerative life support [DOT/FAA/AM-93-8] p 283 N93-271S8 CONTROL VALVES systems • The link between mechanistic and empirical COMMUNICATION EQUIPMENT Regenerate biocide delivery unit, volume 1 models Evaluation of test methods and requirements for [NASA-CR-185701] p 274 N93-27122 [SAE PAPER 921355] p 306 A93-41514 respiratory protection systems 21 CONTROLLED ATMOSPHERES Biomass productivity and sustainability of a [AD-A262466] p317 N93-28757 Initial accomplishments of the Environmental Control bioregenerative life-support system COMPRESSION LOADS and Life Support System (ECLSS) atmosphere [SAE PAPER 921359] p 307 A93-41518 Power assist EVA glove development revitalization (AR) predevelopment operational system test Design and preliminary testing of a membrane based [SAE PAPER 921255] p 299 A93-41425 (POST) for the Space Station Freedom (SSF) water recycling system for European manned space COMPUTER AIDED DESIGN [SAE PAPER 921186] p 294 A93-41365 missions Visualization and modeling of factors influencing visibility Space Shuttle Orbiter oxygen partial pressure sensing [ SAE PAPER 921396 ] p 309 A93-41553 in computer-aided crewstation design and control system improvements Hermes ECLSS - Main requirements and technical [SAE PAPER 921135] p 292 A93-41323 [SAE PAPER 921347] p 305 A93-41506 solutions Air Handling and Atmosphere Conditioning systems for CONTROLLERS [SAE PAPER 921400] p 309 A93-41555 manned spacecraft - A design and performance data A modular head/eye platform for real-time reactive Alternative processes for water reclamation and solid survey vision waste processing in a physical/chemical bioregenerative [ SAE PAPER 921350 ] p 306 A93-41509 [OUEL-1941/92] p320 N93-28B97 life support system p311 N93-27721 Computer modeling of the Variable Pressure Growth COOLING SYSTEMS Closed ecological systems: From test tubes to Earth's Chamber using the CASE/A simulation package Space Shuttle crew compartment biosphere p 315 N93-27976 [SAE PAPER 921354] p 306 A93-41513 debris-contamination Assessment of the state of the art in life support COMPUTER GRAPHICS [SAE PAPER 921345] p 305 A93-41504 environmental control for SEI p315 N93-27978 Ergonomic development of digital map displays Lightweight passive microclimate cooling device Dust protection for environmental control and life support p320 N93-28866 [AD-A262262] p317 N93-28112 systems in the lunar environment p 315 N93-27979 COMPUTER STORAGE DEVICES CORIOLIS EFFECT COATINGS DOKMA: A document oriented communication model Process for selectively recovering algae and protozoa Aquatic biofilms and their responses to disinfection and for medical applications as a basis of a role system in [NASA-CASE-MFS-26124-1-NPO] p 276 N93-29174 invading species the medical field [SAE PAPER 921211] p 296 A93-41387 [ETN-93-93799] p 284 N93-28469 COUNTERMEASURES COCKPIT SIMULATORS COMPUTER VISION Program development for exercise countermeasures An exploratory study of plan-view terrain displays for A modular head/eye platform for real-time reactive [SAE PAPER 921140] p 292 A93-41327 air carrier operations p 289 A93-39573 vision CRACKING (CHEMICAL ENGINEERING) COCKPITS [OUEL-1941/92] p 320 N93-28897 Recent regenerative ECLSS technology developments Flight deck automation and pilot workload COMPUTERIZED SIMULATION in Europe [SAE PAPER 921132] p 291 A93-41320 Analysis of the Variable Pressure Growth Chamber using [SAE PAPER 921332] p 304 A93-41493 Toward a flight deck automation philosophy for the the CASE/A simulation package CREATIVITY Boeing High Speed Civil Transport [SAE PAPER 921122] p 291 A93-41314 How expert pilots think: Cognitive processes in expert [SAE PAPER 921133] p 291 A93-41321 The effect of geometric field of view and tunnel design decision making [DOT/FAA/RD-93/9] p 288 N93-27103 Oculo-motor responses and virtual image displays for perspective flight-path displays [SAE PAPER 921131] p 291 A93-41319 p 319 N93-28862 CRETACEOUS-TERTIARY BOUNDARY Computer modeling of the Variable Pressure Growth Geography of end-Cretaceous marine bivalve Cognitive interface considerations for intelligent Chamber using the CASE/A simulation package extinctions p 273 A93-41075 cockpits p 319 N93-28865 [SAE PAPER 921354] p 306 A93-41513 CREW PROCEDURES (INFLIGHT) Ergonomic development of digital map displays Computerized atmospheric trace contaminant control p320 N93-28866 Performance consequences of automation-induced simulation for manned spacecraft 'complacency' p 286 A93-39571 Overview of cockpit technology research and [NASA-TM-108409] p 321 N93-28977 development programs for improvement of the CONFERENCES CREW WORKSTATIONS man/machine interface: Review of the AGARD AVP Proceedings of a Workshop on Molecular Nuclear Visualization and modeling of factors influencing visibility Symposium held in Madrid. May 1992 Medicine in computer-aided crewstation design p 320 N93-28872 [DE93-010828] p 285 N93-28835 [SAE PAPER 921135] p 292 A93-41323 COGNITION Combat Automation for Airborne Weapon Systems: EVA/manned systems p312 N93-27789 Cognitive predictors of vigilance p 287 A93-40771 Man/Machine Interface Trends and Technologies Evolving technologies for Space Station Freedom How expert pilots think: Cognitive processes in expert [AGARD-CP-520] p317 N93-28850 computer-based workstations p313 N93-27794 decision making Introductions to the Proceedings of the Fourteenth CROP GROWTH Symposium on Biotechnology for Fuels and Chemicals [DOT/FAA/RD-93/9] p 288 N93-27103 Crop interactions in polyculture and their implications [DE93-006235] p 276 N93-28890 The use of electrophysiological and cognitive variables for CELSS design CONNECTIVE TISSUE in the assessment of degradation during periods of [ SAE PAPER 921197 ] p 295 A93-41373 sustained wakefulness Wound healing and connective tissue metabolism: The CRYOGENICS [AD-A263033] p 283 N93-27923 role of hyperbaric oxygen therapy [AD-A262483] p 285 N93-28759 Lunar base thermal management/power system Expertise, text coherence, and constraint satisfaction: analysis and design p315 N93-27985 Effects on harmony and settling rate — mental CONSUMABLES (SPACECREW SUPPLIES) Consumables and wastes estimations for the First Lunar representations CUES Outpost [AD-A262703] p 288 N93-28901 Pilot decision aiding for weapon delivery: A novel [SAE PAPER 921287] p 302 A93-41453 approach to fire control cueing using parallel computing COGNITIVE PSYCHOLOGY CONTACT LENSES p317 N93-28853 How expert pilots think: Cognitive processes in expert Contact lenses in aviation - The Marine Corps decision making CULTURE TECHNIQUES experience p 289 A93-41172 Wound healing and connective tissue metabolism: The [DOT/FAA/RD-93/9] p 288 N93-27103 Prevalence of corrective lens wear in Royal Australian Expertise, text coherence, and constraint satisfaction: role of hyperbaric oxygen therapy Air Force flight crews p 289 A93-41173 [AD-A262483] p 285 N93-287S9 Effects on harmony and settling rate — mental CONTAMINATION representations Aquatic biofilms and their responses to disinfection and CYANIDES [AD-A262703] p 288 N93-28901 invading species Variations in time-to-incapacitation and blood cynanide COLO TOLERANCE [SAE PAPER 921211] p 296 A93-41387 values for rats exposed to two hydrogen cyanide gas Influence of the Cold Buster (tm) sports bar on heat Evaluation of capillary electrophoresis for in-flight ionic concentrations debt, mobilization and oxidation of energy substrates contaminant monitoring of SSF potable water [DOT/FAA/AM-93-8] p 283 N93-27158 [AD-A262762] p 285 N93-28939 [SAE PAPER 921268] p 300 A93-41438 CYTOLOGY COLD WEATHER TESTS Biofilm formation and control in a simulated spacecraft Flow cytometric analysis of lymphocyte surface markers Biophysical model for handwear insulation testing water system - Three year results following a 1-Gy dose of gamma radiation [AD-A262926] p 320 N93-28884 [SAE PAPER 921310] p 303 A93-41472 p281 A93-41170

A-4 SUBJECT INDEX EMBOLISMS

DISEASES EARTH ENVIRONMENT Wound healing and connective tissue metabolism: The Labels and visual cues to reproduce an earthlike DATA BASES role of hyperbaric oxygen therapy environment in space - Going ahead in designing Columbus Age 60 Project: Consolidated database experiments [AD-A262483] p 285 N93-28759 APM interior architecture [HS-TR-8025-3C(R2>] P 314 N93-27851 Proceedings of a Workshop on Molecular Nuclear [SAE PAPER 921193] p 295 A93-41371 DOKMA: A document oriented communication model Medicine EARTH ORBITAL ENVIRONMENTS for medical applications as a basis of a role system in [DE93-010828] p 285 N93-28835 Enhanced softgoods structures for spacesuit the medical field Gene transcription and electromagnetic fields micrometeoroid/debris protective systems (ETN-93-93799) P 284 N93-28469 [DE93-010854] p 276 N93-28848 [SAE PAPER 921258] p 299 A93-41428 DISPLAY DEVICES DATA PROCESSING EDEMA An exploratory study of plan-view terrain displays tor Comparative test data assessment and simplified math High-altitude pulmonary edema with pulmonary air carrier operations p 289 A93-39573 modelling foi Sabafe CO2 (eduction subsystem thromboembolism p 278 A93-39709 Instrument-approach-plate design considerations for (SAE PAPER 921228] P 296 A93-41402 EFFLUENTS displaying radio frequencies p 289 A93-39574 Anaerobic treatment of organic wastes from Controlled DOKMA: A document oriented communication model Performance under dichoptic versus binocular viewing for medical applications as a basis of a role system in Ecological Life Support Systems conditions - Effects of attention and task requirements [SAE PAPER 921272] p 301 A93-41442 the medical field p287 A93-40772 [ETN-93-93799] P 284 N93-28469 EGGS The effect of geometric field of view and tunnel design Altering the position of the first horizontal cleavage DATA SYSTEMS for perspective flight-path displays Dark cycle monitoring of biological specimens on Space furrow of the amphibian (Xenopus) egg reduces embryonic [ SAE PAPER 921131 ] p 291 A93-41319 survival p 272 A93-39717 Station Freedom Combat Automation for Airborne Weapon Systems: [SAE PAPER 921393] P 274 A93-41551 Man/Machine Interface Trends and Technologies EJECTION INJURIES DECISION MAKING [AGARD-CP-520] p317 N93-28850 Case report - Chronic sub-dural hematoma following A study of decision making and performance in rejected Pilot intent and error recognition as part of a knowledge high-speed ejection p 282 A93-41171 takeoffs based cockpit assistant p318 N93-288S5 ELASTIC PROPERTIES [ SAE PAPER 921134 ] P 287 A93-41322 The design and development of the new RAF standard Power assist EVA glove development How expert pilots think: Cognitive processes in expert HUD format p318 N93-28856 [SAE PAPER 921255] p 299 A93-41425 decision making Symbology for head up and head down applications for Power assist EVA glove development [DOT/FAA/RD-93/9] P 288 N93-27103 highly agile fighter aircraft: To improve spatial awareness, p314 N93-27850 Specification of adaptive aiding systems trajectory control, and unusual attitude recovery, part 1 ELECTRIC POWER SUPPLIES [AD-A263071] P314 N93-27927 p318 N93-28857 Manned lunar surface site p316 N93-28033 Pilo\ decision aiding 1oi weapon delwer/- m no^al Head-steered sensor (light test cesults and ELECTRO-OPTICS approach to fire control cueing using parallel computing implications p 318 N93-28859 > The quest for an integrated flying helmet p317 N93-28853 Oculo-motor responses and virtual image displays p319 N93-28860 Crucial role of detailed function, task, timeline, link, and p319 N93-28862 ELECTROCHEMISTRY human vulnerability analyses in HRA Ergonomic development of digital map displays Post-treatment of reclaimed waste water based on an [DE93-001923] P 321 N93-28942 p320 N93-28866 electrochemical advanced oxidation process DECISION THEORY Head mounted displays for virtual reality [SAE PAPER 921275] p 301 A93-41444 Theory of signal detection and its application to visual [AD-A263498] p 322 N93-29340 ELECTRODES target acquisition: A review of Ihe literature DISRUPTING New technologies for in-flight pasteless bioelectrodes [AD-A262920] P 288 N93-28307 Intracellular targeting of the Yersinia YopE cytotoxin in p289 A93-41174 DECONTAMINATION mammalian cells induces actin microfilament disruption ELECTROLYSIS Use of sorption technology for treatment of humidity [FOA-B-40420-4.4] p 275 N93-27989 Oxygen generation by static feedwater electrolysis for condensate for potable water DISSOLVED GASES Space Station Freedom [SAE PAPER 921312] P 303 A93-41474 Measurement of free and dissolved gas content of water [SAE PAPER 921151 ] p 293 A93-41335 Defining contamination control requirements for samples on Space Station Freedom Recent regenerative ECLSS technology developments non-human research on Space Station Freedom [SAE PAPER 921267] p 300 A93-41437 in Europe [SAE PAPER 921332] p 304 A93-41493 [SAE PAPER 921386] P 308 A93-41544 DISTILLATION DEGASSING Gray water recycling with a unique vapor compression SPE water electrolyzers in support of the lunar outpost p315 N93-27977 Development of membrane das removal technology for distillation (VCD) design microgravity liquid flow systems [SAE PAPER 921318] p 304 A93-41480 ELECTROLYTE METABOLISM Body ttuid compartments, renat blood flow, and [SAE PAPER 921162] P 294 A93-41344 Water reclamation technology development for future DEHUMIDIFICATION hormones at 6,000 m in normal subjects long range missions p281 A93-41125 Operation of a breadboard [SAE PAPER 921351 ] p 306 A93-41510 liquid-sorbent/membrane-contsictor system for removing ELECTROLYTES Experimental and theoretical study on membrane carbon dioxide and water vapor from air SPE water electrolyzers in support of the lunar distillation using thermopervaporation [SAE PAPER 921321] P 304 A93-41483 outpost p315 N93-27977 [SAE PAPER 921397] p 309 A93-41554 A novel membrane device for the removal of water vapor ELECTROLYTIC CELLS DISTILLATION EQUIPMENT and water droplets from air A low pressure electrolyzer for the next generation [SAE PAPER 921322] P 304 A93-41484 An update on the readiness of vapor compression submarine distillation for spacecraft wastewater processing DEOXYRIBONUCLEIC ACID [SAE PAPER 921125] p 291 A93-41316 Comparative mutagenesis of human cells in vivo and [SAE PAPER 921114] p 290 A93-41307 ELECTROMAGNETIC FIELDS in vitro DOWN-CONVERTERS Gene transcription and electromagnetic fields [DE93-012269] P 276 N93-28651 Wide-bandwidth high-resolution search for [DE93-010854] p 276 N93-28848 DESIGN ANALYSIS extraterrestrial intelligence ELECTROMAGNETIC RADIATION Glovebox design for Space Station Freedom Crew [NASA-CR-193137] p 322 N93-28895 Gene transcription and electromagnetic fields Health Care System DRUGS [DE93-010854] p 276 N93-28848 [SAE PAPER 921139] P 292 A93-41326 Aminohydroxybutane bisphosphonate and clenbuterol ELECTROMYOGRAPHY Design of a Shuttle air and water prefilter for reduced prevent bone changes and retard muscle atrophy Sudden loading and fatigue effects on the human gravity operation respectively in tail-suspended rats p 271 A93-39703 spine [SAE PAPER 921161 ] P 294 A93-41343 Analysis of neural systems involved in modulation of [PB93-167526] p 286 N93-29199 Conceptual design of ECLSS microgravity test beds memory storage ELECTRON MOBILITY [SAE PAPER 921164] P 294 A93-41346 [AD-A262418] p 283 N93-27654 Wide-bandwidth high-resolution search for Ergonomic development of digital map displays DUST COLLECTORS extraterrestrial intelligence [NASA-CR-193137] p 322 N93-28895 p 320 N93-28866 Dust protection for environmental control and life support DEW POINT systems in the lunar environment p 315 N93-27979 ELECTROPHORESIS Evaluation of capillary electrophoresis for in-flight ionic Dew point analysis for Space Station Freedom DYNAMIC LOADS [SAE PAPER 921227] P 296 A93-41401 contaminant monitoring of SSF potable water Sudden loading and fatigue effects on the human [SAE PAPER 921268] p 300 A93-41438 DIAGNOSIS spine Electrophoretic separation of cells and particles from Long-lasting neuropsycholodical changes after a single [PB93-167526] p 286 N93-29199 rat pituitary and rat spleen high altitude climb P 278 A93-39713 DYNAMIC MODELS New technology (ot the analysis of the results of an [NASA-CR-193073] p 276 N93-28415 EVA Glove Research Team ultrasound experiment performed in aviation-medicine Comparative mutagenesis of human cells in vivo and [NASA-CR-193014] p 313 N93-27847 medical examination P 279 A93-40774 in vitro Case report - Chronic sub-dural hematoma following DYNAMIC STRUCTURAL ANALYSIS [DE93-012269] p 276 N93-28651 A preliminary structural analysis of space-based high-speed ejection P 282 A93-41171 ELECTROPHYSIOLOGY Use of RNA hybridization in the diagnosis of a case of inflatable tubular frame structures p313 N93-27849 The use of electrophysiological and cognitive variables ulceroglandular tularemia Power assist EVA glove development in the assessment of degradation during periods of [FOA-B-40422-4.4] P 275 N93-28212 p314 N93-27850 sustained wakefulness Proceedings of a Workshop on Molecular Nuclear [AD-A263033] p 283 N93-27923 Medicine EMBEDDING [DE93-010828] P 285 N93-28835 Virtual interface applications for airborne weapons DIGESTING systems p 318 N93-28858 Comparative mutagenesis of human cells in vivo and EARDRUMS EMBOLISMS in vitro Barotrauma in Boeing 737 cabin crew High-altitude pulmonary edema with pulmonary [DE93-012269] P 276 N93-28651 p 278 A93-39706 thromboembolism p 278 A93-39709

A-5 EMBRYOLOGY SUBJECT INDEX

EMBRYOLOGY ENVIRONMENTAL MONITORING Development of the Hermes EVA Space Suit Glove Altering the position of the first horizontal cleavage Space Station Freedom Environmental Health Care [SAE PAPER 921256] p 299 A93-41426 furrow of the amphibian (Xenopus) egg reduces embryonic Program Development of a regenerable metal oxide sheet matrix survival p272 A93-39717 [SAE PAPER 921138] p 292 A93-41325 CO2 removal system ENERGY BUDGETS Microbiological concerns and methodological [SAE PAPER 921298] p 302 A93-41463 Biomass productivity and sustainability of a approaches related to bacterial water quality in Portable life support system regenerative carbon dioxide bioregenerative life-support system spaceflight and water vapor removal by metal oxide absorbents [SAE PAPER 921359] p 307 A93-41518 [ SAE PAPER 921232 ] p 297 A93-41406 preprototype hardware development and testing ENVIRONMENTAL CONTROL Instrumentation for microbial monitoring of [SAE PAPER 921299] p303 A93-41464 Space Station Water Processor. Current flight design decontamination or biocide system effectiveness Metabolic responses to simulated extravehicular I SAE PAPER 921112] p 289 A93-41306 [SAE PAPER 921233] p 297 A93-41407 activity Overview of NASA's 199) Life Support Systems Analysis (SAE PAPER 921303] p 282 A93-41468 Crew Health Care Systems installations for Space Workshop Performance evaluation of candidate space suit Station Freedom [SAE PAPER 921118] p 290 A93-41310 elements for the next generation orbital EMU [SAE PAPER 921249] p 298 A93-41420 The development of an atmosphere composition monitor [SAE PAPER 921344] p 305 A93-41503 for the Environmental Control and Life Support System Continuous monitoring of effluent iodine levels of Space Extravehicular activity system p 312 N93-27787 [SAE PAPER 921149] p 292 A93-41333 Station water using solid state technology EVA/manned systems p 312 N93-27789 Oxygen generation by static feettwater electrolysis for [SAE PAPER 921265] p 299 A93-41435 Evolving EVA system capability for the evolving Space Space Station Freedom Measurement of free and dissolved gas content of water Station Freedom requirements p312 N93-27791 [SAE PAPER 921151] p 293 A93-41335 samples on Space Station Freedom EVA and telerobot interaction p312 N93-27792 The Centrifuge Facility Life Sciences Glovebox [SAE PAPER 921267] p 300 A93-41437 Extravehicular activity technology discipline configuration study First entry operations for spacecraft p314 N93-27859 [SAE PAPER 921158] p 293 A93-41341 [SAE PAPER 921384] p 308 A93-41542 EXTRAVEHICULAR MOBILITY UNITS Zero gravity phase separator technologies - Past, ENVIRONMENTAL QUALITY Performance evaluation of candidate space suit present and future Microbiology operations and facilities aboard elements for the next generation orbital EMU [ SAE PAPER 921160 ] p 293 A93-41342 restructured Space Station Freedom [SAE PAPER 921344] p 305 A93-41503 Conceptual design of ECLSS microgravity test beds [SAE PAPER 921213] p 296 A93-41389 ASDA - Advanced Suit Design Analyzer computer [SAE PAPER 921164] p 294 A93-41346 ENZYME ACTIVITY program Initial accomplishments of the Environmental Control Mechanical stimulation of skeletal muscle increases [SAE PAPER 921381] p 308 A93-41539 and Life Support System (ECLSS) atmosphere prostaglandin F2(alpha) synthesis and cyclooxygenase Evolution of Space Station EMU PLSS technology revitalization (AR) predevelopment operational system test activity by a pertussis toxin sensitive mechanism recommendations p312 N93-27790 (POST) for the Space Station Freedom (SSF) [NASA-CR-193041] p 282 N93-27102 Evolving EVA system capability for the evolving Space [ SAE PAPER 921186 ] p 294 A93-41365 Comparative mutagenesis of human cells in vivo and Station Freedom requirements p312 N93-27791 A trade study method for determining the design in vitro Simplified Aid For Crew Rescue (SAFR) parameter of CELSS subsystems [DE93-012269] p 276 N93-28651 p313 N93-27793 [ SAE PAPER 921198 ] p 295 A93-41374 ENZYMES Extravehicular activity technology discipline A systems approach to water recovery testing for space Comparative mutagenesis of human cells in vivo and p314 N93-27859 life support - Initial biomedical results from the ECLSS in vitro EXTREMELY LOW FREQUENCIES Water Recovery Test and plans for testbed utilization [DE93-012269] p 276 N93-28651 Gene transcription and electromagnetic fields [SAE PAPER 921210] p 295 A93-41386 Introductions to the Proceedings of the Fourteenth [DE93-010854] p 276 N93-28848 Dew point analysis for Space Station Freedom Symposium on Biotechnology for Fuels and Chemicals EYE MOVEMENTS [SAE PAPER 921227] p 296 A93-41401 [DE93-006235] p 276 N93-28890 NASA supporting studies for microgravity research on Comparative test data assessment and simplified math EPIDERMIS eye movements modelling for Sabatier CO2 reduction subsystem Inhibition of EGF-induced signal transaction by [NASA-CR-193233] p 285 N93-29041 [ SAE PAPER 921228 ] p 296 A93-41402 microgravity is independent of EGF receptor redistribution Head mounted displays for virtual reality [AD-A263498] p 322 N93-29340 The effects of a reduced pressure scenario on the in the plasma membrane of human A431 cells Columbus APM environmental control system p272 A93-39715 [SAE PAPER 921247] p 298 A93-41418 ERRORS Identification of hazardous awareness states in System integration and verification approach for the monitoring environments environmental control system of the Columbus Attached [SAE PAPER 921136] p 287 A93-41324 Pressurised Module F-16 AIRCRAFT ETIOLOGY Head-steered sensor flight test results and (SAE PAPER 921261] p 299 A93-41431 Barotrauma in Boeing 737 cabin crew implications p318 N93-28859 The analytical control program for the NASA Space p278 A93-39706 FABRICS Station Freedom Environmental Control and Life Support Motion sickness induced by sinusoidal linear System (ECLSS) Water Recovery Test EVA Glove Research Team acceleration in rats p 272 A93-39712 [NASA-CR-193014] p313 N93-27847 [SAE PAPER 921269] p 300 A93-41439 EUKARYOTES Power assist EVA glove development Environmental control of the Mini Pressurized Logistic Intracellular targeting of the Yersinia YopE cytotoxin in p314 N93-27850 Module mammalian cells induces actin microfilament disruption [SAE PAPER 921281] p 302 A93-41449 [FOA-B-40420-4.4] p 275 N93-27989 FACTOR ANALYSIS Crucial role of detailed function, task, timeline, link, and Recent regenerative ECLSS technology developments Regulation of alternative CO2 fixation pathways in in Europe procaryotic and eucaryotic photosynthetic organisms human vulnerability analyses in HRA [DE93-001923] p 321 N93-28942 [SAE PAPER 921332] p 304 A93-41493 [DE93-012109] p 276 N93-29181 Life Support and Habitability Manual ESA PSS-03-406 EUROPEAN SPACE AGENCY FEASIBILITY ANALYSIS [SAE PAPER 921338] p 305 A93-41497 European involvement in CELSS • Definition of a Closed A feasibility study of hand kinematics for EVA analysis using magnetic resonance imaging Shuttle Orbiter Environmental Control and Life Support Ecological Systems Test Bed [SAE PAPER 921253] p 298 A93-41423 System - Flight experience [SAE PAPER 921200] p 295 A93-41376 [SAE PAPER 921348] p 305 A93-41507 Life Support and Habitability Manual ESA PSS-03-406 A feasibility study of hand kinematics for EVA analysis using magnetic resonance imaging p313 N93-27848 Air Handling and Atmosphere Conditioning systems for [SAE PAPER 921338] p 305 A93-41497 manned spacecraft - A design and performance data EUSTACHIAN TUBES FEEDBACK CONTROL survey Barotrauma in Boeing 737 cabin crew An update on the readiness of vapor compression p 278 A93-39706 distillation for spacecraft wastewater processing [SAE PAPER 921350] p 306 A93-41509 EXPERIMENT DESIGN [SAE PAPER 921114] p 290 A93-41307 The General Purpose Work Station, a spacious Plant growth modeling at the JSC variable pressure microgravity workbench FERTILIZERS growth chamber - An application of experimental design [SAE PAPER 921394] p 309 A93-41552 Development of the nitrogen fixation system for [SAE PAPER 921356] p 307 A93-41515 CELSS Environmental control and life support system EXPOSURE [ SAE PAPER 921238 ] p 297 A93-41411 p311 N93-27718 Variations of time-tc-incapacitation and FIELD OF VIEW Environmental control and life support system carboxyhemoglobin values in rats exposed to two carbon The effect of geometric field of view and tunnel design evolution p311 N93-27719 monoxide concentrations for perspective flight-path displays Technologies for ECLSS evolution [DOT/FAA/AM-93/7] p 274 N93-27152 [SAE PAPER 921131] p 291 A93-41319 p311 N93-27720 EXTINCTION Visual field information in nap-of-the-Earth flight by Geography of end-Cretaceous marine bivalve The ECLSS advanced automation project evolution and teleoperated helmet-mounted displays technology assessment p 312 N93-27723 extinctions p 273 A93-41075 p311 N93-27177 EXTRAVEHICULAR ACTIVITY Marshall Space Flight Center ECLSS technology FIGHTER AIRCRAFT activities p312 N93-27724 The effects of a reduced pressure scenario on the Columbus APM environmental control system Specification of adaptive aiding systems JSC ECLSS R/T program overview [SAE PAPER 921247] p 298 A93-41418 [AD-A263071] p 314 N93-27927 p312 N93-27725 A feasibility study of hand kinematics for EVA analysis Symbology for head up and head down applications for Environmental control and life support systems using magnetic resonance imaging highly agile fighter aircraft To improve spatial awareness, p314 N93-27858 [SAE PAPER 921253] p 298 A93-41423 trajectory control, and unusual attitude recovery, part 1 Assessment of the state of the art in life support Development of a test protocol for evaluating EVA glove p318 N93-28857 environmental control for SEI p315 N93-27978 performance The physiological limitations of man in the high G Oust protection for environmental control and life support [SAE PAPER 921254] p 298 A93-41424 environment p319 N93-28861 systems in the lunar environment p315 N93-27979 Power assist EVA glove development Requirements for pilot assistance in a thrust-vectoring Manned lunar surface site p 316 N93-28033 [SAE PAPER 921255] p 299 A93-41425 combat aircraft P 320 N93-28870

A-6 SUBJECT INDEX HEALTH

FILTRATION FLUID MANAGEMENT GENETIC ENGINEERING The application of nitration technology within the Water Development of membrane gas removal technology for Characterization and classification of strains of Processor on board Space Station Freedom microgravity liquid flow systems Francisella tularensis isolated in the central Asian focus [SAE PAPER 9212701 p 300 A93-41440 [SAE PAPER 921162) p 294 A93-41344 of the Soviet Union and in Japan Evaluation and optimization of a flexible filtration system Two phase fluid management for hydroponics [FOA-B-40421-4.4] p 275 N93-28200 for respiratory protection system 21 [SAE PAPER 921163] p 294 A93-41345 Use of RNA hybridization in the diagnosis of a case of IAD-A262467] p 284 N93-28758 FLUOROCARBONS ulceroglandular tularemia FINGERS Human performance and physiological function during [FOA-B-40422-4.4] p 275 N93-28212 A feasibility study of hand kinematics for EVA analysis a 24-hr exposure to 1 percent bromotrifluoromethane GENETICS using magnetic resonance imaging p313 N93-27848 (Halon1301) p277 A93-39704 Comparative mutagenesis of human cells in vivo and Power assist EVA glove development Toxicokinetics of inhaled bromotrifluoromethane (Halon in vitro p 314 N93-27850 1301) in human subjects p 278 A93-39705 [DE93-012269] p 276 N93-28651 FLYING PERSONNEL FIRE CONTROL Gene transcription and electromagnetic fields The use of electrophysiological and cognitive variables Increased fire and toxic contaminant detection [DE93-010854) p 276 N93-28848 in the assessment of degradation during periods of responsibility by use of distributed, aspirating sensors sustained wakefulness GLOVES p311 N93-27722 Glovebox design for Space Station Freedom Crew [AD-A263033] p 283 N93-27923 Pilot decision aiding for weapon delivery: A novel FOOD PRODUCTION (IN SPACE) Health Care System approach to fire control cueing using parallel computing Biosphere 2 - Overview of system performance during [SAE PAPER 921139] p 292 A93-41326 p317 N93-28853 the first nine months The Centrifuge Facility Life Sciences Glovebox Head-steered sensor flight test results and [SAE PAPER 921129] p 291 A93-41317 configuration study implications p318 N93-28859 Crop interactions in potyculture and their implications [SAE PAPER 921158] p 293 A93-41341 FLIGHT CONTROL for CELSS design Development of a test protocol for evaluating EVA glove Combat Automation for Airborne Weapon Systems: [SAEPAPER921197] p295 A93-41373 performance Man/Machine Interface Trends and Technologies OCAM - A CELSS modeling tool: Description and results [SAE PAPER 921254) p 298 A93-41424 [AGARD-CP-520] p317 N93-28850 — Object-oriented Controlled Ecological Life Support Power assist EVA glove development Virtual interface applications for airborne weapons System Analysis and Modeling [SAE PAPER 921255] p 299 A93-41425 systems p 318 N93-28858 [SAE PAPER 921241) p 298 A93-4U13 Development of the Hermes EVA Space Suit Glove Head-steered sensor flight test results and FOSSILS [SAE PAPER 921256] p 299 A93-41426 implications p 318 N93-28859 Microfossils of the Early Archean Apex chert • New EVA Glove Research Team Overview of cocKpit technology research and evidence of the antiquity of life p 272 A93-40308 [NASA-CR-193014] p313 N93-27847 FRAGMENTS development programs for improvement of the Power assist EVA glove development man/machine interface: Review of the AGARD AVP Amino acid sequences for the binding regions in serum p314 N93-27850 albumin proteins Symposium held in Madrid, May 1992 Biophysical model for handwear insulation testing p 320 N93-28872 [NASA-CASE-MFS-28402-1] p 276 N93-28952 FREON [AD-A262926] p 320 N93-28884 FLIGHT CREWS Human performance and physiological function during GLUCOSE Barotrauma in Boeing 737 cabin crew a 24-hr exposure to 1 percent bromotrifluoromethane Effects of sleep deprivation and exercise on glucose P278 A93-39706 (Halon 1301) p 277 A93-39704 tolerance p 281 A93-41165 New technology for the analysis of the results of an Toxicokinetics of inhaled bromotrifluoromethane (Halon GRAVITATION ultrasound experiment performed in aviation-medicine 1301) in human subjects p 278 A93-39705 The physiological limitations of man in the high G medical examination p 279 A93-40774 FROZEN FOODS environment p319 N93-28861 Identification of hazardous awareness states in Space Station Freedom food management GRAVITATIONAL EFFECTS monitoring environments [SAE PAPER 921248] p 298 A93-41419 NASA supporting studies for microgravity research on [SAE PAPER 921136] p 287 A93-41324 FUMES eye movements Crew Health Care Systems installations for Space Potential health effects of fume particles on the crew [NASA-CR-193233] p 285 N93-29041 Station Freedom of spacecrafts GRAVITATIONAL PHYSIOLOGY [SAE PAPER 921249) P 298 A93-41420 [SAE PAPER 921387] p 308 A93-41545 Intraocular pressure and retinal vascular changes during FLIGHT FITNESS FUNCTIONAL DESIGN SPECIFICATIONS transient exposure to microgravity p 278 A93-39710 New technology for the analysis of the results of an Functions simulation model of integrated regenerate Altering the position of the first horizontal cleavage ultrasound experiment performed in aviation-medicine life support system furrow of the amphibian (Xenopus) egg reduces embryonic medical examination p 279 A93-40774 [SAE PAPER 921201] p 295 A93-41377 survival p 272 A93-39717 FLIGHT INSTRUMENTS Extravehicular activity system p 312 N93-27787 Program development for exercise countermeasures Pilot intent and error recognition as part of a knowledge FUNCTIONAL INTEGRATION [SAE PAPER 921140] p 292 A93-41327 based cockpit assistant p318 N93-28855 The quest for an integrated flying helmet The physiological limitations of man in the high G FLIGHT PATHS p319 N93-28860 environment p 319 N93-28861 FUNGI The effect of geometric field of view and tunnel design GROWTH for perspective flight-path displays Relative resistance of biofilms and planktonic cells of Electrophoretic separation of cells and particles from [SAE PAPER 921131] p 291 A93-41319 common molds and yeasts to antimicrobials rat pituitary and rat spleen [SAE PAPER 921212] p 273 A93-41388 Symbology for head up and head down applications for [NASA-CR-193073] p 276 N93-28415 highly agile fighter aircraft: To improve spatial awareness, Altered immunological response in mice subjected to trajectory control, and unusual attitude recovery, part 1 stress and exposed to fungal spores p318 N93-28857 [SAE PAPER 921215] p 274 A93-41391 H FLIGHT PLANS Pilot intent and error recognition as part of a knowledge HAND (ANATOMY) based cockpit assistant p318 N93-2885S A feasibility study of hand kinematics for EVA analysis FLIGHT SIMULATION using magnetic resonance imaging GAMMA RAYS Performance consequences of automation-induced [SAE PAPER 921253] p 298 A93-41423 Flow cytometric analysis of lymphocyte surface markers 'complacency1 P 286 A93-39571 HARDWARE following a 1 -Gy dose of gamma radiation Increasing hits and reducing misses in CRM/LOS Tests characterizing bioprocessor hardware for p281 A93-41170 scenarios - Guidelines for simulator scenario analytical modeling GAS EXCHANGE development p 286 A93-39575 [SAE PAPER 921357] p 307 A93-41516 Mathematical model for the exchange of gases in the Virtual interface applications for airborne weapons Marshall Space Flight Center ECLSS technology lungs with special reference to carbon monoxide systems p318 N93-28858 activities p 312 N93-27724 p 271 A93-39707 Requirements for pilot assistance in a thrust-vectoring HEAD DOWN TILT GAS PRESSURE combat aircraft P 320 N93-28870 Microgravity and orthostatic intolerance - Carotid Growing wheat to maturity in reduced gas pressures FLIGHT SIMULATORS hernodynamics and peripheral responses [NASA-CR-193245] p 277 N93-29216 Increasing hits and reducing misses in CRM/LOS p278 A93-39716 GELS scenarios - Guidelines for simulator scenario Response of genioglossus EMG activity to passive tilt Comparative mutagenesis of human cells in vivo and development p 286 A93-39575 in men p 279 A93-41118 in vitro A study of decision making and performance in rejected Cerebral blood velocity and other cardiovascular [DE93-012269] p 276 N93-28651 takeoffs responses to 2 days of head-down tilt GENE EXPRESSION [SAE PAPER 921134] p 287 A93-41322 p 280 A93-41122 Plasmid encoded virulence of Yersinia Pilot intent and error recognition as part of a knowledge Performance and mood-state parameters during 30-day [FOA-B-40419-4.4] p 275 N93-28199 based cockpit assistant p318 N93-28855 6 deg head-down bed rest with exercise training Gene transcription and electromagnetic fields FLIGHT TESTS p281 A93-41169 [DE93-010854] p 276 N93-28848 Head-steered sensor flight test results and HEAD-UP DISPLAYS implications p318 N93-28859 GENETIC CODE Oculo-motor responses and virtual image displays Intracellular targeting of the Yersinia YopE cytotoxin in FLIR DETECTORS p 319 N93-28862 Visual field information in nap-of-the-Earth flight by mammalian cells induces actin microfilament disruption HEALTH teleoperated helmet-mounted displays IFOA-B-40420-4.4] p 275 N93-27989 Space Station Freedom Environmental Health Care p311 N93-27177 Plasmid encoded virulence of Yersinia Program The design and development of the new RAF standard [FOA-B-40419-4.4] p 275 N93-28199 [SAE PAPER 921138] p 292 A93-41325 HUD format P 318 N93-28856 Comparative mutagenesis of human cells in vivo and Crew Health Care Systems installations for Space Head-steered sensor flight test results and in vitro Station Freedom implications P 318 N93-28859 [DE93-012269] p 276 N93-28651 [SAE PAPER 921249] p 298 A93-41420

A-7 HEAT BALANCE SUBJECT INDEX

HEAT BALANCE HUMAN BEHAVIOR Crucial role of detailed function, task, timeline, link, and Influence of the Cold Buster (tm) sports bar on heat Method of encouraging attention by correlating video human vulnerability analyses in HRA debt, mobilization and oxidation of energy substrates game difficulty with attention level [DE93-001923] p 321 N93-28942 [AD-A262762] p 285 N93-28939 [NASA-CASE-LAR-15022-1] p 288 N93-28128 HUMAN REACTIONS HEAT EXCHANGERS Theory of signal detection and its application to visual Armstrong Laboratory space visual function tester Tests characterizing bioprocessor hardware for target acquisition: A review of the literature program p 284 N93-28739 analytical modeling [AD-A262920] p 288 N93-28307 HUMAN WASTES [SAE PAPER 921357] p 307 A93-41516 HUMAN BEINGS Concept of waste transferring mechanisms Space Station Condensing Heat Exchanger biofilm Comparative mutagenesis of human cells in vivo and [SAE PAPER 921239) p 297 A93-41412 formation and control evaluation in vitro Test of the Shuttle Extended Duration Orbiter (EDO) [SAE PAPER 921383] p 308 A93-41541 [DE93-012269] p 276 N93-28651 Waste Collection Subsystem (WCS) HEAT TRANSFER [SAE PAPER 921346] p 305 A93-41505 Sudden loading and fatigue effects on the human Tests characterizing bioprocessor hardware for HUMIDITY spine analytical modeling Use of sorption technology for treatment of humidity [PB93-167526] p 286 N93-29199 [SAE PAPER 921357) p 307 A93-41516 condensate for potable water ASDA - Advanced Suit Design Analyzer computer HUMAN FACTORS ENGINEERING [SAE PAPER 921312] p 303 A93-41474 program Operational space human factors - Methodology for a Space Station Condensing Heat Exchanger biofilm [SAE PAPER 921381] p 308 A93-41539 DSO — Detailed Supplementary Objective for manned formation and control evaluation Lunar base thermal management/power system Shuttle Orbiter missions [SAE PAPER 921383] p 308 A93-41541 analysis and design p315 N93-27985 [SAE PAPER 921156] P 293 A93-41339 HUMIDITY MEASUREMENT HELICOPTER CONTROL Development of the Hermes EVA Space Suit Glove Analysis of the Variable Pressure Growth Chamber using Visual field information in nap-of-the-Earth flight by [SAE PAPER 921256] p 299 A93-41426 the CASE/A simulation package teleoperated helmet-mounted displays Development of a 500 hPa shoulder joint for the [SAE PAPER 921122] p 291 A93-41314 P311 N93-27177 European EVA Space Suit System HYDRAULIC EQUIPMENT HELMET MOUNTED DISPLAYS [SAE PAPER 921257] p 299 A93-41427 An update on the readiness of vapor compression Visual field information in nap-of-the-Earth flight by Comparison of portable crewmember protective distillation for spacecraft wastewater processing teleoperated helmet-mounted displays breathing equipment (CPBE) designs [SAE PAPER 921114] p 290 A93-41307 P311 N93-27177 [DOT/FAA/AM-93/6] p 310 N93-27121 HYDROCYANIC ACID Low-cost helmet-mounted displays Man-systems distributed system for Space Station Variations in time-to-incapacitation and blood cynanide [AD-A262616] p 317 N93-28479 Freedom p312 N93-27788 values for rats exposed to two hydrogen cyanide gas Head-steered sensor flight test results and EVA/manned systems p 312 N93-27789 concentrations implications p 318 N93-28859 Evolution of Space Station EMU PLSS technology [DOT/FAA/AM-93-8] p 283 N93-27158 The quest for an integrated flying helmet recommendations p 312 N93-27790 HYDROPONICS Two phase fluid management for hydroponics p 319 N93-28860 Evolving EVA system capability for the evolving Space [SAE PAPER 921163] p 294 A93-41345 Oculc-motor responses and virtual image displays Station Freedom requirements p 312 N93-27791 HYPERBARIC CHAMBERS p 319 N93-28862 EVA and telerobot interaction p 312 N93-27792 Evolving technologies for Space Station Freedom Hyperbaric treatment operations aboard Space Station Head mounted displays for virtual reality computer-based workstations p 313 N93-27794 Freedom [AD-A263498] p 322 N93-29340 Man-systems integration and the man-machine [SAE PAPER 921142] p 292 A93-41328 HELMETS interface p 313 N93-27795 HYPERGLYCEMIA The quest for an integrated flying helmet Manned systems technology discipline Effects of sleep deprivation and exercise on glucose P319 N93-28860 p 314 N93-27860 tolerance p 281 A93-41165 HEMODYNAMIC RESPONSES Specification of adaptive aiding systems HYPERTENSION Microgravity and orthostatic intolerance - Carotid [AD-A263071] p 314 N93-27927 Minimal hypoxic pulmonary hypertension in normal hemodynamics and peripheral responses Combat Automation for Airborne Weapon Systems: Tibetans at 3,658 m p 280 A93-41121 P278 A93-39716 Man/Machine Interface Trends and Technologies HYPOBARIC ATMOSPHERES Orthostatic intolerance during a 13-day bed rest does [AGARD-CP-520] p 317 N93-28850 Influence of in vivo hypobaric hypoxia on function of not result from increased leg compliance The design and development of the new RAF standard lymphocytes, neutrocytes, natural killer cells, and p280 A93-41119 HUD format p 318 N93-28856 cytokines p 280 A93-41123 Minimal hypoxic pulmonary hypertension in normal Operator and automation capability analysis: Picking the HYPOKINESIA Tibetans at 3.658 m p 280 A93-41121 right team p 319 N93-28864 Myosin and troponin changes in rat soleus muscle after Cerebral blood velocity and other cardiovascular Ergonomic development of digital map displays hindlimb suspension p 273 A93-41124 responses to 2 days of head-down tilt P320 N93-28866 HYPOTHALAMUS P280 A93-41122 System automation and pilot-vehicle-interface for Norepinephrine content in discrete brain areas and Body fluid compartments, renal blood flow, and unconstrained low-altitude night attack neurohypophysial vasopressin in rats after a 9-d spaceflight hormones at 6,000 m in normal subjects p 320 N93-28867 (SLS-1) p273 A93-41167 Crucial role of detailed function, task, timeline, link, and p281 A93-41125 HYPOXIA human vulnerability analyses in HRA Effects of dynamic exercise on cardiovascular regulation Hypoxic ventilatory responsiveness in Tibetan compared [DE93-001923] p 321 N93-28942 during lower body negative pressure with Han residents of 3,658 m p280 A93-41120 NASA supporting studies for microgravity research on P281 A93-41168 Minimal hypoxic pulmonary hypertension in normal eye movements Tibetans at 3,658 m p 280 A93-41121 HEMOGLOBIN [NASA-CR-193233] p 285 N93-29041 Interactions between Hb, Mg, DPG, ATP, and Cl Anthropometric data from launch and entry suited test Influence of in vivo hypobaric hypoxia on function of determine the change in Hb-O2 affinity at high altitude subjects for the design of a recumbent seating system lymphocytes, neutrocytes, natural killer cells, and P279 A93-41117 [NASA-TM-104769] p 321 N93-29044 cytokines p 280 A93-41123 13 C NMR spectra of allosteric effectors of HUMAN FACTORS LABORATORIES hemoglobin A feasibility study of hand kinematics for EVA analysis [AD-A262979] p 284 N93-28293 using magnetic resonance imaging p 313 N93-27848 HEMORRHAGES HUMAN PATHOLOGY Case report - Chronic sub-dural hematoma following Barotrauma in Boeing 737 cabin crew IMAGE PROCESSING high-speed ejection p 282 A93-41171 p 278 A93-39706 A modular head/eye platform for real-time reactive HERMES MANNED SPACEPLANE Growth factor involvement in tension-induced skeletal vision Hermes ECLSS - Main requirements and technical muscle growth [OUEL-1941/92] p 320 N93-28897 solutions fNASA-CR-193023] p 282 N93-27113 IMAGING TECHNIQUES [SAE PAPER 921400] p 309 A93-41555 HUMAN PERFORMANCE Mapping of electrical muscle stimulation using MRI HEURISTIC METHODS Performance consequences of automation-induced p279 A93-40549 Specification of adaptive aiding systems •complacency' p 286 A93-39571 A feasibility study of hand kinematics for EVA analysis [AD-A263071] p 314 N93-27927 Structured interviews for pilot selection - No incremental using magnetic resonance imaging HIGH ALTITUDE ENVIRONMENTS validity p 286 A93-39572 [SAE PAPER 921253] p 298 A93-41423 High-altitude pulmonary edema with pulmonary Human performance and physiological function during Dark cycle monitoring of biological specimens on Space thromboembolism p 278 A93-39709 a 24-hr exposure to 1 percent bromotrifluoromethane Station Freedom (Haton 1301) p 277 A93-39704 HIGH ELECTRON MOBILITY TRANSISTORS (SAE PAPER 921393) p 274 A93-41551 Dynamic analysis of human visuc-oculc-manual Wide-bandwidth high-resolution search for EVA Glove Research Team coordination control in target tracking tasks [NASA-CR-193014] p313 N93-27847 extraterrestrial intelligence P287 A93-41166 A feasibility study of hand kinematics for EVA analysis [NASA-CR-193137] p 322 N93-28895 Identification of hazardous awareness states in using magnetic resonance imaging p 313 N93-27848 HISTAMINES monitoring environments Neuropharmacology of motion sickness and emesis - [SAE PAPER 921136] p 287 A93-41324 Low-cost helmet-mounted displays A review p 271 A93-39711 How expert pilots think: Cognitive processes in expert [AD-A262616] p317 N93-28479 HORMONES decision making IMMUNE SYSTEMS Absence of a growth hormone effect on rat soleus [DOT/FAA/RD-93/9] p 288 N93-27103 Influence of in vivo hypobaric hypoxia on function of atrophy during a 4-day spaceflight p 272 A93-40548 Method of encouraging attention by correlating video lymphocytes, neutrocytes, natural killer cells, and HORN ANTENNAS game difficulty with attention level cytokines p280 A93-41123 Wide-bandwidth high-resolution search for [NASA-CASE-LAR-15022-1] p 288 N93-28128 Altered immunological response in mice subjected to extraterrestrial intelligence Human capabilities and limitations in situation stress and exposed to fungal spores [NASA-CR-193137] p 322 N93-28895 awareness p 319 N93-28863 [SAE PAPER 921215) p 274 A93-41391

A-8 SUBJECTINDEX LIFE SUPPORT SYSTEMS

IMMUNITY Regenerable Microbial Check Valve - Life cycle tests The development of an atmosphere composition monitor Relative resistance of biofilms and planktonic cells of results for the Environmental Control and Life Support System common molds and yeasts to antimicrobials [SAE PAPER 921316) p 303 A93-41478 [SAE PAPER 921149] p 292 A93-41333 ISAE PAPER 921212] p 273 A93-41388 Regenerable biocide delivery unit, volume 1 Oxygen generation by static feedwater electrolysis for IMMUNOLOGY [NASA-CR-185701) p 274 N93-27122 Space Station Freedom Altered immunological response in mice subjected to IRON OXIDES [SAE PAPER 9211511 p 293 A93-41335 stress and exposed to fungal spores Ferrous iron oxidation by anoxygenic phototrophic The Centrifuge Facility Life Sciences Glovebox [SAE PAPER 921215) p 274 A93-41391 bacteria p 271 A93-39280 configuration study INDEXES (DOCUMENTATION) ISOLATION [SAE PAPER 921158] p 293 A93-41341 Index of international publications in aerospace The psychological effects of isolation on a space station Zero gravity phase separator technologies - Past, medicine - A simulation study present and future [AD-A262908] p 284 N93-28306 [SAE PAPER 921191) p 287 A93-41369 [ SAE PAPER 921160) p 293 A93-41342 ISOTOPE EFFECT INDOOR AIR POLLUTION Conceptual design of ECLSS microgravity test beds 13 C NMR spectra of allosteric effectors of Setting Spacecraft Maximum Allowable Concentrations [SAE PAPER 921164] p 294 A93-41346 for 1 hour or 24 hour contingency exposures to airborne hemoglobin [AD-A262979] p 284 N93-28293 Initial accomplishments of the Environmental Control chemicals and Life Support System (ECLSS) atmosphere [SAE PAPER 921410] p 310 A93-41564 revitalization (AR) predevelopment operational system test The role of Environmental Health System air quality (POST) for the Space Station Freedom (SSF) monitors in Space Station Contingency Operations [SAE PAPER 921186) p 294 A93-41365 [SAE PAPER 921414] p 310 A93-41565 JAPANESE SPACECRAFT Development of the carbon dioxide removal system INFLATABLE STRUCTURES Manned lunar surface site: Conceptual study on blower used on Space Station Freedom A preliminary structural analysis of space-based pressurized lunar surface operation rover [SAE PAPER 921188] p 294 A93-41367 inflatable tubular frame structures p 313 N93-27849 p 316 N93-28032 Crop interactions in polyculture and their implications INFORMATION MANAGEMENT for CELSS design Man-systems integration and the man-machine K [SAE PAPER 921197] p 295 A93-41373 interface p 313 N93-27795 A trade study method for determining the design INFORMATION PROCESSING (BIOLOGY) KINEMATICS parameter of CELSS subsystems How expert pilots think: Cognitive processes in expert [SAE PAPER 921198] p 295 A93-41374 decision making A feasibility study of hand kinematics for EVA analysis using magnetic resonance imaging European involvement in CELSS - Definition of a Closed (DOT/FAA/RD-93/9) p 288 N93-27103 [SAE PAPER 921253] p 298 A93-41423 Ecological Systems Test Bed INFORMATION SYSTEMS A feasibility study of hand kinematics for EVA analysis [SAE PAPER 921200] p 295 A93-41376 Head mounted displays for virtual reality using magnetic resonance imaging p 313 N93-27848 Functions simulation model of integrated regenerable [AD-A263498] p 322 N93-29340 KNOWLEDGE BASED SYSTEMS life support system INFRARED DETECTORS Pilot intent and error recognition as part of a knowledge [SAE PAPER 921201] p 295 A93-41377 Dark cycle monitoring of biological specimens on Space based cockpit assistant p 318 N93-28855 A systems approach to water recovery testing for space Station Freedom Cognitive interface considerations for intelligent life support - Initial biomedical results from the ECLSS [SAE PAPER 921393] p 274 A93-41551 cockpits p319 N93-28865 Water Recovery Test and plans for testbed utilization INJURIES [ SAE PAPER 921210] p 295 A93-41386 Potential health hazards from thermal degradation Dew point analysis for Space Station Freedom events - Particulate vs. gas phase effects [SAE PAPER 921227] p 296 A93-41401 [ SAE PAPER 921388 ] p 282 A93-41546 Comparative test data assessment and simplified math Secondary injury factors and preventative treatment LANDING modelling for Sabatier CO2 reduction subsystem [SAE PAPER 921228] p 296 A93-41402 [PB93-176014] p283 N93-27409 The effect of geometric field of view and tunnel design for perspective flight-path displays Simplified analysis of water distribution for Space Station Wound healing and connective tissue metabolism: The [SAE PAPER 921131] p 291 A93-41319 Freedom role of hyperbaric oxygen therapy [SAE PAPER 921230] p 296 A93-41404 (AD-A262483) p 285 N93-28759 LAUNCH ESCAPE SYSTEMS A comparison of two Shuttle launch and entry suits - Evaluation of the carbon dioxide removal assembly Sudden loading and fatigue effects on the human Reach envelope, isokinetic strength, and treadmill tests requirements for the Space Station Freedom in the Manned spine [SAE PAPER 921154] p 293 A93-41337 Tended Capability through Permanently Manned Capability [PB93-167526] p 286 N93-29199 LENSES configurations INSTRUMENT APPROACH A study of the effects of lens focal length on remote [SAE PAPER 921231] p 297 A93-41405 Instrument-approach-plate design considerations for driver performance Development of the nitrogen fixation system for displaying radio frequencies p 289 A93-39574 [AD-A263191] p 321 N93-28941 CELSS INSTRUMENT FLIGHT RULES [SAE PAPER 921238] p 297 A93-41411 LEUKOCYTES Pilot intent and error recognition as part of a knowledge Concept of waste transferring mechanisms Influence of in vivo hypobaric hypoxia on function of based cockpit assistant p 318 N93-28855 [SAE PAPER 921239] p 297 A93-41412 lymphocytes, neutrocytes, natural killer cells, and INTERFACES OCAM - A CELSS modeling tool: Description and results cytokines p 280 A93-41123 DOKMA: A document oriented communication model — Object-oriented Controlled Ecological Life Support for medical applications as a basis of a role system in LIFE (DURABILITY) System Analysis and Modeling the medical field Regenerable Microbial Check Valve - Life cycle tests [SAE PAPER 921241] p 298 A93-41413 [ETN-93-93799] p 284 N93-28469 results System integration and verification approach for the INTERPLANETARY SPACECRAFT [SAE PAPER 921316] p 303 A93-41478 environmental control system of the Columbus Attached Human life support during interplanetary travel and LIFE SCIENCES Pressurised Module domicile. V - Mars expedition technology trade study for Microfossils of the Early Archean Apex chert - New [SAE PAPER 921261] p 299 A93-41431 solid waste management evidence of the antiquity of life p 272 A93-40308 The analytical control program for the NASA Space [SAE PAPER 921119] p 290 A93-41311 JPRS report: Science and technology. Central Eurasia: Station Freedom Environmental Control and Life Support Human life support during interplanetary travel and Life sciences System (ECLSS) Water Recovery Test domicile. VI - Generic modular flow schematic for hybrid [JPRS-ULS-93-005] p 276 N93-28683 [SAE PAPER 921269] p 300 A93-41439 physical/chemical-biological life support systems JPRS report: Science and technology. Central Eurasia: An assessment of waste processing/resource recovery [SAE PAPER 921120] p 290 A93-41312 Life sciences technologies for lunar/Mars life applications INTRACRANIAL PRESSURE [JPRS-ULS-92-027] p 276 N93-28684 [SAE PAPER 921271] p 300 A93-41441 Case report - Chronic sub-dural hematoma following LIFE SUPPORT SYSTEMS Catalytic oxidation for treatment of ECLSS and PMMS high-speed ejection p 282 A93-41171 Space Station Water Processor - Current flight design waste streams — Process Material Management INTRAOCULAR PRESSURE [SAE PAPER 921112] p 289 A93-41306 Systems Intraocular pressure and retinal vascular changes during Overview of NASA's 1991 Life Support Systems Analysis [SAE PAPER 921274] p 301 A93-41443 transient exposure to microgravity p 278 A93-39710 Workshop Post-treatment of reclaimed waste water based on an IODINE [SAE PAPER 921118] p 290 A93-41310 electrochemical advanced oxidation process [SAE PAPER 921275] p 301 A93-41444 Regenerable Microbial Check Valve - Life cycle tests Human life support during interplanetary travel and A hybrid regenerative water recovery system for results domicile. V - Mars expedition technology trade study for lunar/Mars life support applications [SAE PAPER 921316] p 303 A93-41478 solid waste management Inactivatton of a model coliphage virus in water by [SAE PAPER 921276] p 301 A93-41445 [SAE PAPER 921119) p 290 A93-41311 iodine Environmental control of the Mini Pressurized Logistic Human life support during interplanetary travel and [SAE PAPER 921361] p 274 A93-41520 Module domicile. VI - Generic modular flow schematic for hybrid Generation of iodine disinfection by-products (IDP's) in [SAE PAPER 921281) p 302 A93-41449 a water recycle system physical/chemical-biological life support systems Hazard and risk assessment for surface components [SAE PAPER 921120] p 290 A93-41312 [SAE PAPER 921362] p 307 A93-41521 of a lunar base Controlled Ecological Life Support Regenerable biocide delivery unit, volume 1 Recycling and source reduction for long duration space System [NASA-CR-185701] p 274 N93-27122 habitation [SAE PAPER 921285] p 302 A93-41451 ION EXCHANGE MEMBRANE ELECTROLYTES [SAE PAPER 921121] p 290 A93-41313 Advanced life support systems in lunar and Martian SPE water electrolyzers in support of the lunar TRIALSS - Tool for Rapid and Intelligent Advanced Life environments utilizing a higher plant based engineering outpost p315 N93-27977 Support System Selection and Sizing paradigm ION EXCHANGE RESINS [SAE PAPER 921123] p 291 A93-41315 [SAE PAPER 921286] p 302 A93-41452 Biofilm formation and control in a simulated spacecraft A low pressure electrolyzer for the next generation Consumables and wastes estimations for the First Lunar water system - Three year results submarine Outpost [SAE PAPER 921310) p 303 A93-41472 [SAE PAPER 921125] p 291 A93-41316 [SAE PAPER 921287) p 302 A93-41453

A-9 LINE OF SIGHT SUBJECT INDEX

Portable life support system regenerative carbon dioxide LIQUID COOLING Conceptual study of manned lunar surface site and water vapor removal by metal oxide absorbents Lightweight passive microclimate cooling device p316 N93-28031 preprototype hardware development and testing [AD-A262262] p 317 N93-28112 Manned lunar surface site: Conceptual study on [SAE PAPER 921299] p 303 A93-41464 LIQUID CRYSTALS pressurized lunar surface operation rover Biodeterioration of materials in water reclamation Low-cost helmet-mounted displays p316 N93-28032 systems [AD-A262616] p317 N93-28479 Lunar surface experiment system p 316 N93-28034 [SAE PAPER 921311) p 303 A93-41473 LIQUID FLOW LUNAR OUST Determination of organic carbon and ionic accountability Development of membrane gas removal technology for Dust protection for environmental control and life support of various waste and product waters derived from ECLSS microgravity liquid flow systems systems in the lunar environment p 315 N93-27979 water recovery tests and Spacelab humidity condensate [SAE PAPER 921162] p 294 A93-41344 LUNAR ENVIRONMENT [SAE PAPER 921313) p 303 A93-41475 LIQUID OXYGEN A study to explore locomotion patterns in partial gravity Gray water recycling with a unique vapor compression Hybrid oxygen system environments distillation (VCD) design [AD-A262417] p 317 N93-28464 [SAE PAPER 921157] p 293 A93-41340 [SAE PAPER 921318] p 304 A93-41480 LIQUID-GAS MIXTURES Dust protection for environmental control and life support Membrane technology for zero gravity life support Zero gravity phase separator technologies - Past, systems in the lunar environment p315 N93-27979 systems present and future LUNAR EXPLORATION [SAE PAPER 921320] p 304 A93-41482 [SAE PAPER 921160] p 293 A93-41342 Consumables and wastes estimations for the First Lunar Operation of a breadboard LOAD DISTRIBUTION (FORCES) Outpost liquid-sorbent/membrane-contactor system for removing Pilot investigation - Nominal crew induced forces in [SAE PAPER 921287] p 302 A93-41453 carbon dioxide and water vapor from air zero-g LUNAR LANDING SITES [SAE PAPER 921321] p 304 A93-41483 [SAE PAPER 921155] p 293 A93-41338 Lunar surface experiment system p316 N93-28034 Recent regenerative ECLSS technology developments LOCOMOTION LUNAR RESOURCES in Europe Simulating reduced gravity - A review of biomechanical Oxygen production on the Lunar materials processing [SAE PAPER 921332] p 304 A93-41493 issues pertaining to human locomotion frontier p315 N93-27967 Life Support and Habitability Manual ESA PSS-03-406 p289 A93-41175 Assessment of the state of the art in life support [SAE PAPER 921338] p 305 A93-41497 LONG DURATION SPACE FLIGHT environmental control for SEI p 315 N93-27978 Test of the Shuttle Extended Duration Obiter (EDO) Recycling and source reduction for long duration space LUNAR ROCKS Waste Collection Subsystem (WCS) habitation Oxygen production on the Lunar materials processing [SAE PAPER 921346] p 305 A93-41505 [SAE PAPER 921121 ] p 290 A93-41313 frontier p315 N93-27967 Shuttle Orbiter Environmental Control and Life Support Development of membrane gas removal technology for LUNAR ROVING VEHICLES System - Flight experience microgravity liquid flow systems Manned lunar surface site: Conceptual study on [SAE PAPER 921348] p 305 A93-41507 [SAE PAPER 921162] p 294 A93-41344 pressurized lunar surface operation rover Air Handling and Atmosphere Conditioning systems for The psychological effects of isolation on a space station p316 N93-28032 manned spacecraft - A design and performance data - A simulation study LUNAR SHELTERS survey [SAE PAPER 921191] p 287 A93-41369 Conceptual study on manned lunar surface site [SAE PAPER 921350] p 306 A93-41509 Crop interactions in polyculture and their implications p316 N93-28029 Modeling of membrane processes tor air revitalization for CELSS design LUNAR SOIL and water recovery [SAE PAPER 921197] p 295 A93-41373 Oxygen production on the Lunar materials processing [SAE PAPER 921352] p 306 A93-41511 Instrumentation for microbial monitoring of frontier p315 N93-27967 Plant canopy transpiration in bioregenerative life support decontamination or biocide system effectiveness LUNAR SURFACE systems - The link between mechanistic and empirical [SAE PAPER 921233] p 297 A93-41407 Lunar base thermal management/power system models Space Station Freedom food management analysis and design p315 N93-27985 [SAE PAPER 921355] p 306 A93-41514 [SAE PAPER 921248] p 298 A93-41419 LUNGS Biomass productivity and sustainability of a An assessment of waste processing/resource recovery Evaluation of NO(x)-induced toxicity bioregenerative life-support system technologies for lunar/Mars life applications [AD-A261034] p 283 N93-28122 [SAE PAPER 921359] p 307 A93-41518 [SAE PAPER 921271] p 300 A93-41441 LYMPHOCYTES Regenerative Life Support Systems Test Bed Test of the Shuttle Extended Duration Orbiter (EDO) Flow cytometric analysis of lymphocyte surface markers performance - Lettuce crop characterization Waste Collection Subsystem (WCS) following a 1-Gy dose of gamma radiation [SAE PAPER 921391] p 309 A93-41549 [SAE PAPER 921346] p 305 A93-41505 p281 A93-41170 Experimental and theoretical study on membrane Water reclamation technology development lor future distillation using thermopervaporation long range missions [SAE PAPER 921397] p 309 A93-41554 [SAE PAPER 921351 ] p 306 A93-41510 M Hermes ECLSS • Main requirements and technical NASA Specialized Center for Research and Training MAGNETIC RESONANCE solutions (NSCORT) in space environmental health Mapping of electrical muscle stimulation using MRI [SAE PAPER 921400] p 309 A93-41555 [SAE PAPER 921358] p 307 A93-41S17 p279 A93-40549 1991 NASA Life Support Systems Analysis workshop Contaminant distribution and accumulation in water A feasibility study of hand kinematics for EVA analysis [NASA-CR-4466] p 310 N93-27100 recycle systems using magnetic resonance imaging 1992 NASA Life Support Systems Analysis workshop [SAE PAPER 921360] p 307 A93-41519 | SAE PAPER 921253] p 298 A93-41423 [NASA-CR-4467] p 310 N93-27101 LOW PRESSURE Environmental control and life support system Growing wheat to maturity in reduced gas pressures EVA Glove Research Team [NASA-CR-193014] p313 N93-27847 p311 N93-27718 [NASA-CR-193245] p 277 N93-29216 A feasibility study of hand kinematics for EVA analysis Environmental control and life support system LOWER BODY NEGATIVE PRESSURE using magnetic resonance imaging p 313 N93-27848 evolution p311 N93-27719 Orthostatic intolerance during a 13-day bed rest does Technologies for ECLSS evolution not result from increased leg compliance MAN MACHINE SYSTEMS p 311 N93-27720 p280 A93-41119 Man-systems distributed system for Space Station Freedom p312 N93-27788 The ECLSS advanced automation project evolution and Effects of dynamic exercise on cardiovascular regulation EVA and telerobot interaction p312 N93-27792 technology assessment p312 N93-27723 during lower body negative pressure Man-systems integration and the man-machine Marshall Space Flight Center ECLSS technology p281 A93-41168 interface p313 N93-27795 activities p312 N93-27724 LUNAR BASED EQUIPMENT JSC ECLSS R/T program overview Conceptual study on manned lunar surface site Extravehicular activity technology discipline p312 N93-27725 p 316 N93-28029 p314 N93-27859 Evolving EVA system capability for the evolving Space Conceptual study of manned lunar surface site Manned systems technology discipline Station Freedom requirements p312 N93-27791 p316 N93-28031 p314 N93-27860 Environmental control and life support systems LUNAR BASES Combat Automation for Airborne Weapon Systems: p314 N93-27858 An assessment of waste processing/resource recovery Man/Machine Interface Trends and Technologies Oxygen production on the Lunar materials processing technologies for lunar/Mars life applications [AGARD-CP-520] p317 N93-28850 frontier p315 N93-27967 [SAE PAPER 921271] p 300 A93-41441 Pilot decision aiding for weapon delivery: A novel Assessment of the state of the art in life support A hybrid regenerative water recovery system for approach to fire control cueing using parallel computing environmental control for SEI p 315 N93-27978 lunar/Mars life support applications p317 N93-28853 Dust protection for environmental control and life support [SAE PAPER 921276] p 301 A93-41445 Pilot intent and error recognition as part of a knowledge systems in the lunar environment p315 N93-27979 Hazard and risk assessment for surface components based cockpit assistant P 318 N93-28855 of a lunar base Controlled Ecological Life Support Manned lunar surface site p 316 N93-28033 The design and development of the new RAF standard System HUD format p 318 N93-28856 Evaluation of test methods and requirements for [SAE PAPER 921285] p 302 A93-41451 Virtual interface applications for airborne weapons respiratory protection systems 21 Oxygen production on the Lunar materials processing [AD-A262466] p317 N93-28757 frontier p315 N93-27967 Systems P 318 N93-28858 LINE OF SIGHT SPE water electrolyzers in support of the lunar Operator and automation capability analysis: Picking the Visual field information in nap-of-the-Earth flight by outpost p315 N93-27977 right team p 319 N93-28864 teleoperated helmet-mounted displays Assessment of the state of the art in life support System automation and pilot-vehicle-interface for p311 N93-27177 environmental control for SEI p315 N93-27978 unconstrained low-altitude night attack UPS (ANATOMY) Dust protection for environmental control and life support p 320 N93-28867 Direct measurement of capillary blood pressure in the systems in the lunar environment p315 N93-27979 Overview of cockpit technology research and human lip p 279 A93-40550 Lunar base thermal management/power system development programs for improvement of the LIQUEFACTION anarysis and design p315 N93-27985 man/machine interface: Review of the AGARD AVP Hybrid oxygen system Conceptual study on manned lunar surface site Symposium held in Madrid, May 1992 [AD-A262417] p317 N93-28464 p316 N93-28029 p320 N93-28872

A-10 SUBJECT INDEX MOTION SICKNESS

Anthropometric data from launch and entry suited test Manned lunar surface site: Conceptual study on METAL OXIDES subjects for the design of a recumbent seating system pressurized lunar surface operation rover Development of a regenerate metal oxide sheet matrix [NASA-TM-104769] p 321 N93-29044 p316 N93-28032 CO2 removal system MAN-COMPUTER INTERFACE Computerized atmospheric trace contaminant control [SAE PAPER 921298] p 302 A93-41463 Man-systems distributed system for Space Station simulation for manned spacecraft Portable life support system regenerative carbon dioxide Freedom p312 N93-27788 [NASA-TM-108409] p 321 N93-28977 and water vapor removal by metal oxide absorbents EVA/manned systems p312 N93-27789 MANUALS preprototype hardware development and testing Evolving technologies for Space Station Freedom Life Support and Habitability Manual ESA PSS-03-406 [SAE PAPER 921299] p 303 A93-41464 computer-based workstations p313 N93-27794 [SAE PAPER 921338] p 305 A93-41497 MICROBIOLOGY MARS ENVIRONMENT Man-systems integration and the man-machine Microbiology operations and facilities aboard A study to explore locomotion patterns in partial gravity interface p313 N93-27795 restructured Space Station Freedom environments [SAE PAPER 921213] p 296 A93-41389 Combat Automation for Airborne Weapon Systems: [ SAE PAPER 921157 ] p 293 A93-41340 Effects of refrigerating preinoculated Vitek cards on Man/Machine Interface Trends and Technologies ASDA - Advanced Suit Design Analyzer computer [AGARD-CP-520J p317 N93-28850 microbial physiology and antibiotic susceptibility program [SAE PAPER 921214] p 273 A93-41390 The design and development of the new RAF standard [SAE PAPER 921381] p 308 A93-41539 Microbiological concerns and methodological HUD format p318 N93-28856 MASKS approaches related to bacterial water quality in MANNED MARS MISSIONS Evaluation and optimization of a flexible filtration system Radiation exposure predictions for short-duration stay for respiratory protection system 21 spaceflight [SAE PAPER 921232] p 297 A93-41406 Mars missions [AD-A262467] p 284 N93-28758 [AAS PAPER 92-107] p 277 A93-39261 MATERIAL BALANCE MICROFIBERS Human life support during interplanetary travel and Recycling and source reduction for long duration space Intracellular targeting of the Yersinia YopE cytotoxin in domicile. V - Mars expedition technology trade study for habitation mammalian cells induces actin microfilament disruption solid waste management [SAE PAPER 921121] p 290 A93-41313 [FOA-B-40420-4.4] p 275 N93-27989 [SAE PAPER 921119] p 290 A93-41311 MATERIALS TESTS MICROMETEOROIDS An assessment of waste processing/resource recovery Biodeterioration of materials in water reclamation Enhanced softgoods structures for spacesuit technologies for lunar/Mars life applications systems micrometeoroid/debris protective systems [SAE PAPER 921271] p 300 A93-41441 [SAE PAPER 921311] p 303 A93-41473 [SAE PAPER 921258] p 299 A93-41428 A hybrid regenerative water recovery system for MATHEMATICAL LOGIC MICROORGANISMS lunar/Mars life support applications Crucial role of detailed function, task, timeline, link, and Effects of refrigerating preinoculated Vitek cards on [SAE PAPER 921276] p 301 A93-41445 human vulnerability analyses in HRA microbial physiology and antibiotic susceptibility MANNED REENTRY [DE93-001923] p 321 N93-28942 [SAE PAPER 921214] p 273 A93-41390 Anthropometric data from launch and entry suited test MATHEMATICAL MODELS Instrumentation for microbial monitoring of subjects for the design of a recumbent seating system Comparative test data assessment and simplified math decontamination or biocide system effectiveness [NASA-TM-104769] p 321 N93-29044 modelling for Sabatier CO2 reduction subsystem [SAE PAPER 921233] p 297 A93-41407 MANNED SPACE FLIGHT [SAE PAPER 921228] p 296 A93-41402 Water purification, microbiological control, sterilization Space Station Freedom Environmental Health Care and organic waste decomposition using an electrochemical 1991 NASA Life Support Systems Analysis workshop Program advanced ozonation process [NASA-CR-4466] p 310 N93-27100 [SAE PAPER 921138] p 292 A93-41325 [SAE PAPER 921234] p 297 A93-41408 The psychological effects of isolation on a space station 1992 NASA Life Support Systems Analysis workshop Immobilized cell bioreactors for water reclamation - - A simulation study [NASA-CR-4467] p 310 N93-27101 Process stability and effect of reactor design [SAEPAPER921191] p287 A93-41369 Marshall Space Flight Center ECLSS technology [SAE PAPER 921277] p 301 A93-41446 Crop interactions in polyculture and their implications activities p 312 N93-27724 Contaminant distribution and accumulation in water for CELSS design Biophysical model for handwear insulation testing recycle systems [SAE PAPER 921197] p 295 A93-41373 [AD-A262926I p 320 N93-28884 [SAE PAPER 921360] p 307 A93-41519 A trade study method for determining the design MEMBRANES Process for selectively recovering algae and protozoa parameter of CELSS subsystems Development of membrane gas removal technology for [NASA-CASE-MFS-26124-1-NPO] p 276 N93-29174 [SAE PAPER 921198] p 295 A93-41374 microgravity liquid flow systems MILITARY AVIATION Instrumentation for microbial monitoring of [SAE PAPER 921162] p 294 A93-41344 Prevalence of corrective lens wear in Royal Australian decontamination or biocide system effectiveness Membrane technology for zero gravity life support Air Force flight crews p 289 A93-41173 [SAE PAPER 921233] p 297 A93-41407 systems MILITARY TECHNOLOGY Advanced life support systems in lunar and Martian [SAE PAPER 921320] p 304 A93-41482 Cognitive interface considerations for intelligent environments utilizing a higher plant based engineering Modeling of membrane processes for air revitalization cockpits p319 N93-28865 paradigm and water recovery System automation and pilot-vehicle-interface for [SAE PAPER 921286] p 302 A93-41452 [SAE PAPER 921352] p 306 A93-41511 unconstrained low-altitude night attack p 320 N93-28867 Consumables and wastes estimations for the First Lunar High-recovery low-pressure reverse osmosis A study of the effects of lens focal length on remote Outpost [SAE PAPER 921353] p 306 A93-41512 [SAE PAPER 921287] p 302 A93-41453 driver performance Design and preliminary testing of a membrane based Biofilm formation and control in a simulated spacecraft [AD-A263191] p 321 N93-28941 water system - Three year results water recycling system for European manned space MISSILE CONTROL missions [SAE PAPER 921310] p 303 A93-41472 Pilot decision aiding for weapon delivery: A novel Air Handling and Atmosphere Conditioning systems for [SAE PAPER 921396] p 309 A93-41553 approach to fire control cueing using parallel computing manned spacecraft - A design and performance data Experimental and theoretical study on membrane p317 N93-28853 survey distillation using thermopervaporation MISSION PLANNING [SAE PAPER 921350] p 306 A93-41509 [SAE PAPER 921397] p 309 A93-41554 Manned lunar surface site: Conceptual study on Shielding strategies for human exploration missions MEMORY pressurized lunar surface operation rover [SAE PAPER 921376] p 308 A93-41534 How expert pilots think: Cognitive processes in expert p316 N93-28032 First entry operations for spacecraft decision making Lunar surface experiment system p316 N93-28034 [SAE PAPER 921384] p 308 A93-41542 [DOT/FAA/RD-93/9] p 288 N93-27103 Pilot intent and error recognition as part of a knowledge Potential health hazards from thermal degradation Analysis of neural systems involved in modulation of based cockpit assistant p318 N93-28855 events - Paniculate vs. gas phase effects memory storage MOISTURE CONTENT [SAE PAPER 921388] p 282 A93-41546 [AD-A262418] p 283 N93-27654 Dew point analysis for Space Station Freedom Design and preliminary testing of a membrane based MENTAL PERFORMANCE [ SAE PAPER 921227 ] p 296 A93-41401 water recycling system for European manned space Expertise, text coherence, and constraint satisfaction: MOLDS missions Effects on harmony and settling rate — mental Relative resistance of biofilms and planktonic cells of [SAE PAPER 921396] p 309 A93-41553 representations common molds and yeasts to antimicrobials Evolving EVA system capability for the evolving Space [AD-A262703] p 288 N93-28901 [SAE PAPER 921212] p 273 A93-41388 Station Freedom requirements p312 N93-27791 METABOLISM MOLECULAR BIOLOGY Simplified Aid For Crew Rescue (SAFR) Mathematical model for the exchange of gases in the Proceedings of a Workshop on Molecular Nuclear p313 N93-27793 lungs with special reference to carbon monoxide Medicine Manned systems technology discipline p 271 A93-39707 [DE93-010828] p 285 N93-28835 MOLLUSKS p314 N93-27860 Analysis of the Variable Pressure Growth Chamber using Geography of end-Cretaceous marine bivalve MANNED SPACECRAFT the CASE/A simulation package extinctions p 273 A93-41075 TRIALSS - Tool for Rapid and Intelligent Advanced Life [SAE PAPER 921122] p 291 A93-41314 Support System Selection and Sizing MONITORS Metabolic responses to simulated extravehicular [SAE PAPER 921123] p 291 A93-41315 New technologies for in-flight pasteless bioelectrodes activity Catalytic oxidation for treatment of ECLSS and PMMS p289 A93-41174 [SAE PAPER 921303] p 282 A93-41468 waste streams — Process Material Management Measurement of free and dissolved gas content of water Systems SPE water electrolyzers in support of the lunar samples on Space Station Freedom [SAE PAPER 921274] p 301 A93-41443 outpost p315 N93-27977 [SAE PAPER 921267] p 300 A93-41437 Regenerative Life Support Systems Test Bed Wound healing and connective tissue metabolism: The MOTION PERCEPTION performance - Lettuce crop characterization role of hyperbaric oxygen therapy Effects of long-term weightlessness on roll [ SAE PAPER 921391) p 309 A93-41549 [AD-A262483] p 285 N93-28759 circularvection p 279 A93-39725 EVA/manned systems p312 N93-27789 Regulation of alternative CO2 fixation pathways in MOTION SICKNESS Manned systems technology discipline procaryotic and eucaryotic photosynthetic organisms 8-OH-DPAT does not interfere with habituation to p314 N93-27860 [DE93-012109] p 276 N93-29181 motion-induced emesis in cats p 271 A93-38451

A-11 MULTIPROCESSING (COMPUTERS) SUBJECTINDEX

Neuropharmacology of motion sickness and emesis - NIGHT VISION OXYGEN A review p 271 A93-39711 Evaluation of test methods and requirements lor Oxygen production on the Lunar materials processing Motion sickness induced by sinusoidal linear respiratory protection systems 21 frontier p315 N93-27967 acceleration in rats p 272 A93-39712 [AD-A262466] p 317 N93-28757 OXYGEN CONSUMPTION MULTIPROCESSING (COMPUTERS) Head-steered sensor flight test results and Oxygen regime in the frontal cerebral cortex of monkeys A modular head/eye platform for real-time reactive implications p 318 N93-28859 during a two-week space flight p 272 A93-40773 vision System automation and pilot-vehicle-interface for OXYGEN MASKS [OUEL-1941/92] p320 N93-28897 unconstrained low-altitude night attack Evaluation ol test methods and requirements for MUSCLES p 320 N93-28867 respiratory protection systems 21 Mapping of electrical muscle stimulation using MRI [AD-A262466] p317 N93-28757 NITROGEN OXIDES p279 A93-40549 OXYGEN PRODUCTION Evaluation of NO(x)-induced toxicity Myosin and troponin changes in rat soleus muscle after A low pressure electrolyzer lor the next generation [AD-A261034] p 283 N93-28122 hindlimb suspension p 273 A93-41124 submarine NOREPINEPHRINE Mechanical stimulation of skeletal muscle increases [SAE PAPER 921125] p 291 A93-41316 Norepinephrine content in discrete brain areas and prostaglandin F2(alpha) synthesis and cydooxygenase Oxygen generation by static feedwater electrolysis for neurohypophysial vasopressin in rats after a 9-d spaceflight activity by a pertussis toxin sensitive mechanism Space Station Freedom (SLS-1) p273 A93-41167 [NASA-CR-193041] p 282 N93-27102 [SAE PAPER 921151] p293 A93-41335 NUCLEAR MAGNETIC RESONANCE Intracellular targeting of the Yersinia YopE cytotoxin in OCAM - A CELSS modeling tool: Description and results 13 C NMR spectra of allosteric effectors of mammalian cells induces actin microfilament disruption — Object-oriented Controlled Ecological Life Support hemoglobin [FOA-B-40420-4.4] p 275 N93-27989 System Analysis and Modeling [AD-A262979] p 284 N93-28293 MUSCULAR FATIGUE [SAE PAPER 921241] p 298 A93-41413 NUCLEAR MEDICINE Sudden loading and fatigue effects on the human Regenerative Life Support Systems Test Bed Proceedings of a Workshop on Molecular Nuclear spine performance - Lettuce crop characterization Medicine [PB93-167526] p 286 N93-29199 [SAE PAPER 921391] p 309 A93-41549 [DE93-010828] p 285 N93-28835 MUSCULAR FUNCTION Comparison of portable crewmember protective NUMERICAL CONTROL Growth factor involvement in tension-induced skeletal breathing equipment (CPBE) designs Computerized atmospheric trace contaminant control muscle growth [DOT/FAA/AM-93/6] p310 N93-27121 simulation for manned spacecraft [NASA-CR-193023] p 282 N93-27113 Oxygen production on the Lunar materials processing [NASA-TM-108409] p 321 N93-28977 MUSCULAR STRENGTH frontier p315 N93-27967 NUTRIENTS Aminohydroxybutane bisphosphonate and clenbuterol SPE water electrolyzers in support of the lunar A matrix-based porous tube water and nutrient delivery outpost P315 N93-27977 prevent bone changes and retard muscle atrophy system Hybrid oxygen system respectively in tail-suspended rats p 271 A93-39703 [SAE PAPER 921390] p 309 A93-41548 MUSCULOSKELETAL SYSTEM [AD-A262417] p317 N93-28464 Absence of a growth hormone effect on rat soleus OXYGEN SUPPLY EQUIPMENT atrophy during a 4-day spaceflight p 272 A93-40548 Comparison of portable crewmember protective Mechanical stimulation of skeletal muscle increases breathing equipment (CPBE) designs prostaglandin F2(alpha) synthesis and cydooxygenase OBJECT-ORIENTED PROGRAMMING [DOT/FAA/AM-93/6] P310 N93-27121 activity by a pertussis toxin sensitive mechanism DOKMA: A document oriented communication model Evolution of Space Station EMU PLSS technology [NASA-CR-193041] p 282 N93-27102 for medical applications as a basis ol a role system in recommendations p 312 N93-27790 Growth factor involvement in tension-induced skeletal the medical field Hybrid oxygen system muscle growth [ETN-93-93799] p 284 N93-28469 [AD-A262417] p317 N93-28464 [NASA-CR-193023] p 282 N93-27113 OBSTACLE AVOIDANCE OXYGEN TENSION The physiological limitations of man in the high G A study of the effects of lens focal length on remote Interactions between Hb, Mg, DPG, ATP, and Cl environment p 319 N93-28861 driver performance determine the change in Hb-O2 affinity at high altitude MUTATIONS [AO-A263191] p321 N93-28941 p279 A93-41117 Comparative mutagenesis of human cells in vivo and OCCUPATIONAL DISEASES Space Shuttle Orbiter oxygen partial pressure sensing in vitro Barotrauma in Boeing 737 cabin crew and control system improvements [DE93-012269] p 276 N93-28651 p278 A93-39706 [SAE PAPER 921347] p 305 A93-41506 MYOELECTRICITY OPERATOR PERFORMANCE Mapping of electrical muscle stimulation using MRI Cognitive predictors of vigilance p 287 A93-40771 p 279 A93-40549 Performance under dichoptic versus binocular viewing MYOGLOBIN conditions - Effects of attention and task requirements Myosin and troponin changes in rat soleus muscle after p287 A93-40772 PALEOBIOLOGY hindlimb suspension p 273 A93-41124 OPTICAL MEASUREMENT Microfossils of the Early Archean Apex chert - New Theory of signal detection and its application to visual evidence of the antiquity of life p 272 A93-40308 target acquisition: A review of the literature PALEONTOLOGY N [AD-A262920] p 288 N93-28307 Geography of end-Cretaceous marine bivalve OPTICAL TRACKING NAP-OF-THE-EARTH NAVIGATION extinctions p 273 A93-41075 Dynamic analysis of human visuo-oculo-manual Visual field information in nap-of-the-Earth flight by coordination control in target tracking tasks PARALLEL PROCESSING (COMPUTERS) teleoperated helmet-mounted displays p287 A93-41166 Combat Automation lor Airborne Weapon Systems: p311 N93-27177 OPTIMIZATION Man/Machine Interface Trends and Technologies NASA PROGRAMS An approach to the functional optimization of the CELSS [AGARD-CP-520] p317 N93-28850 Overview of NASA's 1991 Life Support Systems Analysis Test Facility Pilot decision aiding for weapon delivery: A novel Workshop [SAE PAPER 921199] p 295 A93-41375 approach to fire control cueing using parallel computing [SAE PAPER 921118] p 290 A93-41310 ORBITAL SPACE TESTS P317 N93-28853 NASA SPACE PROGRAMS Conceptual design of ECLSS microgravity test beds PARTIAL PRESSURE Human life support during interplanetary travel and [SAE PAPER 921164] p 294 A93-41346 Space Shuttle Orbiter oxygen partial pressure sensing domicile. VI - Generic modular now schematic for hybrid ORGANIC COMPOUNDS and control system improvements physical/chemical-biological life support systems The development and testing ol a volatile organics [SAE PAPER 921347] p 305 A93-41506 [SAE PAPER 921120] p 290 A93-41312 concentrator for use in monitoring Space Station water PARTICULATES NEGATIVE IONS quality Potential health hazards from thermal degradation Regenerable Microbial Check Valve - Life cycle tests [SAE PAPER 921266] p 300 A93-41436 events - Paniculate vs. gas phase effects results Determination of organic carbon and ionic accountability [SAE PAPER 921388] p 282 A93-41546 [SAE PAPER 921316] p 303 A93-41478 ol various waste and product waters derived from ECLSS PAYLOAD INTEGRATION Inactivation of a model coliphage virus in water by water recovery tests and Spacelab humidity condensate Design and evaluation of a payload to support plant iodine [SAE PAPER 921313] p 303 A93-41475 growth onboard COMET 1 [SAE PAPER 921361] p 274 A93-41520 Generation of iodine disinfection by-products (IDP's) in [SAE PAPER 921389] p 308 A93-41547 NEUROLOGY a water recycle system PERFORMANCE PREDICTION Neuropharmacology of motion sickness and emesis - [SAE PAPER 921362] p 307 A93-41521 Structured interviews for pilot selection - No incremental A review p 271 A93-39711 ORTHOSTATIC TOLERANCE validity p 286 A93-39572 Microgravity and orthostatic intolerance - Carotid Case report - Chronic sub-dural hematoma following PERFORMANCE TESTS hemodynamics and peripheral responses high-speed ejection p 282 A93-41171 Development of a test protocol for evaluating EVA glove p278 A93-39716 Secondary injury factors and preventative treatment performance Orthostatic intolerance during a 13-day bed rest does [ PB93-176014 ] p 283 N93-27409 (SAE PAPER 921254] p 298 A93-41424 not result from increased leg compliance NEUROPHYSIOLOGY p280 A93-41119 Performance evaluation of candidate space suit Long-lasting neuropsychological changes after a single OXIDATION elements for the next generation orbital EMU high altitude Climb p 278 A93-39713 Ferrous iron oxidation by anoxygenic phototrophic [ SAE PAPER 921344 ] p 305 A93-41503 Inhibition of EGF-induced signal transduction by bacteria p 271 A93-39280 PERIPHERAL CIRCULATION microgravity is independent of EGF receptor redistribution Post-treatment of reclaimed waste water based on an Microgravity and orthostatic intolerance - Carotid in the plasma membrane of human A431 cells electrochemical advanced oxidation process hemodynamics and peripheral responses p272 A93-39715 [SAE PAPER 921275] p 301 A93-41444 p 278 A93-39716 Analysis of neural systems involved in modulation of Influence of the Cold Buster (tm) sports bar on heat PERSONALITY memory storage debt, mobilization and oxidation ol energy substrates Accident proneness: A research review [AD-A262418] p 283 N93-27654 [AD-A262762] P 285 N93-28939 [DOT/FAA/AM-93/9] p 288 N93-28622

A-12 SUBJECT INDEX PROTECTIVE CLOTHING

PERSONNEL MANAGEMENT Flight deck automation and pilot workload Evaluation of capillary electrophoresis for in-flight ionic Increasing hits and reducing misses in CRM/LOS [SAE PAPER 9211321 p 291 A93-41320 contaminant monitoring of SSF potable water scenarios - Guidelines for simulator scenario Toward a flight deck automation philosophy for the [SAE PAPER 921268] p 300 A93-41438 development p 286 A93-39575 Boeing High Speed Civil Transport Use of sorption technology for treatment of humidity PESTICIDES [SAE PAPER 921133] p 291 A93-41321 condensate for potable water Regenerable biocide delivery unit, volume 2 A study of decision making and performance in rejected [SAE PAPER 921312] p 303 A93-41474 [NASA-CR-185701-VOL-2] p 275 N93-27360 takeoffs Regenerable Microbial Check Valve - Life cycle tests PHARMACOLOGY [SAE PAPER 921134] p 287 A93-41322 results Aminohydroxybutane bisphosphonate and clenbuterol Age 60 Project: Consolidated database experiments [SAE PAPER 921316) p 303 A93-41478 prevent bone changes and retard muscle atrophy [HS-TR-8025-3C(R2)1 p 314 N93-27851 Recovering potable water from wastewater in space respectively in tail-suspended rats p 271 A93-39703 Combat Automation for Airborne Weapon Systems: platforms by tyophilization Toxicokinetics of inhaled bromotrifluoromethane (Halon Man/Machine Interface Trends and Technologies [SAE PAPER 921323] p 304 A93-41485 1301) in human subjects p 278 A93-39705 [AGARD-CP-520] p 317 N93-28850 Generation of iodine disinfection by-products (IDP's) in Pilot decision aiding for weapon delivery. A novel Neuropharmacology o) motion sickness and emesis - a water recycle system approach to fire control cueing using parallel computing A review p 271 A93-39711 [SAE PAPER 921362] p 307 A93-41521 PHOTOCHEMICAL REACTIONS p317 N93-28853 Regenerable biocide delivery unit, volume 1 Ferrous iron oxidation by anoxygenic phototrophic Pilot intent and error recognition as part of a knowledge bacteria p 271 A93-39280 based cockpit assistant p318 N93-28855 [NASA-CR-185701] p 274 N93-27122 PHOTOLYSIS The design and development of the new RAF standard PRESSURE CHAMBERS Water purification, microbiological control, sterilization HUD format p 318 N93-28856 Analysis of the Variable Pressure Growth Chamber using and organic waste decomposition using an electrochemical Symbology for head up and head down applications for the CASE/A simulation package advanced ozonation process highly agile fighter aircraft: To improve spatial awareness, [SAE PAPER 921122] p 291 A93-41314 [SAE PAPER 921234] p 297 A93-41408 trajectory control, and unusual attitude recovery, part 1 PRESSURE EFFECTS PHOTOSYNTHESIS p318 N93-28857 The effects of a reduced pressure scenario on the Regulation of alternative CO2 fixation pathways in The quest for an integrated flying helmet Columbus APM environmental control system procaryotic and eucaryotic photosynthetic organisms p319 N93-28860 [SAE PAPER 921247] p 298 A93-41418 [DE93-012109] p 276 N93-29181 The physiological limitations of man in the high G PRESSURE MEASUREMENT PHYSICAL EXERCISE environment p319 N93-28861 Direct measurement of capillary blood pressure in the Effects of sleep deprivation and exercise on glucose Oculo-motor responses and virtual image displays human lip p 279 A93-40550 tolerance p 281 A93-4116S p319 N93-28862 Computer modeling of the Variable Pressure Growth Effects of dynamic exercise on cardiovascular regulation Human capabilities and limitations in situation Chamber using the CASE/A simulation package during lower body negative pressure awareness p319 N93-28863 [SAE PAPER 921354] p 306 A93-41513 p281 A93-41168 PILOT SELECTION Plant growth modeling at the JSC variable pressure Performance and mood-state parameters during 30-day Structured interviews for pilot selection - No incremental growth chamber - An application of experimental design 6 deg head-down bed rest with exercise training validity p 286 A93-39572 [SAE PAPER 921356] p 307 A93-41515 PILOT TRAINING p281 A93-41169 PRESSURE SENSORS A study of decision making and performance in rejected Simulating reduced gravity - A review of biomechanical Space Shuttle Orbiter oxygen partial pressure sensing takeoffs issues pertaining to human locomotion and control system improvements [SAE PAPER 921134] p 287 A93-41322 p289 A93-41175 [SAE PAPER 921347] p 305 A93-41506 Program development for exercise countermeasures PITUITARY GLAND Power assist EVA glove development [SAE PAPER 921140] p 292 A93-41327 Electrophoretic separation of cells and particles from p 314 N93-27850 PHYSIOLOGICAL DEFENSES rat pituitary and rat spleen Plasmid encoded virulence ol Yersinia [NASA-CR-193073] p 276 N93-28415 PRESSURE VESSELS [FOA-B-40419-4.4] p 275 N93-28199 PITUITARY HORMONES High-recovery low-pressure reverse osmosis PHYSIOLOGICAL EFFECTS Norepinephrine content in discrete brain areas and [SAE PAPER 921353] p 306 A93-41512 Growth factor involvement in tension-induced skeletal neurohypophysial vasopressin in rats after a 9-d spaceflight PRESSURIZED CABINS muscle growth (SLS-1) p273 A93-41167 Labels and visual cues to reproduce an earthlike [NASA-CR-193023] p 282 N93-27113 Electrophoretic separation of cells and particles from environment in space - Going ahead in designing Columbus Variations of time-to-incapacitation and rat pituitary and rat spleen APM interior architecture carboxyhemoglobin values in rats exposed to two carbon [NASA-CR-193073] p 276 N93-28415 [SAE PAPER 921193] p 295 A93-41371 monoxide concentrations PLANKTON Shuttle Orbiter Environmental Control and Life Support [DOT/FAA/AM-93/7] p 274 N93-27152 Relative resistance of biofilms and planktonic cells of System - Flight experience Variations in time-to-incapacitation and blood cynanide common molds and yeasts to antimicrobials [SAE PAPER 921348] p 305 A93-41507 values for rats exposed to two hydrogen cyanide gas [SAE PAPER 921212] p 273 A93-41388 PROBLEM SOLVING concentrations PLANT ROOTS How expert pilots think: Cognitive processes in expert [DOT/FAA/AM-93-8] p 283 N93-27158 A matrix-based porous tube water and nutrient delivery decision making Evaluation of test methods and requirements for system [DOT/FAA/RD-93/9] p 288 N93-27103 respiratory protection systems 21 [SAE PAPER 921390] p 309 A93-41548 PRODUCTION ENGINEERING (AD-A262466] p317 N93-28757 PLANTS (BOTANY) Oxygen production on the Lunar materials processing PHYSIOLOGICAL RESPONSES Biosphere 2 - Overview of system performance during frontier p 315 N93-27967 Human performance and physiological function during the first nine months PROJECT SET! a 24-hr exposure to 1 percent bromotrifluoromethane [SAE PAPER 921129] p 291 A93-41317 Wide-bandwidth high-resolution search for (Halon 1301) p277 A93-39704 Advanced life support systems in lunar and Martian extraterrestrial intelligence The prediction of the adaptation of circadian rhythms environments utilizing a higher plant based engineering [NASA-CR-193137] p 322 N93-28895 to rapid time zone changes p 278 A93-39714 paradigm PROKARYOTES Interactions between Hb, Mg, DPG, ATP, and Cl [SAE PAPER 921286] p 302 A93-41452 Regulation of alternative CO2 fixation pathways in determine the change in Hb-O2 affinity at high altitude Computer modeling of the Variable Pressure Growth procaryotic and eucaryotic photosynthetic organisms p279 A93-41117 Chamber using the CASE/A simulation package [DE93-012109] p 276 N93-29181 Influence of in vivo hypobaric hypoxia on function of [SAE PAPER 921354] p 306 A93-41513 PROSTAGLANDINS lymphocytes, neutrocytes, natural killer cells, and Plant growth modeling at the JSC variable pressure Mechanical stimulation of skeletal muscle increases cytokines p 280 A93-41123 growth chamber - An application of experimental design prostaglandin F2(alpha) synthesis and cyclooxygenase Secondary injury factors and preventative treatment [SAE PAPER 921356] p 307 A93-41515 activity by a pertussis toxin sensitive mechanism [PB93-176014] p283 N93-27409 Regenerative Life Support Systems Test Bed [NASA-CR-193041] p 282 N93-27102 The use of electrophysiological and cognitive variables performance - Lettuce crop characterization PROTECTION in the assessment of degradation during periods of [SAE PAPER 921391] p309 A93-41549 Dust protection for environmental control and life support sustained wakefulness POLLUTION MONITORING systems in the lunar environment p 315 N93-27979 [AD-A263033] p 283 N93-27923 The role of Environmental Health System air quality PROTECTIVE CLOTHING PHYSIOLOGY monitors in Space Station Contingency Operations Glovebox design for Space Station Freedom Crew Effects of refrigerating preinoculated Vitek cards on [SAE PAPER 921414] p 310 A93-41565 Health Care System microbial physiology and antibiotic susceptibility PORTABLE LIFE SUPPORT SYSTEMS [ SAE PAPER 921139 ] p 292 A93-41326 [SAE PAPER 921214] p 273 A93-41390 Comparison of portable crewmember protective The Centrifuge Facility Life Sciences Glovebox PHYTOTRONS breathing equipment (CPBE) designs configuration study Computer modeling of the Variable Pressure Growth [DOT/FAA/AM-93/6] p 310 N93-27121 [SAE PAPER 921158] p 293 A93-41341 Chamber using the CASE/A simulation package Evolution of Space Station EMU PLSS technology Enhanced softgoods structures for spacesuit [SAE PAPER 921354] p 306 A93-41513 recommendations p 312 N93-27790 micrometeoroid/debris protective systems Plant growth modeling at the JSC variable pressure POTABLE WATER [SAE PAPER 921258] p 299 A93-41428 growth chamber - An application of experimental design Phase III Integrated Water Recovery Testing at MSFC Lightweight passive microclimate cooling device (SAE PAPER 921356] p 307 A93-41515 - Closed hygiene and potable loop test results and lesson [AD-A262262] p317 N93-28112 Growing wheat to maturity in reduced gas pressures learned Evaluation of test methods and requirements for [NASA-CR-193245] p 277 N93-29216 [SAE PAPER 921117] p 290 A93-41309 respiratory protection systems 21 PILOT ERROR Process Control Water Quality Monitor for Space Station [AD-A262466] p317 N93-28757 Pilot intent and error recognition as part of a knowledge Freedom - Development update Evaluation and optimization of a flexible filtration system based cockpit assistant p 318 N93-2885S [SAE PAPER 921264] p 299 A93-41434 for respiratory protection system 21 PILOT PERFORMANCE Continuous monitoring of effluent iodine levels of Space [AD-A262467] p 284 N93-28758 Influence of aging and practice on piloting tasks Station water using solid state technology Biophysical model for handwear insulation testing p 286 A93-39708 [SAE PAPER 921265] p 299 A93-41435 [AO-A262926] p 320 N93-28884

A-13 PROTEIN SYNTHESIS SUBJECT INDEX

PROTEIN SYNTHESIS RADIATION HAZARDS A novel membrane device for the removal of water vapor Mechanical stimulation of skeletal muscle increases Shielding strategies for human exploration missions and water droplets from air prostaglandin F2(a!pha) synthesis and cyclooxygenase [SAE PAPER 921376] p 308 A93-41534 I SAE PAPER 921322] p 304 A93-41484 activity by a pertussis toxin sensitive mechanism RADIATION SHIELDING Design and evaluation of a payload to support plant [NASA-CR-193041] p 282 N93-27102 Lunar base thermal management/power system growth onboard COMET 1 PROTEINS analysis and design p 315 N93-27985 [SAE PAPER 9213891 p 308 A93-41547 Intracellular targeting of the Yersinia YopE cytotoxin in RADIO COMMUNICATION The General Purpose Work Station, a spacious mammalian cells induces actin microfilament disruption Influence of aging and practice on piloting tasks microgravity workbench [FOA-B-40420-4.4] p 275 N93-27989 p286 A93-39708 [SAE PAPER 921394] p 309 A93-41552 Plasmid encoded virulence of Yersinia Experimental and theoretical study on membrane RADIO FREQUENCIES (FOA-B-40419-4.4] p 275 N93-28199 distillation using thermopervaporation Instrument-approach-plate design considerations for 13 C NMR spectra of allosteric effectors of [SAE PAPER 9213971 p 309 A93-41554 displaying radio frequencies p 289 A93-39574 hemoglobin Growth factor involvement in tension-induced skeletal [AD-A262979] p 284 N93-28293 RATS muscle growth PROTOTYPES Dark cycle monitoring of biological specimens on Space [NASA-CR-193023] p 282 N93-27113 Sabatier carbon dioxide reduction system for Space Station Freedom Electrophoretic separation of cells and particles from Station Freedom [SAE PAPER 921393] p 274 A93-41551 rat pituitary and rat spleen [SAE PAPER 921189] p 294 A93-41368 Variations of time-to-incapacitation and [NASA-CR-193073] p 276 N93-28415 Development of a test protocol for evaluating EVA glove carboxyhemoglobin values in rats exposed to two carbon Effect of microgravity on several visual functions during performance monoxide concentrations STS Shuttle missions: Visual Function Tester-Model 1 [SAE PAPER 921254] p 298 A93-41424 [DOT/FAA/AM-93/7] p 274 N93-27152 (VFT-1) p284 N93-28740 PROTOZOA Electrophoretic separation of cells and particles from Effect of microgravity on visual contrast threshold during Process for selectively recovering algae and protozoa rat pituitary and rat spleen STS Shuttle missions: Visual Function Tester-Model 2 [NASA-CASE-MFS-26124-1-NPO] p 276 N93-29174 [NASA-CR-193073] p 276 N93-28415 (VFT-2) P284 N93-28741 PSEUDOMONAS REACTION KINETICS Effect of microgravity on the visual near point: Visual Aquatic biofilms and their responses to disinfection and Regenerate biocide delivery unit, volume 2 Function Tester-Model 4 (VFT-4) p 284 N93-28742 invading species [NASA-CR-185701-VOL-2] p 275 N93-27360 NASA supporting studies for microgravity research on [SAE PAPER 921211] p 296 A93-41387 REACTION PRODUCTS eye movements PSYCHOLOGICAL EFFECTS Generation of iodine disinfection by-products (IDP's) in [NASA-CR-193233] p 285 N93-29041 Performance and mood-state parameters during 30-day a water recycle system Anthropometric data from launch and entry suited test 6 deg head-down bed rest with exercise training [SAE PAPER 921362] p 307 A93-41521 subjects for the design of a recumbent seating system p281 A93-41169 REACTOR DESIGN [NASA-TM-104769] p 321 N93-29044 The psychological effects of isolation on a space station Sabatier carbon dioxide reduction system for Space REFRIGERATING - A simulation study Station Freedom Effects of refrigerating preinoculated Vitek cards on [SAE PAPER 921191] p 287 A93-41369 [SAE PAPER 921189] p 294 A93-41368 microbial physiology and antibiotic susceptibility PSYCHOLOGICAL FACTORS [ SAE PAPER 921214 ] p 273 A93-41390 READING Hybrid oxygen system Evaluation of test methods and requirements for Expertise, text coherence, and constraint satisfaction: respiratory protection systems 21 [AD-A262417] p317 N93-28464 Effects on harmony and settling rate — mental [AD-A262466] p 317 N93-28757 REFRIGERATORS representations PSYCHOLOGICAL TESTS Space Station Freedom food management [AD-A262703] p 288 N93-28901 Structured interviews for pilot selection - No incremental [SAE PAPER 921248 J p 298 A93-41419 validity p 286 A93-39572 RECEPTORS (PHYSIOLOGY) REGENERATION (ENGINEERING) 8-OH-DPAT does not interfere with habitation to Long-lasting neuropsychological changes after a single Development of a regenerable metal oxide sheet matrix high altitude climb p 278 A93-39713 motion-induced emesis in cats p 271 A93-38451 CO2 removal system PSYCHOMOTOR PERFORMANCE Neuropharmacology of motion sickness and emesis - [SAE PAPER 921298] p 302 A93-41463 Human performance and physiological function during A review p 271 A93-39711 Biomass productivity and sustainability of a a 24-hr exposure to 1 percent bromotrifluoromethane Inhibition of EGF-induced signal transaction by bioregenerative life-support system (HalOn 1301) p 277 A93-39704 microgravity is independent of EGF receptor redistribution [SAE PAPER 921359] p 307 A93-41518 PSYCHOPHARMACOLOGY in the plasma membrane of human A431 cells Regenerative Life Support Systems Test Bed Analysis of neural systems involved -in modulation of p 272 A93-39715 performance - Lettuce crop characterization memory storage RECIRCULATIVE FLUID FLOW [SAE PAPER 921391] p 309 A93-41549 [AD-A262418] p 283 N93-27654 Effects of air bubble contamination in recirculating water REGENERATIVE FUEL CELLS PSYCHOPHYSIOLOGY loop SPE water electrolyzers in support of the lunar Identification of hazardous awareness states in [SAE PAPER 921282] p 302 A93-41450 Outpost p 315 N93-27977 monitoring environments RECYCLING RELIABILITY [SAE PAPER 921136] p 287 A93-41324 Recycling and source reduction for long duration space Crucial role of detailed function, task, timeline, link, and Theory of signal detection and its application to visual habitation human vulnerability analyses in HRA target acquisition: A review of the literature [SAE PAPER 921121] p 290 A93-41313 [DE93-001923] p 321 N93-28942 [AD-A262920] p 288 N93-28307 Gray water recycling with a unique vapor compression RELIABILITY ANALYSIS PULMONARY CIRCULATION distillation (VCD) design Crucial role of detailed function, task, timeline, link, and Minimal hypoxic pulmonary hypertension in normal [SAE PAPER 921318] p 304 A93-41480 human vulnerability analyses in HRA Tibetans at 3.658 m p 280 A93-41121 REDUCED GRAVITY [DE93-001923] p 321 N93-28942 PULMONARY FUNCTIONS 8-OH-DPAT does not interfere with habituation to RELIEF MAPS Mathematical model for the exchange of gases in the motion-induced emesis in cats p 271 A93-38451 An exploratory study of plan-view terrain displays for lungs with special reference to carbon monoxide Intraocular pressure and retinal vascular changes during air carrier operations p 289 A93-39573 p 271 A93-39707 transient exposure to microgravity p 278 A93-39710 REMOTE CONTROL Response of genioglossus EMG activity to passive tilt Inhibition of EGF-induced signal transduction by A study of the effects of lens focal length on remote in men p 279 A93-41118 microgravity is independent of EGF receptor redistribution driver performance Hypoxic ventilatory responsiveness in Tibetan compared in the plasma membrane of human A431 cells [AD-A263191] p 321 N93-28941 with Han residents of 3,658 m p 280 A93-41120 p272 A93-39715 REMOTE MANIPULATOR SYSTEM PULMONARY LESIONS Microgravity and orthostatic intolerance - Carotid Manned lunar surface site: Conceptual study on Potential health hazards from thermal degradation hemodynamics and peripheral responses pressurized lunar surface operation rover events - Paniculate vs. gas phase effects p278 A93-39716 p 316 N93-28032 [SAE PAPER 921388] p 282 A93-41546 Oxygen regime in the frontal cerebral cortex of monkeys RESCUE OPERATIONS during a two-week space flight p 272 A93-40773 Simplified Aid For Crew Rescue (SAFR) Simulating reduced gravity - A review of biomechanical p313 N93-27793 issues pertaining to human locomotion RESEARCH AND DEVELOPMENT p289 A93-41175 Advanced life support systems in lunar and Martian RADIATION DAMAGE Program development for exercise countermeasures environments utilizing a higher plant based engineering [ SAE PAPER 921140 ] p 292 A93-41327 Photobiological investigations on spores of paradigm Pilot investigation - Nominal crew induced forces in streptomyces griseus [SAE PAPER 921286] p 302 A93-41452 zero-g [ESA-TT-1269] p 277 N93-29274 JPRS report: Science and technology. Central Eurasia: [SAE PAPER 921155] p 293 A93-41338 RADIATION DOSAGE A study to explore locomotion patterns in partial gravity Ufe sciences Radiation exposure predictions for short-duration stay [JPRS-ULS-93-005] p 276 N93-28683 environments Mais, missions [SAE PAPER 921157] p 293 A93-41340 JPRS report Science and technology. Central Eurasia: [AAS PAPER 92-107] p 277 A93-39261 Design of a Shuttle air and water prefilter for reduced Ufe sciences RADIATION EFFECTS gravity operation [JPRS-ULS-92-027] p 276 N93-28684 Flow cytometric analysis of lymphocyte surface markers [SAE PAPER 921161 ] p 294 A93-41343 RESEARCH MANAGEMENT following a 1-Gy dose of gamma radiation Development of membrane gas removal technology for Proceedings of a Workshop on Molecular Nuclear p281 A93-41170 microgravity liquid flow systems Medicine Gene transcription and electromagnetic fields [SAE PAPER 921162] p 294 A93-41344 [DE93-010828] p 285 N93-28835 [DE93-010854] p276 N93-28848 Two phase fluid management for hydroponics RESEARCH VEHICLES Photobiological investigations on spores of [SAE PAPER 921163] P 294 A93-41345 A study of the effects of lens focal length on remote streptomyces griseus Conceptual design of ECLSS microgravity test beds driver performance [ESA-TT-1269] p 277 N93-29274 [SAE PAPER 921164] p 294 A93-41346 [AD-A263191] p 321 N93-28941

A-14 SUBJECT INDEX SPACE STATION FREEDOM

RESPIRATION SEROTONIN SPACE HABITATS Evaluation of test methods and requirements for 8-OH-DPAT does not interfere with habitualion to Recycling and source reduction for long duration space respiratory protection systems 21 motion-induced emesis in cats p 271 A93-38451 habitation [AD-A262466] p317 N93-28757 SERUMS [SAE PAPER 921121] p 290 A93-41313 RESPIRATORS Amino acid sequences for the binding regions in serum Microbiological concerns and methodological Evaluation and optimization of a flexible filtration system albumin proteins approaches related to bacterial water quality in for respiratory protection system 21 [NASA-CASE-MFS-28402-1] p 276 N93-28952 spaceflight [AD-AZ62467] p 284 N93-28758 SERVICE LIFE [SAE PAPER 921232] p 297 A93-41406 RESPIRATORY DISEASES Regenerate biocide delivery unit, volume 1 SPE water electrolyzers in support of the lunar Potential health effects of fume particles on the crew [NASA-CR-185701] p 274 N93-27122 outpost p315 N93-27977 of spacecrafts SHOULDERS Conceptual study on manned lunar surface site [SAE PAPER 921387] p 308 A93-41545 Development of a 500 hPa shoulder joint for the p316 N93-28029 European EVA Space Suit System Evaluation of NO(x).induced toxicity Manned lunar surface site: Conceptual study on [SAE PAPER 921257] p 299 A93-41427 [AD-A261034J p283 N93-28122 pressurized lunar surface operation rover SIGNAL DETECTION RESPIRATORY REFLEXES p316 N93-28032 Increased fire and toxic contaminant detection Hypoxic ventilatory responsiveness in Tibetan compared responsibility by use of distributed, aspirating sensors Lunar surface experiment system p316 N93-28034 with Han residents of 3,658 m p 280 A93-41120 p311 N93-27722 SPACE PERCEPTION RESPIRATORY SYSTEM Theory of signal detection and its application to visual Symbology for head up and head down applications for Evaluation of test methods and requirements for target acquisition: A review of the literature highly agile fighter aircraft: To improve spatial awareness, respiratory protection systems 21 [AD-A262920] p 288 N93-28307 trajectory control, and unusual attitude recovery, part 1 [AD-A262466) p317 N93-28757 SLEEP DEPRIVATION p318 N93-28857 Evaluation and optimization of a flexible filtration system Effects of sleep deprivation and exercise on glucose SPACE PLATFORMS for respiratory protection system 21 tolerance p 281 A93-41165 Recovering potable water from wastewater in space [AD-A262467] p 284 N93-28758 The use of electrophysiological and cognitive variables platforms by lyophilization RETINA in the assessment of degradation during periods of [SAE PAPER 921323] p 304 A93-41485 Intraocular pressure and retinal vascular changes during sustained wakefulness SPACE SHUTTLE MISSIONS transient exposure to microgravity p 278 A93-39710 [AD-A263033] p 283 N93-27923 Operational space human factors - Methodology for a REVERSE OSMOSIS SMOKE DETECTORS DSO - Detailed Supplementary Objective for manned Modeling of membrane processes for air revitalization Increased fire and toxic contaminant detection Shuttle Orbiter missions and water recovery responsibility by use of distributed, aspirating sensors [SAE PAPER 921156] p 293 A93-41339 [SAE PAPER 921352] p 306 A93-41511 p311 N93-27722 Effect of microgravity on several visual functions during High-recovery low-pressure reverse osmosis SOFTWARE ENGINEERING STS Shuttle missions: Visual Function Tester-Model 1 [SAE PAPER 921353] p 306 A93-41512 The ECLSS advanced automation project evolution and (VFT-1) p 284 N93-28740 RIBONUCLEIC ACIDS technology assessment p312 N93-27723 Effect of microgravity on visual contrast threshold during Characterization and classification of strains of SOLAR RADIATION SHIELDING STS Shuttle missions: Visual Function Tester-Model 2 Francisella tularensis isolated in the central Asian focus Radiation exposure predictions for short-duration stay (VFT-2) p 284 N93-28741 of the Soviet Union and in Japan Mars missions [AAS PAPER 92-107] p 277 A93-39261 SPACE SHUTTLE ORBITERS [FOA-B-40421-4.4] p 275 N93-28200 Test of the Shuttle Extended Duration Orbiter (EDO) SOLID WASTES Use of RNA hybridization in the diagnosis of a case of Waste Collection Subsystem (WCS) Human life support during interplanetary travel and ulceroglandular tularemia [SAE PAPER 921346] p 305 A93-41505 domicile. V - Mars expedition technology trade study for [FOA-B-40422-4.4] p 275 N93-28212 solid waste management Space Shuttle Orbiter oxygen partial pressure sensing ROBOT DYNAMICS [SAE PAPER 921119] p 290 A93-41311 and control system improvements EVA and telerobot interaction p312 N93-27792 Test of the Shuttle Extended Duration Orbiter (EDO) [SAE PAPER 921347). p 305 A93-41506 ROBOT SENSORS Waste Collection Subsystem (WCS) Shuttle Orbiler Environmental Control and Life Support A modular head/eye platform for real-time reactive [SAE PAPER 921346] p 305 A93-41505 System - Flight experience vision Alternative processes for water reclamation and solid [SAE PAPER 921348] p 305 A93-41507 [OUEL-1941/92] p 320 N93-28897 waste processing in a physical/chemical bioregenerative SPACE SHUTTLES life support system ' p311 N93-27721 A comparison of two Shuttle launch and entry suits - SORBENTS Reach envelope, isokinetic strength, and treadmill tests Development of a regenerable metal oxide sheet matrix [SAE PAPER 921154] p 293 A93-41337 CO2 removal system Design of a Shuttle air and water prefilter for reduced SABATIER REACTION [SAE PAPER 921298) p 302 A93-41463 gravity operation Sabatier carbon dioxide reduction system for Space SORPTION [SAE PAPER 921161] p 294 A93-41343 Station Freedom Use of sorption technology for treatment of humidity SPACE STATION FREEDOM [SAE PAPER 921189] p 294 A93-41368 condensate for potable water Space Station Water Processor - Current flight design SAFETY [SAE PAPER 921312] p 303 A93-4H74 [SAE PAPER 921112] p 289 A93-41306 Gene transcription and electromagnetic fields SOURCE PROGRAMS Space Station Freedom Environmental Health Care [DE93-010854] p 276 N93-28848 Regenerable biocide delivery unit, volume 2 Program SAFETY MANAGEMENT [NASA-CR-185701-VOL-2] p 275 N93-27360 [SAE PAPER 921138] p 292 A93-41325 Hazard and risk assessment for surface components SPACE ADAPTATION SYNDROME Glovebox design for Space Station Freedom Crew of a lunar base Controlled Ecological Life Support Effects of long-term weightlessness on roll Health Care System System circularvection p 279 A93-39725 [SAE PAPER 921139] p 292 A93-41326 [SAE PAPER 921285] p 302 A93-41451 Oxygen regime in the frontal cerebral cortex of monkeys Program development for exercise countermeasures First entry operations for spacecraft during a two-week space flight p 272 A93-40773 [SAE PAPER 921140] p 292 A93-41327 [SAE PAPER 921384] p 308 A93-41542 Cerebral blood velocity and other cardiovascular Hyperbaric treatment operations aboard Space Station SCHEDULING responses to 2 days of head-down tilt Freedom The use of electrophysiological and cognitive variables p280 A93-41122 [SAE PAPER 921142] p 292 A93-41328- in the assessment of degradation during periods of SPACE DEBRIS The development of an atmosphere composition monitor sustained wakefulness Enhanced softgoods structures for spacesuit for the Environmental Control and Life Support System [AD-A263033] p 283 N93-27923 micrometeoroid/debris protective systems [SAE PAPER 921149] p 292 A93-41333 SENSITIVITY [SAE PAPER 921258] p 299 A93-41428 Oxygen generation by static feedwater electrolysis for Effects of refrigerating preinoculated Vitek cards on Space Shuttle crew compartment Space Station Freedom microbial physiology and antibiotic susceptibility debris-contamination [SAE PAPER 921151] p 293 A93-41335 [SAE PAPER 921214] p 273 A93-41390 [SAE PAPER 921345] p 305 A93-41504 The Centrifuge Facility Life Sciences Glovebox SENSORIMOTOR PERFORMANCE SPACE ENVIRONMENT SIMULATION configuration study Dynamic analysis of human visuo-oculo-manual Metabolic responses to simulated extravehicular [SAE PAPER 921158] p 293 A93-41341 coordination control in target tracking tasks activity Two phase fluid management for hydroponics p287 A93-41166 [SAE PAPER 921303] p 282 A93-41468 (SAE PAPER 921163] p 294 A93-41345 Human capabilities and limitations in situation SPACE ERECTABLE STRUCTURES Initial accomplishments of the Environmental Control awareness p 319 N93-28863 A preliminary structural analysis ol space-based and Life Support System (ECLSS) atmosphere SENSORY PERCEPTION inflatable tubular frame structures p 313 N93-27849 revitalization (AR) predevelopment operational system test Theory of signal detection and its application to visual SPACE EXPLORATION (POST) for the Space Station Freedom (SSF) target acquisition: A review of the literature Shielding strategies for human exploration missions [SAE PAPER 921186] p 294 A93-41365 [AD-A262920] P 288 N93-28307 [SAE PAPER 921376] p 308 A93-41534 Development of the carbon dioxide removal system SEPARATION Assessment of the state of the art in life support blower used on Space Station Freedom Process for selectively recovering algae and protozoa environmental control for SEI p 315 N93-27978 [SAE PAPER 921188] p 294 A93-41367 [NASA-CASE-MFS-26124-1-NPO] p 276 N93-29174 SPACE FLIGHT Labels and visual cues to reproduce an earthlike SEPARATORS Absence of a growth hormone effect on rat soleus environment in space - Going ahead in designing Columbus Zero gravity phase separator technologies - Past, atrophy during a 4-day spaceflight p 272 A93-40548 APM interior architecture present and future Armstrong Laboratory space visual function tester [SAE PAPER 921193] p 295 A93-41371 [SAE PAPER 921160] P 293 A93-41342 program p 284 N93-28739 A systems approach to water recovery testing for space A novel membrane device for the removal of water vapor SPACE FLIGHT FEEDING life support - Initial biomedical results from the ECLSS and water droplets from air Space Station Freedom food management Water Recovery Test and plans for testbed utilization [SAE PAPER 921322] P 304 A93-41484 [SAE PAPER 921248] p 298 A93-41419 [SAE PAPER 921210] p 295 A93-41386

A-15 SPACE STATION PAYLOADS SUBJECT INDEX

Microbiology operations and facilities aboard SPACE STATION PAYLOADS SPACECRAFT CONTAMINATION restructured Space Station Freedom Defining contamination control requirements for Instrumentation for microbial monitoring of [SAE PAPER 921213] p 296 A93-41389 non-human research on Space Station Freedom decontamination or biocide system effectiveness Pressure, composition, and temperature control of cabin [SAE PAPER 921386] p 308 A93-41544 [SAEPAPER921233] p297 A93-41407 atmosphere on Space Station Freedom Environmental control and life support system The development and testing of a volatile organics [SAE PAPER 921216] p 296 A93-41392 evolution p311 N93-27719 concentrator for use in monitoring Space Station water Dew point analysis for Space Station Freedom SPACE STATIONS quality [SAE PAPER 921227] p 296 A93-41401 The psychological effects of isolation on a space station | SAE PAPER 9212661 p 300 A93-41436 Comparative test data assessment and simplified math - A simulation study Space Shuttle crew compartment modelling for Sabatier CO2 reduction subsystem [SAE PAPER 921191] p 287 A93-41369 debris-contamination [SAE PAPER 921228) p 296 A93-41402 [SAE PAPER 9213451 p 305 A93-41504 Biodeterioration of materials in water reclamation Simplified analysis of water distribution for Space Station NASA Specialized Center for Research and Training systems Freedom (NSCORT) in space environmental health [SAE PAPER 921311] p 303 A93-41473 [SAE PAPER 921230] p 296 A93-41404 [SAE PAPER 921358) p 307 A93-41517 Evaluation of the carbon dioxide removal assembly Environmental control and life support system Contaminant distribution and accumulation in water requirements for the Space Station Freedom in the Manned p311 N93-27718 recycle systems Tended Capability through Permanenlly Manned Capability Increased fire and toxic contaminant detection [SAE PAPER 921360) p 307 A93-41519 configurations responsibility by use of distributed, aspirating sensors Space Station Condensing Heat Exchanger biofilm [SAE PAPER 921231 ] p 297 A93-41405 p 311 N93-27722 formation and control evaluation The effects of a reduced pressure scenario on the SPE water electrolyzers in support of the lunar [SAE PAPER 921383] p 308 A93-41541 Columbus APM environmental control system outpost p 315 N93-87977 First entry operations for spacecraft [SAE PAPER 921247] p 298 A93-41418 SPACE SUITS [SAE PAPER 921384] p 308 A93-41542 Space Station Freedom food management A comparison of two Shuttle launch and entry suits - Defining contamination control requirements for [SAE PAPER 921248] p 298 A93-41419 Reach envelope, isokinetic strength, and treadmill tests non-human research on Space Station Freedom Crew Health Care Systems installations for Space (SAE PAPER 921154] p 293 A93-41337 [SAE PAPER 921386] p 308 A93-41544 Station Freedom Development of the Hermes EVA Space Suit Glove Setting Spacecraft Maximum Allowable Concentrations [SAE PAPER 921249] p 298 A93-41420 [SAE PAPER 921256] p 299 A93-41426 for 1 hour or 24 hour contingency exposures to airborne Continuous monitoring of effluent iodine levels of Space Development of a 500 hPa shoulder joint for the chemicals Station water using solid state technology European EVA Space Suit System [SAE PAPER 921410] p310 A93-41564 [SAE PAPER 921265] p 299 A93-41435 [SAE PAPER 921257] p 299 A93-41427 The role of Environmental Health System air quality Measurement of free and dissolved gas content of water Enhanced softgoods structures for spacesuit monitors in Space Station Contingency Operations samples on Space Station Freedom micrometeoroid/debris protective systems [SAE PAPER 921414] p310 A93-41565 [SAE PAPER 921267] p 300 A93-41437 [SAE PAPER 921258] p 299 A93-41428 Evaluation of capillary electrophoresis for in-flight ionic SPACECRAFT DESIGN An approach to the functional optimization of the CELSS contaminant monitoring of SSF potable water Metabolic responses to simulated extravehicular [SAE PAPER 921268] p 300 A93-41438 activity Test Facility [SAE PAPER 921199] p 295 A93-41375 The analytical control program for the NASA Space [SAE PAPER 921303] p 282 A93-41468 Station Freedom Environmental Control and Life Support Performance evaluation of candidate space suit System integration and verification approach for the System (ECLSS) Water Recovery Test elements for the next generation orbital EMU environmental control system of the Columbus Attached [SAE PAPER 921269] p 300 A93-41439 [SAE PAPER 921344] p 305 A93-41503 Pressurised Module The application of filtration technology within the Water SPACEBORNE EXPERIMENTS (SAE PAPER 921261] p 299 A93-41431 Processor on board Space Station Freedom Pilot investigation - Nominal crew induced forces in Manned lunar surface site: Conceptual study on [SAE PAPER 921270] p 300 A93-41440 zero-g pressurized lunar surface operation rover Use of sorption technology for treatment of humidity [SAE PAPER 921155] p 293 A93-41338 P316 N93-28032 condensate for potable water Defining contamination control requirements for SPACECRAFT ENVIRONMENTS [SAE PAPER 921312] p 303 A93-41474 non-human research on Space Station Freedom Space Station Freedom Environmental Health Care Determination of organic carbon and ionic accountability [SAE PAPER 921386] p 308 A93-41544 Program of various waste and product waters derived from ECLSS Design and evaluation of a payload to support plant [SAE PAPER 921138] p 292 A93-41325 water recovery tests and Spacelab humidity condensate growth onboard COMET 1 Zero gravity phase separator technologies - Past, [SAE PAPER 921313] p 303 A93-41475 [SAE PAPER 921389] p 308 A93-41547 present and future Performance evaluation of candidate space suit A matrix-based porous tube water and nutrient delivery [SAE PAPER 921160] p 293 A93-41342 elements for the next generation orbital EMU system Conceptual design of ECLSS microgravity test beds [SAE PAPER 921344) p 305 A93-41503 [SAE PAPER 921390] p 309 A93-41548 [ SAE PAPER 921164) p 294 A93-41346 Space Station Condensing Heat Exchanger biofilm Lunar surface experiment system p 316 N93-28034 Sabatier carbon dioxide reduction system for Space formation and control evaluation SPACECRAFT CABIN ATMOSPHERES Station Freedom [SAE PAPER 921383] p 308 A93-41541 The development of an atmosphere composition monitor [SAE PAPER 921189] p 294 A93-41368 Defining contamination control requirements for for the Environmental Control and Life Support System System integration and verification approach for the non-human research on Space Station Freedom [SAE PAPER 921149] p 292 A93-41333 environmental control system of the Columbus Attached [SAE PAPER 921386] p 308 A93-41544 Pressure, composition, and temperature control of cabin Pressurised Module Dark cycle monitoring of biological specimens on Space atmosphere on Space Station Freedom [SAE PAPER 921261] p 299 A93-41431 Station Freedom [SAE PAPER 921216] p 296 A93-41392 The development and testing of a volatile organics [SAE PAPER 921393] p 274 A93-41551 Evaluation of the carbon dioxide removal assembly concentrator for use in monitoring Space Station water The role of Environmental Health System air quality requirements for the Space Station Freedom in the Manned quality monitors in Space Station Contingency Operations Tended Capability through Permanently Manned Capability [SAE PAPER 921266] p 300 A93-41436 [SAE PAPER 921414] p 310 A93-41565 configurations Regenerable biocide delivery unit, volume 1 [SAE PAPER 921231] p 297 A93-41405 The analytical control program for the NASA Space [NASA-CR-185701] p 274 N93-27122 Operation of a breadboard Station Freedom Environmental Control and Life Support Environmental control and life support system liquid-sorbent/membrane-contactor system for removing System (ECLSS) Water Recovery Test evolution p311 N93-27719 carbon dioxide and water vapor from air [SAE PAPER 921269] p 300 A93-41439 Technologies for ECLSS evolution [SAE PAPER 921321) p 304 A93-41483 Environmental control of the Mini Pressurized Logistic p 311 N93-27720 Space Shuttle crew compartment Module Alternative processes for water reclamation and solid debris-contamination [SAE PAPER 921281 ] p 302 A93-41449 waste processing in a physical/chemical bioregenerative [SAE PAPER 921345] p 305 A93-41504 SPACECRAFT EQUIPMENT life support system p 311 N93-27721 Space Shuttle Ortaiter oxygen partial pressure sensing Lunar surface experiment system p 316 N93-28034 The ECLSS advanced automation project evolution and and control system improvements SPACECRAFT INSTRUMENTS technology assessment p 312 N93-27723 [SAE PAPER 921347] p 305 A93-41506 Lunar surface experiment system p 316 N93-28034 Marshall Space Flight Center ECLSS technology Shuttle Orbiter Environmental Control and Life Support SPACECRAFT MODULES activities p 312 N93-27724 System - Flight experience Labels and visual cues to reproduce an earthlike JSC ECLSS R/T program overview [SAE PAPER 921348] p 305 A93-41507 environment in space - Going ahead in designing Columbus p312 N93-27725 Air Handling and Atmosphere Conditioning systems for APM interior architecture Extravehicular activity system p 312 N93-27787 manned spacecraft - A design and performance data [SAE PAPER 921193] p 295 A93-41371 Man-systems distributed system for Space Station survey The effects of a reduced pressure scenario on the Freedom p 312 N93-27788 [SAE PAPER 921350] p 306 A93-41509 Columbus APM environmental control system Evolution of Space Station EMU PLSS technology NASA Specialized Center for Research and Training [SAE PAPER 921247] p 298 A93-41418 (NSCORT) in space environmental health recommendations p 312 N93-27790 Environmental control of the Mini Pressurized Logistic [SAE PAPER 921358] p 307 A93-41517 Simplified Aid For Crew Rescue (SAFR) Module The General Purpose Work Station, a spacious p 313 N93-27793 [SAE PAPER 921281] p 302 A93-41449 microgravity workbench Evolving technologies for Space Station Freedom [SAE PAPER 921394] p 309 A93-41552 Evolving technologies for Space Station Freedom computer-based workstations p 313 N93-27794 Setting Spacecraft Maximum Allowable Concentrations computer-based workstations p 313 N93-27794 Environmental control and life support systems for 1 hour or 24 hour contingency exposures to airborne SPACECRAFT POWER SUPPLIES p 314 N93-27858 chemicals Evolution of Space Station EMU PLSS technology Extravehicular activity technology discipline [SAE PAPER 921410] p310 A93-41564 recommendations p 312 N93-27790 p314 N93-27859 The role of Environmental Health System air quality SPACECRAFT SHIELDING Manned systems technology discipline monitors in Space Station Contingency Operations Shielding strategies for human exploration missions p 314 N93-27860 [SAE PAPER 921414] p 310 A93-41565 [SAE PAPER 921376] p 308 A93-41534

A-16 SUBJECT INDEX THRUST VECTOR CONTROL

SPACECREWS SYMBOLS TECHNOLOGICAL FORECASTING Glovebox design lor Space Station Freedom Crew Symbology for head up and head down applications for Water reclamation technology development for future Health Care System highly agile fighter aircraft: To improve spatial awareness, long range missions [SAE PAPER 9211391 p 292 A93-41326 trajectory control, and unusual attitude recovery, part 1 [SAE PAPER 921351] p 306 A93-41510 A comparison of two Shuttle launch and entry suits - p 318 N93-28857 TECHNOLOGY ASSESSMENT Reach envelope, isokinetic strength, and treadmill tests SYNTHESIS (CHEMISTRY) 1991 NASA Life Support Systems Analysis workshop ISAE PAPER 921154] p 293 A93-41337 Development of the nitrogen fixation system for [NASA-CR-4466] p310 N93-27100 Potential health effects of fume particles on the crew CELSS 1992 NASA Life Support Systems Analysis workshop of spacecrafts [ SAE PAPER 921238 ] p 297 A93-41411 [NASA-CR-4467] p 310 N93-27101 [SAE PAPER 921387] p 308 A93-41545 13 C NMR spectra of allosteric effectors of The ECLSS advanced automation project evolution and SPACELAB PAYLOADS hemoglobin technology assessment p312 N93-27723 [AD-A262979] p 284 N93-28293 The General Purpose Work Station, a spacious Assessment of the state of the art in life support SYNTHETIC FUELS microgravity workbench environmental control for SEI p315 N93-27978 Introductions to the Proceedings of the Fourteenth | SAE PAPER 921394] p 309 A93-41552 TECHNOLOGY UTILIZATION SPECIFICATIONS Symposium on Biotechnology for Fuels and Chemicals [DE93-006235] p 276 N93-28890 JPRS report: Science and technology. Central Eurasia: Specification of adaptive aiding systems Life sciences SYSTEMS ANALYSIS [AD-A263071] p314 N93-27927 [JPRS-ULS-93-005] p 276 N93-28683 Overview of NASA's 1991 Life Support Systems Analysis SPECTRUM ANALYSIS Workshop JPRS report: Science and technology. Central Eurasia: 13 C NMR spectra of allosteric effectors of [SAE PAPER 921118] p 290 A93-41310 Life sciences hemoglobin [JPRS-ULS-92-027] p 276 N93-28684 [AD-A262979] p 284 N93-28293 TRIALSS - Tool for Rapid and Intelligent Advanced Life Support System Selection and Sizing TELEOPERATORS SPEECH RECOGNITION [SAE PAPER 921123) p 291 A93-41315 A study of the effects of lens focal length on remote Evolving technologies for Space Station Freedom driver performance 1991 NASA Life Support Systems Analysis workshop computer-based workstations p313 N93-27794 [AD-A263191] p 321 N93-28941 [NASA-CR-4466] p 310 N93-27100 SPINAL CORD TELEROBOTICS 1992 NASA Life Support Systems Analysis workshop Secondary injury factors and preventative treatment EVA and telerobot interaction p312 N93-27792 [NASA-CR-4467] p 310 N93-27101 [PB93-176014] p283 N93-27409 TEMPERATURE CONTROL SPINE Lunar base thermal management/power system Analysis of the Variable Pressure Growth Chamber using Sudden loading and fatigue effects on the human analysis and design p315 N93-27985 the CASE/A simulation package spine SYSTEMS ENGINEERING [SAE PAPER 921122] p 291 A93-41314 [PB93-167526] p 286 N93-29199 Functions simulation model of integrated regenerable Pressure, composition, and temperature control of cabin SPORES life support system atmosphere on Space Station Freedom Altered immunological response in mice subjected to [SAE PAPER 921201) p 295 A93-41377 [SAE PAPER 921216] p 296 A93-41392 stress and exposed to fungal spores Simplified analysis of water distribution for Space Station Environmental control of the Mini Pressurized Logistic [SAE PAPER 921215] p 274 A93-41391 Freedom Module Photobiological investigations on spores of [SAE PAPER 921230] p 296 A93-41404 [SAE PAPER 921281] p 302 A93-41449 streptomyces griseus Evaluation of the carbon dioxide removal assembly Metabolic responses to simulated extravehicular [ESA-TT-1269] p 277 N93-29274 requirements for the Space Station Freedom in the Manned activity STAPHYLOCOCCUS Tended Capability through Permanently Manned Capability [SAE PAPER 921303] p 282 A93-41468 Aquatic biofilms and their responses to disinfection and configurations ASDA - Advanced Suit Design Analyzer computer invading species [SAE PAPER 921231 ] p 297 A93-41405 program [SAE PAPER 921211] p 296 A93-41387 Design and preliminary testing of a membrane based [ SAE PAPER 921381 ] p 308 A93-41539 Space Station Condensing Heat Exchanger biofilm STATISTICAL ANALYSIS water recycling system for European manned space formation and control evaluation Age 60 Project: Consolidated database experiments missions (SAE PAPER 921383] p 308 A93-41541 [HS-TR-8025-3C(R2(] p 314 N93-27851 [SAE PAPER 921396] p 309 A93-41553 Hermes ECLSS - Main requirements and technical Environmental control and life support system STATISTICAL DECISION THEORY p311 N93-27718 Theory of signal detection and its application to visual solutions [SAE PAPER 921400] p 309 A93-41555 Lunar base thermal management/power system target acquisition: A review of the literature analysis and design p315 N93-27985 Specification of adaptive aiding systems [AD-A262920] p 288 N93-28307 Manned lunar surface site p316 N93-28033 [AD-A263071] p 314 N93-27927 STERILIZATION TEMPERATURE EFFECTS Water purification, microbiological control, sterilization Operator and automation capability analysis: Picking the Lunar base thermal management/power system and organic waste decomposition using an electrochemical right team p 319 N93-28864 analysis and design p315 N93-27985 advanced ozonation process System automation and pilot-vehicle-interface for TERRAIN ANALYSIS [SAE PAPER 921234] p 297 A93-41408 unconstrained low-altitude night attack An exploratory study of plan-view terrain displays for STIMULATION p 320 N93-28867 air carrier operations p 289 A93-39573 Mapping of electrical muscle stimulation using MRI Overview of cockpit technology research and TEST FACILITIES p 279 A93-40549 development programs for improvement of the An approach to the functional optimization of the CELSS Mechanical stimulation of skeletal muscle increases man/machine interface: Review of the AGARD AVP Test Facility prostaglandin F2(alpha) synthesis and cydooxygenase Symposium held in Madrid, May 1992 [SAE PAPER 921199] p 295 A93-41375 activity by a pertussis toxin sensitive mechanism p320 N93-28872 TEST STANDS [NASA-CR-193041] p 282 N93-27102 SYSTEMS INTEGRATION European involvement in CELSS - Definition of a Closed STREPTOMYCETES Overview of NASA's 1991 Life Support Systems Analysis Ecological Systems Test Bed Photobiological investigations on spores of Workshop [SAE PAPER 921200] p 295 A93-41376 streptomyces griseus [SAE PAPER 921118] p 290 A93-41310 THERAPY [ESA-TT-1269] p 277 N93-29274 Environmental control and life support system Wound healing and connective tissue metabolism: The STRESS (PHYSIOLOGY) evolution p311 N93-27719 role of hyperbaric oxygen therapy Altered immunological response in mice subjected to Combat Automation for Airborne Weapon Systems: [AD-A262483] p 285 N93-28759 stress and exposed to fungal spores Man/Machine Interface Trends and Technologies THERMAL ANALYSIS [SAE PAPER 921215] p 274 A93-41391 [AGARD-CP-520] p 317 N93-28850 Lunar base thermal management/power system STRUCTURAL DESIGN CRITERIA analysis and design p315 N93-27985 SYSTEMS SIMULATION A trade study method for determining the design THERMAL COMFORT Functions simulation model of integrated regenerable parameter of CELSS subsystems Metabolic responses to simulated extravehicular life support system [SAE PAPER 921198] p 295 A93-41374 activity [SAE PAPER 921201] p 295 A93-41377 Power assist EVA glove development [SAE PAPER 921303] p 282 A93-41468 [SAE PAPER 921255] p 299 A93-41425 THERMAL INSULATION SUBMARINES Lunar base thermal management/power system A low pressure electrolyzer for the next generation analysis and design p 315 N93-27985 submarine THERMAL RESISTANCE TAKEOFF [SAE PAPER 921125] p 291 A93-41316 Biophysical model for handwear insulation testing A study of decision making and performance in rejected SUBSTRATES [AD-A262926] p 320 N93-28884 takeofis Influence of the Cold Buster (tm) sports bar on heat THERMOCHEMISTRY [SAE PAPER 921134] p 287 A93-41322 debt, mobilization and oxidation of energy substrates Oxygen production on the Lunar materials processing [AD-A262762] p 285 N93-28939 TARGET ACQUISITION frontier p315 N93-27967 SURVEYS Theory of signal detection and its application to visual THIN FILMS Anthropometric survey of the astronaut applicants and target acquisition: A review of the literature Membrane technology for zero gravity life support astronauts from 1985 to 1991 [AD-A262920] p 288 N93-28307 systems [NASA-RP-1304] p 321 N93-29324 TARGET RECOGNITION [SAE PAPER 921320] p 304 A93-41482 SURVIVAL Theory of signal detection and its application to visual THIOUREAS Altering the position of the first horizontal cleavage target acquisition: A review of the literature 13 C NMR spectra of allosteric effectors of furrow of the amphibian (Xenopus) egg reduces embryonic [AD-A262920] p 288 N93-28307 hemoglobin survival p 272 A93-39717 TARGETS [AD-A262979] p 284 N93-28293 Biosphere 2 - Overview of system performance during Dynamic analysis of human visuo-oculo-manual THRUST VECTOR CONTROL the first nine months coordination control in target tracking tasks Requirements for pilot assistance in a thrust-vectoring [SAE PAPER 921129] p 291 A93-41317 p287 A93-41166 combat aircraft p 320 N93-28870

A-17 THRUSTORS SUBJECT1NDEX

THRUSTORS ULTRAVIOLET RADIATION VISUAL ACUITY Simplified Aid For Crew Rescue (SAFR) Photobiological investigations on spores of Armstrong Laboratory space visual function tester p 313 N93-27793 streptomyces griseus program p 284 N93-28739 TIME DEPENDENCE [ESA-TT-1269] p 277 N93-29274 Effect of microgravity on several visual functions during The prediction of the adaptation of Orcadian rhythms UREAS STS Shuttle missions: Visual Function Tester-Model 1 to rapid time zone changes p 278 A93-39714 13 C NMR spectra of allosteric effectors of (VFT-1) p 284 N93-28740 TISSUES (BIOLOGY) hemoglobin VISUAL CONTROL Wound healing and connective tissue metabolism: The (AD-A262979) p 284 N93-28293 Dynamic analysis of human visuo-oculo-manual role of hyperbaric oxygen therapy URINE coordination control in target tracking tasks [AD-A262483] p 285 N93-28759 An update on the readiness of vapor compression p287 A93-41166 TORSO distillation for spacecraft wastewater processing VISUAL DISCRIMINATION Sudden loading and fatigue effects on the human [ SAE PAPER 921114] p 290 A93-41307 Visualization and modeling of factors influencing visibility spine in computer-aided crewstation design Concept of waste transferring mechanisms [PB93-167526] p 286 N93-29199 [SAE PAPER 921135] p 292 A93-41323 [SAE PAPER 921239] p 297 A93-41412 TOXIC HAZARDS VISUAL FIELDS Potential health effects of fume particles on the crew Visual field information in nap-of-the-Earth flight by of spacecrafts teleoperated helmet-mounted displays (SAE PAPER 921387) p 308 A93-41545 p311 N93-27177 Potential health hazards from thermal degradation VACUUM VISUAL PERCEPTION events - Paniculate vs. gas phase effects Photobiological investigations on spores of Effect of microgravity on the visual near point: Visual [SAE PAPER 921388] p 282 A93-41546 streptomyces griseus Function Tester-Model 4 (VFT-4) p 284 N93-28742 Variations in time-to-incapacitation and blood cynanide [ESA-TT-1269] p277 N93-29274 Head mounted displays for virtual reality values for rats exposed to two hydrogen cyanide gas VACUUM CHAMBERS [AD-A263498] p 322 N93-29340 concentrations Growing wheat to maturity in reduced gas pressures VISUAL SIGNALS [DOT/FAA/AM-93-8] p 283 N93-27158 [NASA-CR-193245] P 277 N93-29216 Theory of signal detection and its application to visual Evaluation of NO(x)-induced toxidty VASOCONSTRICTION target acquisition: A review of the literature [AD-A261034] p 283 N93-28122 Norepinephrine content in discrete brain areas and [AD-A262920] p 288 N93-28307 TOXICITY neurohypophysial vasopressin in rats after a 9-d spaceflight VISUAL TASKS Human performance and physiological function during (SLS-1) P273 A93-41167 Performance under dichoptic versus binocular viewing a 24-hr exposure to 1 percent bromotrifluoromethane VEGETABLES conditions - Effects of attention and task requirements (Halon 1301) p 277 A93-39704 Plant growth modeling at the JSC variable pressure p 287 A93-40772 TOXICITY AND SAFETY HAZARD growth chamber - An application of experimental design Effect of microgravity on visual contrast threshold during Setting Spacecraft Maximum Allowable Concentrations [SAE PAPER 921356] p 307 A93-41515 STS Shuttle missions: Visual Function Tester-Model 2 for 1 hour or 24 hour contingency exposures to airborne Tests characterizing bioprocessor hardware for (VFT-2) p 284 N93-28741 chemicals analytical modeling Human capabilities and limitations in situation [SAE PAPER 921410] p 310 A93-41564 [SAE PAPER 921357] p 307 A93-41516 awareness p319 N93-28863 Variations in time-to-incapacitation and blood cynanide VEGETATION GROWTH VOMITING values for rats exposed to two hydrogen cyanide gas Hazard and risk assessment for surface components Neuropharmacology of motion sickness and emesis - concentrations of a lunar base Controlled Ecological Life Support A review p 271 A93-39711 [DOT/FAA/AM-93-8] p 283 N93-27158 System VULNERABILITY TOXICOLOGY [SAE PAPER 921285] p 302 A93-41451 Crucial role of detailed function, task, timeline, link, and Toxicokinetics of inhaled bromotrifluoromethane (Halon Design and evaluation of a payload to support plant human vulnerability analyses in HRA 1301) in human subjects p 278 A93-39705 growth onboard COMET 1 [DE93-001923] p 321 N93-28942 TOXINS AND ANTITOXINS [SAE PAPER 921389] p 308 A93-41547 Intracellular targeting of the Yersinia YopE cytotoxin in A matrix-based porous tube water and nutrient delivery mammalian cells induces actin microfilament disruption system w [FOA-B-40420-4.4] p 275 N93-27989 [ SAE PAPER 921390) p 309 A93-41548 TRACE CONTAMINANTS Growing wheat to maturity in reduced gas pressures WAKEFULNESS Computerized atmospheric trace contaminant control [NASA-CR-193245] P 277 N93-29216 The use of electrophysiological and cognitive variables simulation for manned spacecraft VERTICAL ORIENTATION in the assessment of degradation during periods ol [NASA-TM-108409] p 321 N93-28977 Effects of long-term weightlessness on roll sustained wakefulness TRAINING EVALUATION circularvection p 279 A93-39725 [AD-A263033] p 283 N93-27923 Increasing hits and reducing misses in CRM/LOS VIBRATION EFFECTS WASTE DISPOSAL scenarios - Guidelines for simulator scenario Pilot investigation - Nominal crew induced forces in Concept of waste transferring mechanisms development p 286 A93-39575 zero-g [SAE PAPER 921239] p 297 A93-41412 TRAJECTORY CONTROL [SAE PAPER 921155] p 293 A93-41338 OCAM - A CELSS modeling tool: Description and results Symbology for head up and head down applications for VIBRATION TESTS — Object-oriented Controlled Ecological Life Support highly agile fighter aircraft: To improve spatial awareness, A preliminary structural analysis of space-based System Analysis and Modeling trajectory control, and unusual attitude recovery, part 1 inflatable tubular frame structures p313 N93-27849 [SAE PAPER 921241] p 298 A93-41413 p 318 N93-28857 VIDEO COMMUNICATION Catalytic oxidation for treatment of ECLSS and PMMS TRANSPIRATION Evolving technologies for Space Station Freedom waste streams — Process Material Management Plant canopy transpiration in bioregenerative life support computer-based workstations p 313 N93-27794 Systems systems - The link between mechanistic and empirical VIDEO EQUIPMENT [SAE PAPER 921274] p 301 A93-41443 models Method of encouraging attention by correlating video [SAE PAPER 921355] p 306 A93-41514 game difficulty with attention level Consumables and wastes estimations for the First Lunar TRANSPORT AIRCRAFT [NASA-CASE-LAR-15022-1] p 288 N93-28128 Outpost An exploratory study of plan-view terrain displays for VIRAL DISEASES [SAE PAPER 921287] p 302 A93-41453 air carrier operations p 289 A93-39573 Inactivation of a model coliphage virus in .water by Test of the Shuttle Extended Duration Orbiter (EDO) Toward a flight deck automation philosophy lor the iodine Waste Collection Subsystem (WCS) Boeing High Speed Civil Transport [SAE PAPER 921361] p 274 A93-41520 [ SAE PAPER 921346 ] p 305 A93-41505 [SAE PAPER 921133] p 291 A93-41321 VIRTUAL REALITY WASTE TREATMENT TURBOGENERATORS Virtual interface applications for airborne weapons Human life support during interplanetary travel and Lunar base thermal management/power system systems p318 N93-28858 domicile. V - Mars expedition technology trade study for analysis and design p 315 N93-27985 Head mounted displays for virtual reality solid waste management [AD-A263498] p 322 N93-29340 [SAE PAPER 921119) p 290 A93-41311 TWO PHASE FLOW Zero gravity phase separator technologies - Past, VIRULENCE An assessment of waste processing/resource recovery present and future Intracellular targeting of the Yersinia YopE cytotoxin in technologies for lunar/Mars life applications mammalian cells induces actin microfilament disruption (SAE PAPER 921160] p 293 A93-41342 [SAE PAPER 921271] p 300 A93-41441 [FOA-B-40420-4.4] p 275 N93-27989 Anaerobic treatment of organic wastes from Controlled Two phase fluid management for hydroponics Plasmid encoded virulence of Yersinia [SAE PAPER 921163] p 294 A93-41345 Ecological Life Support Systems [FOA-B-40419-4.4] p 275 N93-28199 [SAE PAPER 921272] p 301 A93-41442 Effects of air bubble contamination in recirculating water VISION Determination of organic carbon and ionic accountability loop Contact lenses in aviation - The Marine Corps [SAE PAPER 921282] p 302 A93-41450 of various waste and product waters derived from ECLSS experience p 289 A93-41172 water recovery tests and Spacelab humidity condensate Prevalence of corrective lens wear in Royal Australian [SAE PAPER 921313] p 303 A93-41475 Air Force flight crews p 289 A93-41173 Environmental control and life support system U Armstrong Laboratory space visual function tester p311 N93-27718 program p 284 N93-28739 ULCERS Effect of microgravity on several visual functions during Technologies for ECLSS evolution Use of RNA hybridization in the diagnosis of a case of STS Shuttle missions: Visual Function Tester-Model 1 p311 N93-27720 ulceroglandular tularemia (VFT-1) p 284 N93-28740 JSC ECLSS R/T program overview [FOA-B-40422-4.4] p 275 N93-28212' Effect of microgravity on visual contrast threshold during p312 N93-27725 ULTRASONIC TESTS STS Shuttle missions: Visual Function Tester-Model 2 WASTE WATER New technology for the analysis of the results of an (VFT-2) P 284 N93-28741 An update on the readiness of vapor compression ultrasound experiment performed in aviation-medicine Effect of microgravity on the visual near point: visual distillation for spacecraft wastewater processing medical examination p 279 A93-40774 Function Tester-Model 4 (VFT-4) p 284 N93-28742 [SAE PAPER 921114] p 290 A93-41307

A-18 SUBJECT INDEX YEAST

Post-treatment of reclaimed waste water based on an OCAM - A CELSS modeling tool: Description and results Process Control Water Quality Monitor for Space Station electrochemical advanced oxidation process — Object-oriented Controlled Ecological Life Support Freedom - Development update | SAE PAPER 921275) p 301 A93-41444 System Analysis and Modeling [ SAE PAPER 921264 ] p 299 A93-41434 Immobilized cell bioreactors for water reclamation - [SAE PAPER 921241] p 298 A93-41413 The application of filtration technology within the Water Process stability and effect of reactor design Process Control Water Quality Monitor for Space Station Processor on board Space Station Freedom [SAE PAPER 921277] p 301 A93-41446 Freedom - Development update [SAE PAPER 921270] p 300 A93-41440 Gray water recycling with a unique vapor compression [SAEPAPER921264] p299 A93-41434 Anaerobic treatment of organic wastes from Controlled distillation (VCO) design The development and testing of a volatile organics Ecological Life Support Systems |SAE PAPER 921318] p 304 A93-41480 concentrator for use in monitoring Space Station water [SAE PAPER 921272] p 301 A93-41442 Catalytic oxidation for treatment of ECLSS and PMMS Recovering potable water from wastewater in space quality platforms by lyophilization [SAE PAPER 921266] p 300 A93-41436 waste streams — Process Material Management Systems |SAE PAPER 921323) p 304 A93-41485 The analytical control program for the NASA Space Station Freedom Environmental Control and Life Support (SAE PAPER 921274] p 301 A93-41443 High-recovery low-pressure reverse osmosis System (ECLSS) Water Recovery Test A hybrid regenerative water recovery system for (SAE PAPER 921353) p 306 A93-41512 [SAE PAPER 921269] p 300 A93-41439 lunar/Mars life support applications Generation of iodine disinfection by-products (IDP's) in Catalytic oxidation for treatment of ECLSS and PMMS [SAE PAPER 921276] p 301 A93-41445 a water recycle system waste streams -- Process Material Management Effects of air bubble contamination in recirculating water |SAE PAPER 921362) p 307 A93-41521 Systems loop Environmental control and life support systems [SAE PAPER 921274] p 301 A93-41443 [SAE PAPER 921282] p 302 A93-41450 p 314 N93-27858 Post-treatment of reclaimed waste water based on an Biofilm formation and control in a simulated spacecraft WATER electrochemical advanced oxidation process water system - Three year results A matrix-based porous tube water and nutrient delivery [SAE PAPER 921275] p 301 A93-41444 [SAE PAPER 921310) p 303 A93-41472 system A hybrid regenerative water recovery system for Use of sorption technology for treatment of humidity [SAE PAPER 921390] p 309 A93-41548 lunar/Mars life support applications condensate for potable water WATER CONSUMPTION (SAE PAPER 921276] p 301 A93-41445 ISAE PAPER 921312] p 303 A93-41474 Growing wheat to maturity in reduced gas pressures Immobilized cell bioreactors for water reclamation - Experimental and theoretical study on membrane [NASA-CR-193245] p 277 N93-29216 Process stability and effect of reactor design distillation using thermopervaporation WATER MANAGEMENT [SAE PAPER 921277] p 301 A93-41446 [SAE PAPER 921397] p 309 A93-41554 Space Station Water Processor - Current flight design Biofilm formation and control in a simulated spacecraft WATER VAPOR [SAE PAPER 921112] p 289 A93-41306 water system - Three year results Portable life support system regenerative carbon dioxide [SAE PAPER 921310] p 303 A93-41472 and water vapor removal by metal oxide absorbents Simplified analysis of water distribution for Space Station preprototype hardware development and testing Freedom Biodeterioration of materials in water reclamation systems (SAE PAPER 921299] p 303 A93-41464 [SAE PAPER 921230] p 296 A93-41404 [SAE PAPER 921311] p 303 A93-41473 Water reclamation technology development for future The application of filtration technology within the Water Use of sorption technology for treatment of humidity long range missions Processor on board Space Station Freedom condensate for potable water [SAE PAPER 921351 ] p 306 A93-41510 [SAE PAPER 921270] p 300 A93-41440 [SAE PAPER 921312] p 303 A93-41474 Experimental and theoretical study on membrane Effects of air bubble contamination in recirculating water Determination of organic carbon and ionic accountability distillation using thermopervaporation loop of various waste and product waters derived from ECLSS [SAE PAPER 921397] p 309 A93-41554 [SAE PAPER 921282] p 302 A93-41450 water recovery tests and Spacelab humidity condensate WEAPON SYSTEMS Technologies for ECLSS evolution [SAE PAPER 921313] p 303 A93-41475 Combat Automation for Airborne Weapon Systems: p 311 N93-27720 Regenerable Microbial Check Valve - Life cycle tests Man/Machine Interface Trends and Technologies Alternative processes for water reclamation and solid results [AGARD-CP-520] p317 N93-28850 waste processing in a physical/chemical bioregenerative [SAE PAPER 921316] p 303 A93-41478 Pilot decision aiding for weapon delivery: A novel life support system p 311 N93-27721 Gray water recycling with a unique vapor compression approach to fire control cueing using parallel computing WATER QUALITY distillation (VCD) design p317 N93-28853 Microbiology operations and facilities aboard [SAE PAPER 921318] p 304 A93-41480 Virtual interface applications for airborne weapons restructured Space Station Freedom Membrane technology for zero gravity life support systems p 318 N93-28858 [SAE PAPER 921213] p 296 A93-41389 systems WEAPONS DELIVERY Microbiological concerns and methodological [SAE PAPER 921320] p 304 A93-41482 Pilot decision aiding for weapon delivery: A novel approaches related to bacterial water quality in A novel membrane device for the removal of water vapor approach to fire control cueing using parallel computing spaceflight and water droplets from air p317 N93-28853 [SAE PAPER 921232] p 297 A93-41406 [SAE PAPER 921322] p 304 A93-41484 WEIGHTLESSNESS Recovering potable water from wastewater in space Aminohydroxybutane bisphosphonate and clenbuterol Process Control Water Quality Monitor for Space Station platforms by lyophilization prevent bone changes and retard muscle atrophy Freedom - Development update [SAE PAPER 921323] p 304 A93-41485 respectively in tail-suspended rats p 271 A93-39703 [SAE PAPER 921264] p 299 A93-41434 Water reclamation technology development for future Effects of long-term weightlessness on roll Continuous monitoring of effluent iodine levels of Space long range missions circularvection p 279 A93-39725 Station water using solid state technology [SAE PAPER 921351] p 306 A93-41510 Membrane technology for zero gravity life support [SAE PAPER 921265] p 299 A93-41435 Modeling of membrane processes for air revitalization systems The development and testing of a volatile organics and water recovery [SAE PAPER 921320] p 304 A93-41482 concentrator for use in monitoring Space Station water [SAE PAPER 921352] p 306 A93-41511 WEIGHTLESSNESS SIMULATION quality • High-recovery low-pressure reverse osmosis Simulating reduced gravity - A review of biomechanical [SAE PAPER 921266] p 300 A93-41436 [SAE PAPER 921353] p 306 A93-41512 issues pertaining to human locomotion Measurement of free and dissolved gas content of water Contaminant distribution and accumulation in water p289 A93-41175 samples on Space Station Freedom recycle systems WHEAT [SAE PAPER 921267] p 300 A93-41437 [SAE PAPER 921360] p 307 A93-41519 Growing wheat to maturity in reduced gas pressures Contaminant distribution and accumulation in water Inactivation of a model coliphage virus in water by [NASA-CR-193245] p 277 N93-29216 recycle systems iodine WORKLOADS (PSYCHOPHYSIOLOGY) [SAE PAPER 921360] p 307 A93-41519 [SAE PAPER 921361] p 274 A93-41520 Flight deck automation and pilot workload Inactivation of a model coliphage virus in water by Generation of iodine disinfection by-products (IDP's) in [SAE PAPER 921132] p 291 A93-41320 iodine a water recycle system Pilot decision aiding for weapon delivery: A novel [SAE PAPER 921361 ] p 274 A93-41520 [SAE PAPER 921362) p 307 A93-41521 approach to fire control cueing using parallel computing WATER RECLAMATION Design and preliminary testing of a membrane based p 317 N93-28853 Space Station Water Processor - Current flight design water recycling system for European manned space Human capabilities and limitations in situation [SAE PAPER 921112] p 289 A93-41306 missions awareness p 319 N93-28863 An update on the readiness of vapor compression [SAE PAPER 921396] p 309 A93-41553 WORKSTATIONS The General Purpose Work Station, a spacious distillation for spacecraft wastewater processing Alternative processes for water reclamation and solid microgravity workbench [SAE PAPER 921114] p 290 A93-41307 waste processing in a physical/chemical bioregenerative [SAE PAPER 921394] p 309 A93-41552 Phase III Integrated Water Recovery Testing at MSFC life support system p311 N93-27721 - Closed hygiene and potable loop test results and lesson WOUND HEALING Marshall Space Flight Center ECLSS technology Wound healing and connective tissue metabolism: The learned activities p 312 N93-27724 [SAE PAPER 921117] ' p 290 A93-41309 role of hyperbaric oxygen therapy JSC ECLSS R/T program overview Design of a Shuttle air and water prefilter for reduced [AD-A262483] p 285 N93-28759 p312 N93-27725 gravity operation [SAE PAPER 921161 ] p 294 A93-41343 Environmental control and life support systems A systems approach to water recovery testing for space p 314 N93-27858 life support - Initial biomedical results from the ECLSS WATER TREATMENT YEAST Water Recovery Test and plans for testbed utilization Microbiological concerns and methodological Relative resistance of biofilms and planktonic cells of [SAE PAPER 921210] p 295 A93-41386 approaches related to bacterial water quality in common molds and yeasts to antimicrobials Aquatic biofilms and their responses to disinfection and spaceflight [SAE PAPER 921212] p 273 A93-41388 invading species [SAE PAPER 921232] p 297 A93-41406 [SAE PAPER 921211 ] p 296 A93-41387 Water purification, microbiological control, sterilization Simplified analysis of water distribution for Space Station and organic waste decomposition using an electrochemical Freedom advanced ozonation process [SAE PAPER 921230] p 296 A93-41404 [SAE PAPER 921234] p 297 A93-41408

A-19 PERSONAL AUTHOR INDEX

AEROSPACE MEDICINE AND BIOLOGY / A Continuing Bibliography (Supplement 379) September 1993

Typical Personal Author Index Listing ANDES, ROBERT C., JR. BARFIELD, WOODROW Specification of adaptive aiding systems The effect of geometric field of view and tunnel design [AD-A263071I p314 N93-27927 for perspective flight-path displays [PERSONAL AUTHOR | ANTUNANO, MELCHOR J. [SAE PAPER 921131] P 291 A93-41319 Index of international publications in aerospace BARIN, MARCO medicine Labels and visual cues to reproduce an earthlike [AD-A262908] p 284 N93-28306 environment in space - Going ahead in designing Columbus HOROWITZ, STANLEY A. APSELOFF, G. APM interior architecture — Relating Hying hours to aircrew performance: Evidence Aminohydroxybutane bisphosphonate and clenbuterol [SAE PAPER 921193] P 295 A93-41371 for attack and transport missions prevent bone changes and retard muscle atrophy BARKER, ROBERT S. [AD-A253988] p 25 N93-10719 respectively in tail-suspended rats p 271 A93-39703 Dew point analysis for Space Station Freedom ARATOW, M. [SAE PAPER 921227) P 296 A93-41401 Direct measurement of capillary blood pressure in the Comparative test data assessment and simplified math human lip p 279 A93-40550 modelling for Sabatier CO2 reduction subsystem ARDITI, ARIES [SAE PAPER 921228] P 296 A93-41402 Visualization and modeling of factors influencing visibility BARKLEY, ROBERT in computer-aided crewstation design Contaminant distribution and accumulation in water [SAE PAPER 921135] p 292 A93-41323 recycle systems ASHIDA, AKIRA [SAE PAPER 921360] P 307 A93-41519 Listings in this Index are arranged alphabetically by A trade study method for determining the design personal author. The title of the document is used to parameter of CELSS subsystems Generation of iodine disinfection by-products (IDP's) in [SAE PAPER 921198] p 295 A93-41374 a water recycle system provide a brief description ol the subject matter. The [SAE PAPER 921362] P 307 A93-41521 report number helps to indicate the type of document Experimental and theoretical study on membrane distillation using thermopervaporation BARREAU, J. M. (e.g., NASA report, translation, NASA contractor [SAE PAPER 921397] p 309 A93-41554 Design and preliminary testing of a membrane based report). The page and accession numbers are ASSMUS, BERNHARD water recycling system for European manned space located beneath and to the right of the title. Under any Ferrous iron oxidation by anoxygenic phototrophic missions one author's name the accession numbers are bacteria p 271 A93-39280 [SAE PAPER 921396] P 309 A93-41553 arranged in sequence. ATEN, LAURIE A. BART A, DANIEL J. A systems approach to water recovery testing for space Regenerative Life Support Systems Test Bed life support - Initial biomedical results from the ECLSS performance - Lettuce crop characterization Water Recovery Test and plans for testbed utilization [SAE PAPER 921391 ] P 309 A93-41549 [SAE PAPER 921210] p 295 A93-41386 BASSINGER, VIRGINIA J. Effects of refrigerating preinoculated Vitek cards on ATWATER, JAMES E. microbial physiology and antibiotic susceptibility Regenerable Microbial Check Valve - Life cycle tests [ SAE PAPER 921214 ] P273 A93-41390 results BEHREND, A. F. [SAE PAPER 9213161 p 303 A93-41476 JSC ECLSS R/T program overview ADAM, SUSAN C. Regenerable biocide delivery unit, volume 1 P312 N93-27725 Operational space human factors - Methodology for a [NASA-CR-185701] p 274 N93-27122 BENNETT, W. S., II DSO Regenerable biocide delivery unit, volume 2 System automation and pilot-vehicle-interface for [SAE PAPER 921156] p 293 A93-41339 [NASA-CR-185701-VOL-2] p 275 N93-27360 unconstrained low-altitude night attack ADAMS, ALAN AUSONI, SIMONETTA P320 N93-28867 Environmental control and life support system Myosin and troponin changes in rat soleus muscle after BENSON, BRIAN L. p311 N93-27718 hindlimb suspension p 273 A93-41124 The ECLSS advanced automation project evolution and ADAMS, GREGORY R. AYATA, HARUKI technology assessment P 312 N93-27723 Mapping of electrical muscle stimulation using MRl Conceptual study of manned lunar surface site BERGAN, TONE p 279 A93-40549 p316 N93-28031 The psychological effects of isolation on a space station ADAMS, RICHARD J. AZUETA, STEVEN - A simulation study How expert pilots think: Cognitive processes in expert Visualization and modeling of factors influencing visibility [SAE PAPER 921191 ] p 287 A93-41369 decision making in computer-aided crewstation design BERGEN, JAMES [DOT/FAA/RD-93/9) p 288 N93-27103 [SAE PAPER 921135] p 292 A93-41323 Visualization and modeling of factors influencing visibility in computer-aided crewstation design AHEARN, D. G. [SAE PAPER 921135] P 292 A93-41323 Relative resistance of biofilms and planktonic cells of B BERGMAN, T. common molds and yeasts to antimicrobials Plasmid encoded virulence of Yersinia [SAE PAPER 921212] p 273 A93-41388 BAERTSCH, PETER [FOA-B-40419-4.4] p 275 N93-28199 AJJARAPU, SUNDARA R. M. Interactions between Hb, Mg, DPG, ATP, and Cl BEST, LEONARD G. Use of sorption technology for treatment of humidity determine the change in Hb-O2 affinity at high altitude Low-cost helmet-mounted displays condensate for potable water p279 A93-41117 [AOA262616] p 317 N93-28479 [SAE PAPER 921312] p 303 A93-41474 BILARDO, VINCENT BAGDIGIAN, ROBERT M. Overview of NASA's 1991 Life Support Systems Analysis AKSE, JAMES R. Phase III Integrated Water Recovery Testing at MSFC Workshop Catalytic oxidation for treatment of ECLSS and PMMS - Closed hygiene and potable loop test results and lesson [SAE PAPER 921118] P 290 A93-41310 waste streams learned BINOT, R. A. [SAE PAPER 921274] p 301 A93-41443 [SAE PAPER 921117] p 290 A93-41309 Design and preliminary testing of a membrane based ALTENBERG, BARBARA H. BAGGS, RAYMOND water recycling system for European manned space Oxygen production on the Lunar materials processing Potential health hazards from thermal degradation missions frontier p315 N93-27967 events - Particulate vs. gas phase effects [SAE PAPER 921396] P 309 A93-41553 AMBLARD, P. [SAE PAPER 921388] p 282 A93-41546 BIRD, DONALD M. Design and preliminary testing of a membrane based BAGIAN, JAMES P. Recovering potable water from wastewater in space water recycling system for European manned space Cerebral blood velocity and other cardiovascular platforms by fyophilization missions responses to 2 days of head-down tilt [SAE PAPER 921323] P 304 A93-41485 [SAE PAPER 921396] p 309 A93-41553 p280 A93-41122 BITTEN, ROBERT E. AMO, KARL BAKER, DANIEL R. Requirements for pilot assistance in a thrust-vectoring Water reclamation technology development for future Sudden loading and fatigue effects on the human combat aircraft p 320 N93-28870 long range missions spine BLANCHARD, l_ A. [SAE PAPER 921351] p306 A93-41510 [PB93-167526] p 286 N93-29199 Biophysical model for handwear insulation testing ANAND, INDER S. BALLIN, MARK G. [AD-A262926] p 320 N93-28884 Body fluid compartments, renal blood flow, and Consumables and wastes estimations for the First Lunar BLANCHARD, ROBERT E. hormones at 6,000 m in normal subjects Outpost Accident proneness: A research review p281 A93-41125 [SAE PAPER 9212871 p 302 A93-41453 [DOT/FAA/AM-93/9] p 288 N93-28622

B-1 BLOSWICK, DONALD S. PERSONAL AUTHOR INDEX

BLOSWICK, DONALD S. BUCK, COURTNEY A. CHANG, CHI-MIN Sudden loading and fatigue effects on the human Hyperbaric treatment operations aboard Space Station ASDA - Advanced Suit Design Analyzer computer spine Freedom program [P893-167526] p 286 N93-29199 [SAE PAPER 9211421 p 292 A93-41328 [SAE PAPER 9213811 p 308 A93-41539 BOBBA, FABIANA BUE, GRANT C. CHANG, CRAIG H. Labels and visual cues to reproduce an earthlike ASDA - Advanced Suit Design Analyzer computer Portable life support system regenerative carbon dioxide environment in space - Going ahead in designing Columbus program and water vapor removal by metal oxide absorbents ARM interior architecture [ SAE PAPER 921381 ] p 308 A93-41539 preprototype hardware development and testing [SAE PAPER 921193] p 295 A93-41371 BUFFETT, A. R. [ SAE PAPER 921299 ] p 303 A93-41464 BODEK, ITAMAR Pilot decision aiding for weapon delivery: A novel CHANG, S. K. The development and testing of a volatile organics approach to fire control cueing using parallel computing Biophysical model for handwear insulation testing concentrator for use in monitoring Space Station water p317 N93-28853 [AD-A262926] p 320 N93-28884 quality CHARLES, J. BULA, R. J. [SAE PAPER 921266] p 300 A93-41436 Intraocular pressure and retinal vascular changes during A matrix-based porous tube water and nutrient delivery BOEHM, ALBERT M. transient exposure to microgravity p 278 A93-39710 systam Space Station Water Processor - Current flight design CHARLES, JOHN B. [SAE PAPER 921390] p 309 A93-41548 [ SAE PAPER 921112 ] p 289 A93-41306 Cerebral blood velocity and other cardiovascular BULGAJEWSKI, PETER J. BOELJN, I. responses to 2 days of head-down tilt Initial accomplishments of the Environmental Control Plasmid encoded virulence of Yersinia p280 A93-41122 and Life Support System (ECLSS) atmosphere [FOA-B-40419-4.4] p 275 N93-28199 CHATURVEDI, ARVIND K. revitalization (AR) predevelopment operational system test BOGART, EDWARD H. Variations of time-to-incapacitation and (POST) for the Space Station Freedom (SSF) Identification of hazardous awareness states in carboxyhemoglobin values in rats exposed to two carbon [SAE PAPER 921186] p 294 A93-41365 monitoring environments monoxide concentrations BURKE, THOMAS G. [SAE PAPER 921136] p 287 A93-41324 [DOT/FAA/AM-93/7] p 274 N93-27152 13 C NMR spectra of allosteric effectors of Method of encouraging attention by correlating video Variations in time-to-incapacitation and blood cynanide hemoglobin game difficulty with attention level values for rats exposed to two hydrogen cyanide gas [AD-A262979] p 284 N93-28293 [NASA-CASE-LAR-15022-1] p 288 N93-28128 BYGBJERG, I. concentrations BOLSTAD, CHERYL A. [DOT/FAA/AM-93-8] p 283 N93-27158 Influence of in vivo hypobaric hypoxia on function of Human capabilities and limitations in situation CHIARAMONTE, JIM A. lymphocytes, neutrocytes, natural killer cells, and awareness p319 N93-28863 The use of electrophysiological and cognitive variables cytokines p 280 A93-41123 BOONSTRA, J. in the assessment of degradation during periods of Inhibition of EGF-induced signal transduction by sustained wakefulness microgravity is independent of EGF receptor redistribution [AD-A263033] p 283 N93-27923 in the plasma membrane of human A431 cells CHOI, HONGYUNG p272 A93-39715 CADOGAN, DAVID Altered immunological response in mice subjected to BOPARAI, M. S. Enhanced softgoods structures for spacesuit stress and exposed to fungal spores Body fluid compartments, renal blood flow, and micrometeoroid/debris protective systems [SAE PAPER 921215] p 274 A93-41391 hormones at 6,000 m in normal subjects [SAE PAPER 921258] p 299 A93-41428 CHROMIAK, JOSEPH p281 A93-41125 CALDWELL, JOHN A., JR. Mechanical stimulation of skeletal muscle increases BORGHESE, JOSEPH B. The use of electrophysiological and cognitive variables prostaglandin F2(alpha) synthesis and cyclooxygenase Portable life support system regenerative carbon dioxide in the assessment of degradation during periods of activity by a pertussis toxin sensitive mechanism and water vapor removal by metal oxide absorbents sustained wakefulness [NASA-CR-193041] p 282 N93-27102 preprototype hardware development and testing [AD-A263033] p 283 N93-27923 CHUANG, SHERRY [SAE PAPER 921299] p 303 A93-41464 CALKINS, D. S. Dark cycle monitoring of biological specimens on Space BOUET, T. Human performance and physiological function during Station Freedom Design and preliminary testing of a membrane based a 24-hr exposure to 1 percent bromotrifluoromethane [SAE PAPER 921393] p 274 A93-41551 water recycling system for European manned space (Ha!on1301) p 277 A93-39704 CHURCH, T. O. missions CALLAGHAN, THOMAS F. System automation and pilot-vehicle-interface for [SAE PAPER 921396] p 309 A93-41553 Operational space human factors - Methodology for a BOUISSON, X. unconstrained low-altitude night attack DSO p 320 N93-28867 Design and preliminary testing of a membrane based [SAE PAPER 921156] p 293 A93-41339 CIOLETTI, LOUIS A. water recycling system for European manned space CAMPIONE, MARINA Microbiology operations and facilities aboard missions Myosin and troponin changes in rat soleus muscle after restructured Space Station Freedom [SAE PAPER 921396] p 309 A93-41553 hindlimb suspension p 273 A93-41124 [SAE PAPER 921213] p 296 A93-41389 BOURLAND, CHARLES T. CAPUTO, M. Space Station Freedom food management Intraocular pressure and retinal vascular changes during CLARK, BENTON C. [SAE PAPER 921248] p 298 A93-41419 transient exposure to microgravity p 278 A93-39710 Shielding strategies for human exploration missions BOYDA, ROBERT B. CARNES, JAMES R. [SAE PAPER 921376] p 308 A93-41S34 - Sabatier carbon dioxide reduction system for Space The ECLSS advanced automation project evolution and CLARKSON, THOMAS W. Station Freedom technology assessment p312 N93-27723 NASA Specialized Center for Research and Training [SAE PAPER 921189] p 294 A93-41368 CARR, SANDRA E. (NSCORT) in space environmental health BRAGHIN, MASSIMO Biofilm formation and control in a simulated spacecraft [SAE PAPER 921358] p 307 A93-41517 System integration and verification approach for the water system - Three year results COHEN, BERNARD environmental control system of the Columbus Attached [SAE PAPER 921310] p 303 A93-41472 NASA supporting studies for microgravity research on Pressurised Module CARTER, DANIEL C. eye movements [SAE PAPER 921261] p 299 A93-41431 Amino acid sequences for the binding regions in serum [NASA-CR-193233] p 285 N93-29041 BRAUNE, ROLF J. albumin proteins COLASSON, M. Toward a flight deck automation philosophy for the [NASA-CASE-MFS-28402-1] p 276 N93-28952 European involvement in CELSS - Definition of a Closed Boeing High Speed Civil Transport CARTER, DONALD L. Ecological Systems Test Bed [SAE PAPER 921133] p 291 A93-41321 Catalytic oxidation for treatment of ECLSS and PMMS [SAE PAPER 921200] p 295 A93-41376 BRESSAN, RAYMOND A. waste streams COLE, HAROLD Biomass productivity and sustainability of a [SAE PAPER 921274] p 301 A93-41443 Determination of organic carbon and ionic accountability bioregenerative life-support system Determination of organic carbon and ionic accountability of various waste and product waters derived from ECLSS [SAE PAPER 921359] p 307 A93-41518 of various.waste and product waters derived from ECLSS water recovery tests and Spacelab humidity condensate BRETOI, REMUS water recovery tests and Spacelab humidity condensate [SAE PAPER 921313] p 303 A93-41475 [SAE PAPER 921313] p 303 A93-41475 Manned systems technology discipline COLLING, ARTHUR 1C, JR. p 314 N93-27860 CAVALETTI, G. Space Station Water Processor - Current flight design BRION, GAIL M. Long-lasting neuropsychological changes after a single [SAE PAPER 921112] p 289 A93-41306 high altitude climb p 278 A93-39713 Contaminant distribution and accumulation in water CAVANAGH, P. R. COMPERATORE, CARLOS A. recycle systems The use of electrophysiological and cognitive variables Simulating reduced gravity - A review of biomechanical [SAE PAPER 921360] p 307 A93-41519 in the assessment of degradation during periods of issues pertaining to human locomotion sustained wakefulness Inactivation of a model coliphage virus in water by p289 A93-41175 iodine [AD-A263033] p 283 N93-27923 CHAMBERLAND, DENNIS [SAE PAPER 921361] p 274 A93-41520 Advanced life support systems in lunar and Martian CONGER, BRUCE C. Generation of iodine disinfection by-products (IDP's) in environments utilizing a higher plant based engineering ASDA - Advanced Suit Design Analyzer computer a water recycle system paradigm program [ SAE PAPER 921362 ] p 307 A93-41521 [SAE PAPER 921286] p 302 A93-41452 [SAE PAPER 921381] p 308 A93-41539 BRITTON, BRUCE K. CHANDANA, JAGDISH CORBIN, BARBARA J. Expertise, text coherence, and constraint satisfaction: Body fluid compartments, renal blood flow, and Defining contamination control requirements for Effects on harmony and settling rate hormones at 6,000 m in normal subjects non-human research on Space Station Freedom [AD-A262703] p 288 N93-28901 p281 A93-41125 [SAE PAPER 921386] p 308 A93-41544 BRUCE, REBEKAH J. CHANDRASHEKHAR, Y. CORDES, ED Biofilm formation and control in a simulated spacecraft Body fluid compartments, renal blood flow, and Crew Health Care Systems installations for Space water system - Three year results hormones at 6.000 m in normal subjects Station Freedom [SAE PAPER 921310] p 303 A93-41472 p281 A93-41125 [SAE PAPER 921249] p 298 A93-41420

B-2 PERSONAL AUTHOR INDEX EVANICH, PEGGY L.

COTTET-EMARD, JEAN-MARIE DEAN, W. C. DUNN, KEVIN H. Norepinephrine content in discrete brain areas and Zero gravity phase separator technologies - Past, Initial accomplishments of the Environmental Control neurohypophysial vasopressin in rats after a 9-d spaceflight present and future and Life Support System (ECLSS) atmosphere (SLS-1) p273 A93-41167 [SAE PAPER 921160) p 293 A93-41342 revitalization (AR) predevelopment operational system test CRABB, THOMAS M. DEGIOANNI, J. J. (POST) for the Space Station Freedom (SSF) Overview of NASA's 1991 Life Support Systems Analysis Human performance and physiological function during [SAE PAPER 921186] p 294 A93-41365 Workshop a 24-hr exposure to 1 percent bromotrifluoromethane (SAE PAPER 921118] p 290 A93-41310 (Halon 1301) p277 A93-39704 1991 NASA Life Support Systems Analysis workshop DEIMLER, JAMES D. (NASA-CFU466) p310 N93-27100 Age 60 Project: Consolidated database experiments 1992 NASA Life Support Systems Analysis workshop [HS-TR-8025-3C(R2)1 p314 N93-27851 EBERHARDT, RALPH [NASA-CR-4467] p310 N93-27101 DEMPSTER, WILLIAM F. NASA Specialized Center for Research and Training CRAIG, I. Biosphere 2 - Overview of system performance during (NSCORT) in space environmental health Oculomotor responses and virtual image displays the first nine months [ SAE PAPER 921358] p307 A93-41517 ECKHARDT, BRADLEY D. p 319 N93-28862 [SAE PAPER 921129] p 291 A93-41317 Regenerative Life Support Systems Test Bed CRAMPTON, GEORGE H. DENARO, ANGELO performance - Lettuce crop characterization 8-OH-DPAT does not interfere with habituation to Environmental control of the Mini Pressurized Logistic [SAE PAPER 921391] p 309 A93-41549 motion-induced emesis in cats p 271 A93-384S1 Module [SAE PAPER 921281] p 302 A93-41449 EDEEN, MARYBETH CRENSHAW, A. Plant growth modeling at the JSC variable pressure Direct measurement of capillary blood pressure in the DENCKER, WALLY growth chamber - An application of experimental design human lip p 279 A93-40550 The development of an atmosphere composition monitor [SAE PAPER 921356] p 307 A93-41515 CROW, S. A. for the Environmental Control and Life Support System EDEEN, MARYBETH A. Relative resistance of biofilms and planktonic cells of [SAE PAPER 921149] p 292 A93-41333 Analysis of the Variable Pressure Growth Chamber using common molds and yeasts to antimicrobials DEROSHIA, CHARLES W. the CASE/A simulation package [SAE PAPER 921212) p 273 A93-41388 Performance and mood-state parameters during 30-day [SAE PAPER 921122] p 291 A93-41314 CRUMP, WILLIAM J. 6 deg head-down bed rest with exercise training A hybrid regenerative water recovery system for A systems approach to water recovery testing for space p281 A93-41169 lunar/Mars life support applications life support - Initial biomedical results from the ECLSS DEWBERRY, BRANDON S. [SAE PAPER 921276] p 301 A93-41445 Water Recovery Test and plans for testbed utilization The ECLSS advanced automation project evolution and Plant canopy transpiration in bioregenerative life support [SAEPAPER921210] p295 A93-41386 technology assessment p312 N93-27723 systems - The link between mechanistic and empirical CUCHE, J. L. DIAMANT, BRYCE L models Microgravity and orthostatic intolerance - Carotid Technologies for ECLSS evolution [SAE PAPER 921355] p 306 A93-41514 hemodynamics and peripheral responses p 311 N93-27720 Regenerative Life Support Systems Test Bed p278 A93-39716 DICKENSON, REUBEN D. performance - Lettuce crop characterization CURTIS, ROBERT L A feasibility study of hand kinematics for EVA analysis [SAE PAPER 921391 ] p 309 A93-41549 Two phase fluid management for hydroponics using magnetic resonance imaging EDGAR, G. K. [SAE PAPER 921163] p 294 A93-41345 [SAE PAPER 921253] p 298 A93-41423 Oculomotor responses and virtual image displays CUSICK, ROBERT J. DICKENSON, RUEBEN D. p 319 N93-28862 Development of a regenerate metal oxide sheet matrix EVA Glove Research Team EDGERTON, V. R. CO2 removal system [NASA-CR-193014] p313 N93-27847 Absence of a growth hormone effect on rat soleus atrophy during a 4-day spaceflight p 272 A93-40548 [SAE PAPER 921298] p 302 A93-41463 A feasibility study of hand kinematics for EVA analysis EGGLESTON, ROBERT G. Portable life support system regenerative carbon dioxide using magnetic resonance imaging p313 N93-27848 Cognitive interface considerations for intelligent and water vapor removal by metal oxide absorbents DIENER, M. preprototype hardware development and testing cockpits p319 N93-28865 Development of a 500 hPa shoulder joint for the EHNTHOLT, DANIEL J. [SAE PAPER 921299] p 303 A93-41464 European EVA Space Suit System CYMERMAN, ALLEN The development and testing of a volatile organics [SAE PAPER 921257] p 299 A93-41427 concentrator for use in monitoring Space Station water Hypoxic ventilatory responsiveness in Tibetan compared DINAUER, W. R. with Han residents of 3,658 m p 280 A93-41120 quality A matrix-based porous tube water and nutrient delivery [SAE PAPER 921266] p 300 A93-41436 system EHRENREICH, ARMIN [SAE PAPER 921390] p 309 A93-41548 Ferrous iron oxidation by anoxygenic phototrophic DISARIO, ROBERT bacteria P 271 A93-39280 O'AURIA, RENATO Instrument-approach-plate design considerations for EICHSTADT, FRANK Environmental control of the Mini Pressurized Logistic displaying radio frequencies p 289 A93-39574 Crew Health Care Systems installations for Space Module DISMER, BERIT G. Station Freedom [SAE PAPER 921281 ] p 302 A93-41449 Immobilized cell bioreactors for water reclamation - [SAE PAPER 921249] p 298 A93-41420 DALEE, ROBERT C. Process stability and effect of reactor design EICHSTADT, FRANK T. Development of membrane gas removal technology for [SAE PAPER 921277] p 301 A93-41446 Glovebox design for Space Station Freedom Crew microgravity liquid flow systems DOKUNIN, IVAN V. Health Care System [SAE PAPER 921162] p 294 A93-41344 Functions simulation model of integrated regenerate [SAE PAPER 921139] p 292 A93-41326 DALL-BAUMAN, LIESE life support system EISENHART, F. J. Conceptual design of ECLSS microgravity test beds [SAE PAPER 921201] p 295 A93-41377 Expertise, text coherence, and constraint satisfaction: [SAE PAPER 921164] p 294 A93-41346 DOLL, SUSAN Effects on harmony and settling rate DALL-BAUMAN, LIESE A. TRIALSS - Tool for Rapid and Intelligent Advanced Life [AD-A262703] p 288 N93-28901 Modeling of membrane processes for air revitalization Support System Selection and Sizing ENDECOTT, BOYD R. and water recovery [SAE PAPER 921123] p 291 A93-41315 Variations of time-to-incapacitation and carboxyhemoglobin values in rats exposed to two carbon [SAE PAPER 921352] p 306 A93-41511 DOUGHERTY, DALE R. monoxide concentrations DALTON, BONNIE P. Continuous monitoring of effluent iodine levels of Space [DOT/FAA/AM-93/7] p 274 N93-27152 The General Purpose Work Station, a spacious Station water using solid state technology Variations in time-to-incapacitation and blood cynanide microgravity workbench [SAE PAPER 921265] p 299 A93-41435 [ SAE PAPER 921394 ] p 309 A93-41552 values for rats exposed to two hydrogen cyanide gas DREW, MALCOLM C. DAVIDSON, LAARNI concentrations Growing wheat to maturity in reduced gas pressures The development of an atmosphere composition monitor [DOT/FAA/AM-93-8] p 283 N93-27158 [NASA-CR-193245] p 277 N93-29216 for the Environmental Control and Life Support System ENDSLEY, MICA R. [SAE PAPER 921149] p 292 A93-41333 DROMA, TARSHI Human capabilities and limitations in situation DA VIES, D. R. Hypoxic ventilatory responsiveness in Tibetan compared awareness p 319 N93-28863 Cognitive predictors of vigilance p 287 A93-40771 with Han residents of 3,658 m p 280 A93-41120 ENGLAND, HARVEY, JR. DAVIS, BRIAN L Minimal hypoxic pulmonary hypertension in normal Comparison of portable crewmember protective Simulating reduced gravity - A review of biomechanical Tibetans at 3,658 m p 280 A93-41121 breathing equipment (CPBE) designs issues pertaining to human locomotion DRYSDALE, ALAN [DOT/FAA/AM-93/6] p 310 N93-27121 p289 A93-41175 OCAM - A CELSS modeling tool: Description and ERICKSEN, BRYCE J. DAVIS, J. R. results Low-cost helmet-mounted displays Human performance and physiological function during [SAE PAPER 921241 ] p 298 A93-41413 [AD-A262616] p317 N93-28479 ERICKSON, K. a 24-hr exposure to 1 percent bromotriflu'oromethane DUCHIER, J. L Plasmid encoded virulence of Yersinia (Halon 1301) P277 A93-39704 Microgravity and orthostatic intolerance - Carotid [FOA-B-40419-4.4] p 275 N93-28199 DE GROOT, R. P. hemodynamics and peripheral responses ETTER, BRAD D. Inhibition of EGF-induced signal transduction by p278 A93-39716 microgravity is independent of EGF receptor redistribution Growing wheat to maturity in reduced gas pressures DUDLEY, GARY A. in the plasma membrane of human A431 cells [NASA-CR-193245] p 277 N93-29216 p272 A93-39715 Mapping of electrical muscle stimulation using MRI EVANICH, PEGGY L DE LAAT, S. W. p 279 A93-40549 Overview of NASA's 1991 Life Support Systems Analysis Inhibition of EGF-induced signal transduction by DUNHAM, ANDREW Workshop microgravity is independent of EGF receptor redistribution Generation of iodine disinfection by-products (IDP's) in [SAE PAPER 921118] p 290 A93-41310 in the plasma membrane of human A431 cells a water recycle system 1991 NASA Life Support Systems Analysis workshop p272 A93-39715 [SAE PAPER 921362] p 307 A93-41521 [NASA-CR-4466] p310 N93-27100

B-3 EVERT, MARTHA F. PERSONAL AUTHOR INDEX

1992 NASA Ufe Support Systems Analysis workshop FORSBERG, A. GAUOUELIN, GUILLEMETTE [NASA-CR-4467] p 310 N93-27101 Plasmid encoded virulence of Yersinia Norepinephrine content in discrete brain areas and EVERT, MARTHA F. [FOA-B-40419-4.4] p 275 N93-28199 neurohypophysial vasopressin in rats after a 9-d spaceflight Consumables and wastes estimations for the First Lunar FORSBERG, AAKE (SLS-1) p273 A93-41167 Outpost Intraceflufar targeting of the Yersinia YopE cytotoxin in GAUTHIER, GABRIEL M. [SAE PAPER 921287] p 302 A93-41453 mammalian cells induces actin microfilament disruption Dynamic analysis of human visuo-oculo-manual [FOA-B-40420-4.4] p 275 N93-27989 coordination control in target tracking tasks FORSMAN, M. p287 A93-41166 Characterization and classification of strains of GAVACH, C. Design and preliminary testing of a membrane based FADEN, A- I. Fcandsella tularensis isolated in the central Asian focus water recycling system for European manned space Secondary injury factors and preventative treatment of the Soviet Union and in Japan [FOA-B-40421-4.4] p 275 N93-28200 missions [PB93-176014] P283 N93-27409 [SAE PAPER 921396] p 309 A93-41553 FAREH, JEANNETTE Use of RNA hybridization in the diagnosis of a case of GAYDA, CHRISTIAN ulceroglandular tularemia Norepinephrine content in discrete brain areas and DOKMA: A document oriented communication model neurohypophysial vasopressin in rats after a 9-d spaceflight [FOA-B-40422-4.4] p 275 N93-28212 FORTNEY, SUZANNE M. for medical applications as a basis of a role system in (SLS-1) P273 A93-41167 the medical field FASZCZA, JEFFREY J. Orthostatic intolerance during a 13-day bed rest does [ETN-93-93799] p 284 N93-28469 not result from increased leg compliance Membrane technology for zero gravity life support GENCO, LOUIS V. systems p280 A93-41119 FRAMPTON, ROBERT F. Effect of microgravity on several visual functions during [SAE PAPER 921320] p 304 A93-41482 STS Shuttle missions: Visual Function Tester-Model 1 FERIN, JURAJ Space Shuttle Orbiter oxygen partial pressure sensing (VFT-1) p284 N93-28740 and control system improvements Potential health effects of fume particles on the crew Effect of microgravity on visual contrast threshold during of spacecrafts [SAE PAPER 921347] p 305 A93-41506 STS Shuttle missions: Visual Function Tester-Model 2 [SAE PAPER 921387] p 308 A93-41545 FRESA, MARK OCAM - A CELSS modeling tool: Description and (VFT-2) p 284 N93-28741 Potential health hazards from thermal degradation GERBER, N. results events - Paniculate vs. gas phase effects Aminohydroxybutane bisphosphonate and clenbuterol [SAE PAPER 921388] p 282 A93-41546 [SAE PAPER 921241] p 298 A93-41413 FREY, MARY A. B. prevent bone changes and retard muscle atrophy FERRALL, JOE respectively in tail-suspended rats p 271 A93-39703 Cerebral blood velocity and other cardiovascular Human life support during interplanetary travel and responses to 2 days of head-down tilt GHARIB, CLAUDE domicile. V - Mars expedition technology trade study lor Norepinephrine content in discrete brain areas and p280 A93-41122 solid waste management neurohypophysial vasopressin in rats after a 9-d spaceflight FRIEDMAN, M. A. [SAE PAPER 921119] p 290 A93-41311 Gray water recycling with a unique vapor compression (SLS-1) p273 A93-41167 FERRALL, JOSEPH distillation (VCD) design GIBSON, C. R. Intraocular pressure and retinal vascular changes during Human life support during interplanetary travel and [SAE PAPER 921318] p 304 A93-41480 transient exposure to microgravity p 278 A93-39710 domicile. VI - Generic modular flow schematic for hybrid FRIESEN, DWAYNE T. GILLEN, CHRISTOPHER M. physical/chemical-biological life support systems Operation of a breadboard [SAE PAPER 921120] p 290 A93-41312 liquid-sorbent/membrane-contactor system for removing Effects of dynamic exercise on cardiovascular regulation during lower body negative pressure FERRARA, MARINO carbon dioxide and water vapor from air Effects of air bubble contamination in recirculating water [SAE PAPER 921321] p 304 A93-41483 p281 A93-41168 loop A novel membrane device for the removal of water vapor GILLEY, S. D. [SAE PAPER 921282] p 302 A93-41450 and water droplets from air Evaluation of the carbon dioxide removal assembly FERRARI, ROBERTO [SAE PAPER 921322] p 304 A93-41484 requirements for the Space Station Freedom in the Manned Tended Capability through Permanently Manned Capability Body fluid compartments, renal blood flow, and FRYE, ROBERT J. hormones at 6,000 m in normal subjects Closed ecological systems: From test tubes to Earth's configurations [SAE PAPER 921231] p 297 A93-41405 P281 A93-41125 biosphere p315 N93-27976 FILBUM, THOMAS P. FUCHS, W. GIRTEN, B. Aminohydroxybutane bisphosphonate and clenbuterol Development of a regenerable metal oxide sheet matrix Symbology for head up and head down applications for prevent bone changes and retard muscle atrophy CO2 removal system highly agile fighter aircraft: To improve spatial awareness, respectively in tail-suspended rats p 271 A93-39703 [SAE PAPER 921298] p 302 A93-41463 trajectory control, and unusual attitude recovery, part 1 GLEASON, GERALD A. p318 N93-28857 FINKELSTEIN, JACOB Armstrong Laboratory space visual function tester FUHS, SUSAN Potential health hazards from thermal degradation program p 284 N93-28739 Dust protection for environmental control and life support events - Paniculate vs. gas phase effects Effect of microgravity on the visual near point: Visual systems in the lunar environment p 315 N93-27979 [ SAE PAPER 921388 ] p 282 A93-41546 Function Tester-Model 4 (VFT-4) p 284 N93-28742 FUNK, GLENN A. FISCHER, G. GLUMM, MONICA M. Symbology for head up and head down applications for Defining contamination control requirements for non-human research on Space Station Freedom A study of the effects of lens focal length on remote highly agile fighter aircraft: To improve spatial awareness, driver performance [SAE PAPER 921386] p 308 A93-41544 trajectory control, and unusual attitude recovery, part 1 [AD-A263191] p 321 N93-28941 P318 N93-28857 GONZALEZ, R. R. FISHER, H. THOMAS Biophysical model for handwear insulation testing Simplified Aid For Crew Rescue (SAFR) [AD-A262926] p 320 N93-28884 P313 N93-27793 GADSBY, PETE GOODMAN, B. J. FISHER, JOHN Crew Health Care Systems installations for Space Introductions to the Proceedings of the Fourteenth Water reclamation technology development for future Station Freedom Symposium on Biotechnology for Fuels and Chemicals long range missions [SAE PAPER 921249] p 298 A93-41420 [DE93-006235] p 276 N93-28890 [SAE PAPER 921351 ] p 306 A93-41510 GALBO, H. GOODMAN, JERRY R. FLANAGAN, DAVID T. Influence of in vivo hypobaric hypoxia on function of Space Shuttle crew compartment Biofilm formation and control in a' simulated spacecraft lymphocytes, neutrocytes, natural killer cells, and debris-contamination water system - Three year results cytokines p 280 A93-41123 [SAE PAPER 921345] p 305 A93-41504 [SAE PAPER 921310] p 303 A93-41472 GALEN, T. J. GOPHER, DANIEL Regenerable Microbial Check Valve - Life cycle tests Toxicokinetics of inhaled bromotrifluoromethane (Halon Performance under dichoptic versus binocular viewing results 1301) in human subjects p 278 A93-39705 conditions - Effects of attention and task requirements [SAE PAPER 921316] p 303 A93-41478 GANAPATHI, GANI B. p 287 A93-40772 GOSBEE, JOHN W. FLYNN, MICHAEL T. Human life support during interplanetary travel and Operational space human factors - Methodology for a Water reclamation technology development for future domicile. VI - Generic modular flow schematic for hybrid DSO long range missions physical/chemical-biological life support systems [SAE PAPER 921156] p 293 A93-41339 [SAE PAPER 921351 ] p 306 A93-41510 [SAE PAPER 921120] p 290 A93-41312 GANDHI, P. A. GOULART, CARLA V. FOERG, SANDRA Relative resistance of biofilms and planktonic cells of The Centrifuge Facility Life Sciences Glovebox Operation of a breadboard common molds and yeasts to antimicrobials configuration study liquid-sorbent/membrane-contactor system for removing [SAE PAPER 921212] p 273 A93-41388 [SAE PAPER 921158) p 293 A93-41341 carbon dioxide and water vapor from air GARCIA, HECTOR D. GRABOWSKI, NORMAN A. [SAE PAPER 921321J p 304 A93-41483 Setting Spacecraft Maximum Allowable Concentrations Space Station Condensing Heat Exchanger biofilm FOERG, SANDRA L for 1 hour or 24 hour contingency exposures to airborne formation and control evaluation Modeling of membrane processes for air revitalization chemicals [SAE PAPER 921383] p 308 A93-41541 and water recovery [SAE PAPER 921410] p 310 A93-41564 GREEN, N. D. C. [ SAE PAPER 921352 ] p 306 A93-41511 GARGIOLI, EUGENIO The physiological limitations of man in the high G FOMICHEV, ALEKSANDR A. The effects of a reduced pressure scenario on the environment p 319 N93-28861 Functions simulation model of integrated regenerable Columbus APM environmental control system GREENISEN, M. C. life support system [SAE PAPER 921247] p 298 A93-41418 Program development for exercise countermeasures [SAE PAPER 921201] p 295 A93-41377 GARTRELL, CHARLES F. [SAE PAPER 921140] p 292 A93-41327 FORD, TIM 1991 NASA Life Support Systems Analysis workshop GREENLEAF, J. E. Biodeterioration of materials in water reclamation [NASA-CR-4466] p310 N93-27100 Performance and mood-state parameters during 30-day systems 1992 NASA Life Support Systems Analysis workshop 6 deg head-down bed rest with exercise training [SAE PAPER 921311] p 303 A93-41473 [NASA-CR-4467] p 310 N93-27101 p281 A93-41169

B-4 PERSONAL AUTHOR INDEX JAMES, JOHN

GRIFFITH, GUY HASEGAWA, PAUL M. HORII, A. Determination of organic carbon and ionic accountability Biomass productivity and sustainability of a Neuropharmacology of motion sickness and emesis - of various waste and product waters derived from ECLSS bioregenerative life-support system A review p 271 A93-39711 water recovery tests and Spacelab humidity condensate [SAE PAPER 921359] p 307 A93-41518 Motion sickness induced by sinusoidal linear [SAE PAPER 921313] p 303 A93-41475 HASEGAWA, S. acceleration in rats p 272 A93-39712 GRIGGER, DAVID J. Neuropharmacology of motion sickness and emesis - HOROWITZ, PAUL Sabatier carbon dioxide reduction system for Space A review p 271 A93-39711 Wide-bandwidth high-resolution search for Station Freedom HAUSER, GERHARD extraterrestrial intelligence [SAE PAPER 921189] p 294 A93-41368 Hermes ECLSS - Main requirements and technical [NASA-CR-193137] p 322 N93-28895 GROVE, C. M. solutions HOSHI, SEIKO Evaluation of test methods and requirements for [SAE PAPER 921400] p 309 A93-41555 Lunar surface experiment system p316 N93-28034 HAYES, J. C. respiratory protection systems 21 HOWARD, EMILY Program development for exercise countermeasures [AD-A262466] p 317 N93-28757 Virtual interface applications for airborne weapons [SAE PAPER 921140] p 292 A93-41327 GROVES, BERTRON M. systems p318 N93-28858 HEISING, SILKE Minimal hypoxic pulmonary hypertension in normal Requirements for pilot assistance in a thrust-vectoring Tibetans at 3,658 m p 280 A93-41121 Ferrous iron oxidation by anoxygenic phototrophic bacteria p 271 A93-39280 combat aircraft p 320 N93-28870 GRUNWALD, ARTHUR J. HOWARD, GLENN W., JR. Visual field information in nap-of-the-Earth flight by HELDMANN, MICHAEL J. Space Station Water Processor - Current flight design The application of filtration technology within the Water teleoperated helmet-mounted displays Processor on board Space Station Freedom p311 N93-27177 [SAE PAPER 921112] p289 A93-41306 HENDERSON, A. S. [SAE PAPER 921270] p 300 A93-41440 GUEZENNEC, CHARLES Y. HOY, DENNIS M. Myosin and troponin changes in rat soleus muscle after Gene transcription and electromagnetic fields [DE93-010854] p 276 N93-28848 Space Shuttle Orbiter oxygen partial pressure sensing hindlimb suspension p 273 A93-41124 and control system improvements GUIZARD, C. HENNINGER, DONALD H. An assessment of waste processing/resource recovery [SAE PAPER 921347] p 305 A93-41506 Design and preliminary testing of a membrane based HUANG, SHAO YUNG water recycling system for European manned space technologies for lunar/Mars life applications [SAE PAPER 921271 ] p 300 A93-41441 Hypoxic ventilatory responsiveness in Tibetan compared missions with Han residents of 3,658 m p 280 A93-41120 (SAE PAPER 921396] p 309 A93-41553 HERMIDA, J. S. Microgravity and orthostatic intolerance - Carotid HUFF, T. L GUSTAVINO, S. Aquatic biofilms and their responses to disinfection and Tests characterizing bioprocessor hardware for hemodynamics and peripheral responses p278 A93-39716 invading species analytical modeling [SAE PAPER 921211] p 296 A93-41387 [SAE PAPER 921357] p 307 A93-41516 HERRMANN, CAL C. High-recovery low-pressure reverse osmosis HULS, M. H. [SAE PAPER 921353] p 306 A93-41512 Biofilm formation and control in a simulated spacecraft H KEYING, MONTY water system - Three year results Development of membrane gas removal technology for [SAE PAPER 921310] p 303 A93-41472 HAAKANSSON, S. microgravity liquid flow systems HUNTER, N. Intraocular pressure and retinal vascular changes during Plasmid encoded virulence of Yersinia [SAE PAPER 921162] p 294 A93-41344 transient exposure to microgravity p 278 A93-39710 [FOA-B-40419-4.4] p 275 N93-28199 HEZEL, PAUL J. HABERCOM, MARK Head mounted displays for virtual reality HUNTLEY, M. S., JR. Instrument-approach-plate design considerations for Determination of organic carbon and ionic accountability [AD-A263498] p 322 N93-29340 displaying radio frequencies p 289 A93-39574 of various waste and product waters derived from ECLSS HIGHTOWER, T. M. water recovery tests and Spacelab humidity condensate Recycling and source reduction for long duration space HURST, CHARLES Contaminant distribution and accumulation in water [SAE PAPER 921313] p 303 A93-41475 habitation recycle systems HAFELE, BERNARD [SAE PAPER 921121] p 290 A93-41313 [SAE PAPER 921360] p 307 A93-41519 Development of the carbon dioxide removal system Water reclamation technology development for future Generation of iodine disinfection by-products (IDP's) in blower used on Space Station Freedom long range missions a water recycle system [SAE PAPER 921188] p 294 A93-41367 [SAE PAPER 921351] p 306 A93-41510 [SAE PAPER 921362] p 307 A93-41521 HALE, JOSEPH P. HILLMAN, DONALD J. HUTTENBACH, ROBIN C. Man-systems integration and the man-machine Age 60 Project: Consolidated database experiments Life Support and Habitability Manual ESA PSS-03-406 interface p313 N93-27795 [HS-TR-8025-3C(R2)] p 314 N93-27851 [SAE PAPER 921338] p 305 A93-41497 HALL, J. R. HINMAN, ELAINE M. HYLAND, DIANE T. The design and development of the new RAF standard Development of a test protocol for evaluating EVA glove Age 60 Project: Consolidated database experiments HUD format p318 N93-28856 performance (HS-TR-8025-3C(R2)] p 314 N93-27851 HAMAMI, HIDEAKI [SAE PAPER 921254] p 298 A93-41424 HYMER, WESLEY C. A trade study method for determining the design HINSDALE, LLOYD Electrophoretic separation of cells and particles from parameter of CELSS subsystems The development and testing of a volatile organics rat pituitary and rat spleen [SAE PAPER 921198] p 295 A93-41374 concentrator for use in monitoring Space Station water [NASA-CR-193073] p 276 N93-28415 HAMANO, NOBUO quality Experimental and theoretical study on membrane [SAE PAPER 921266] p 300 A93-41436 distillation using thermopervaporation HITCHENS, G. D. [SAE PAPER 921397] . p 309 A93-41554 Water purification, microbiological control, sterilization HANEY, L. N. and organic waste decomposition using an electrochemical IIYAMA, S. Crucial role of detailed function, task, timeline, link, and advanced ozonation process Development of the nitrogen fixation system for human vulnerability analyses in HRA [SAE PAPER 921234] p 297 A93-41408 CELSS [DE93-001923] p 321 N93-28942 Post-treatment of reclaimed waste water based on an [ SAE PAPER 921238 ] p 297 A93-41411 HANSMAN, R. J., JR. electrochemical advanced oxidation process INOUE, M. An exploratory study of plan-view terrain displays for [SAE PAPER 921275] p 301 A93-41444 Development of the nitrogen fixation system for air carrier operations p 289 A93-39573 HODGES, THOMAS K. CELSS HARGENS, A. R. Biomass productivity and sustainability of a [SAE PAPER 921238] p 297 A93-41411 Direct measurement of capillary blood pressure in the bioregenerative life-support system IOVINE, JOHN V. human lip p 279 A93-40550 [SAE PAPER 921359] p 307 A93-41518 ASDA - Advanced Suit Design Analyzer computer HARMA, M. HOEHN, A. program The prediction of the adaptation of circadian rhythms Design and evaluation of a payload to support plant [SAE PAPER 921381] p 308 A93-41539 to rapid time zone changes p 278 A93-39714 growth onboard COMET 1 IVANCHIKOV, A. P. HARPER, ELVIN [SAE PAPER 921389] p 308 A93-41547 New technology for the analysis of the results of an Wound healing and connective tissue metabolism: The HOFACRE, K. C. ultrasound experiment performed in aviation-medicine role of hyperbaric oxygen therapy Evaluation and optimization of a flexible filtration system medical examination p 279 A93-40774 [AD-A262483] p 285 N93-28759 for respiratory protection system 21 HARRIS, B. A. [AD-A262467] p 284 N93-28758 Program development for exercise countermeasures HOLDER, DONALD W., JR. [SAE PAPER 921140] p 292 A93-41327 Phase III Integrated Water Recovery Testing at MSFC HARRIS, JEFFREY JABLONSKI, DAVID - Closed hygiene and potable loop test results and lesson Dust protection for environmental control and life support Geography of end-Cretaceous marine bivalve learned systems in the lunar environment p315 N93-27979 extinctions p 273 A93-41075 [SAE PAPER 921117] p 290 A93-41309 HARRIS, REGINA M. JACOBS, I. Age 60 Project: Consolidated database experiments HOLLAND, PETER J. Influence of the Cold Buster (tm) sports bar on heat [HS-TR-8025-3C(R2>] p 314 N93-27851 Recovering potable water from wastewater in space debt, mobilization and oxidation of energy substrates HARRIS, ROBERT T. platforms by lyophilization [AD-A262762] p 285 N93-28939 Mapping of electrical muscle stimulation using MRI (SAE PAPER 921323] p 304 A93-41485 JAHNS, GARY p 279 A93-40549 HOLLEY, PETER J. Norepinephrine content in discrete brain areas and HART, JOAN M. Cognitive predictors of vigilance p 287 A93-40771 neurohypophysial vasopressin in rats after a 9-d spaceflight Portable life support system regenerative carbon dioxide HORIE, MICHIHIKO (SLS-1) p273 A93-41167 and water vapor removal by metal oxide absorbents Manned lunar surface site: Conceptual study on JAMES, JOHN preprototype hardware development and testing pressurized lunar surface operation rover First entry operations for spacecraft [SAE PAPER 921299] p 303 A93-41464 p316 N93-28032 [SAE PAPER 921384] p 308 A93-41542

B-5 JAMES, JOHN T. PERSONAL AUTHOR INDEX

The role of Environmental Health System air quality KLOKKER, M. KURMAZENKO, EHDUARD A. monitors in Space Station Contingency Operations Influence of in vivo hypobaric hypoxia on function of Functions simulation model of integrated regenerable [SAE PAPER 921414] p 310 A93-41565 lymphocytes, neutrocytes, natural killer cells, and life support system JAMES, JOHN T. cytokines p 280 A93-41123 [SAE PAPER 9212011 p 295 A93-41377 Setting Spacecraft Maximum Allowable Concentrations KLUTE, GLEN K. KUROKAWA, HIDEAKI for 1 hour or 24 hour contingency exposures to airborne Anthropometric data from launch and entry suited test Experimental and theoretical study on membrane chemicals subjects for the design of a recumbent seating system distillation using thermopervaporation (SAE PAPER 921410] p 310 A93-41564 [NASA-TM-104769] p 321 N93-29044 [SAE PAPER 921397] p 309 A93-41554 JANES, CRAIG KLUTE, GLENN K. KURUP, VISWANATH P. Hypoxic ventilatory responsiveness in Tibetan compared A comparison of two Shuttle launch and entry suits - Altered immunological response in mice subjected to with Han residents of 3,658 m p 280 A93-41120 Reach envelope, isokinetic strength, and treadmill tests stress and exposed to fungal spores Minimal hypoxic pulmonary hypertension in normal [SAE PAPER 921154] p 293 A93-41337 [ SAE PAPER 9212151 p 274 A93-41391 Tibetans at 3,658 m p 280 A93-41121 Pilot investigation - Nominal crew induced forces in JARRETT, O. N. zero-g The quest for an integrated frying helmet (SAE PAPER 921155] p 293 A93-41338 p319 N93-28860 A study to explore locomotion patterns in partial gravity LABOURDETTE, X. JEFFERS, E. L environments Development of a 500 hPa shoulder joint for the Process Control Water Quality Monitor for Space Station ISAE PAPER 921157) p 293 A93-41340 Freedom - Development update European EVA Space Suit System Anthropometric survey of the astronaut applicants and [SAE PAPER 921264] p 299 A93-41434 [SAE PAPER 921257] p 299 A93-41427 astronauts from 1985 to 1991 LACOLLEY, P. J. Continuous monitoring of effluent iodine levels of Space [NASA-RP-1304] p321 N93-29324 Station water using solid state technology Microgravity and orthostatic intolerance - Carotid KNOX, J. C. [ SAE PAPER 921265 ] p 299 A93-41435 hemodynamics and peripheral responses Evaluation of the carbon dioxide removal assembly p278 A93-39716 JENKINS, JAMES P. requirements for the Space Station Freedom in the Manned LADISCH, MICHAEL R. EVA/manned systems p312 N93-27789 Tended Capability through Permanently Manned Capability Biomass productivity and sustainability of a JENSEN, DEAN G. configurations bioregenerative life-support system Evolving technologies for Space Station Freedom [SAE PAPER 921231] p 297 A93-41405 [SAE PAPER 921359] p 307 A93-41518 computer-based workstations p 313 N93-27794 KNOX, JOHN LAITINEN, J. T. JIANG, BIAN Pressure, composition, and temperature control of cabin The prediction of the adaptation of arcadian rhythms Absence of a growth hormone effect on rat soleus atmosphere on Space Station Freedom to rapid time zone changes p 278 A93-39714 atrophy during a 4-day spaceflight p 272 A93-40548 [SAE PAPER 921216] p 296 A93-41392 LAM, C. W. JOLLY, CLIFFORD KNUTH, SUSAN L Toxicokinetics of inhaled bromotrifluoromethane (Halon Catalytic oxidation for treatment of ECLSS and PMMS Response of genioglossus EMG activity to passive tilt 1301) in human subjects p 278 A93-39705 waste streams in men p 279 A93-41118 LANDOLT, J. P. [SAE PAPER 921274] p 301 A93-41443 KOBAYASHI, T. Effects of long-term weightlessness on roll High-altitude pulmonary edema with pulmonary circularvection p 279 A93-39725 thromboembolism p 278 A93-39709 LANGE, KEVIN E. K KOHN, S. Modeling of membrane processes for air revitalization Visual field information in nap-of-the-Earth flight by and water recovery KAMATA, TERUMITSU teleoperated helmet-mounted displays [SAE PAPER 921352] p 306 A93-41511 Manned lunar surface site p316 N93-28033 p311 N93-27177 LARBOT, A. KANTOWITZ, BARRY H. KOIZUMI, T. Design and preliminary testing of a membrane based Flight deck automation and pilot workload High-altitude pulmonary edema with pulmonary water recycling system for European manned space [SAE PAPER 921132] p 291 A93-41320 thromboembolism p 278 A93-39709 KARA VIS, A. missions KOLODNEY, MATT [SAE PAPER 921396] p 309 A93-41553 The quest for an integrated frying helmet Conceptual design of ECLSS microgravity test beds LARIMER, JAMES p319 N93-28860 [SAE PAPER 921164] p 294 A93-41346 Visualization and modeling of factors influencing visibility KATOU, NOBUTAKA KOROL'KOV, V. I. Conceptual study of manned lunar surface site in computer-aided crewstation design Oxygen regime in the frontal cerebral cortex of monkeys [SAE PAPER 921135] p 292 A93-41323 p316 N93-28031 during a two-week space flight p 272 A93-40773 LAROCHELLE, F. T. KAY, EDWIN J. KORTSCHOT, H. W. Age 60 Project: Consolidated database experiments Program development for exercise countermeasures Barotrauma in Boeing 737 cabin crew [SAE PAPER 92It40] p 292 A93-41327 [HS-TR-8025-3C(R2>] p314 N93-27851 p278 A93-39706 KELLER, BIRGIT LAURENT, S. KOSMO, JOSEPH Microgravity and orthostatic intolerance - Carotid Photobiological investigations on spores of Enhanced softgoods structures for spacesuit streptomyces griseus hemodynamics and peripheral responses micrometeoroid/debris protective systems p 278 A93-39716 [ESA-TT-1269] p 277 N93-29274 [SAE PAPER 921258] P 299 A93-41428 LEE, M. G. KELLEY, WILLIAM A. KOZLOVSKIJ, A. P. Sabatier carbon dioxide reduction system for Space Flow cytometric analysis of lymphocyte surface markers New technology for the analysis of the results of an Station Freedom following a 1-Gy dose of gamma radiation ultrasound experiment performed in aviation-medicine [SAE PAPER 921189] p 294 A93-41368 p281 A93-41170 medical examination p 279 A93-40774 KELLY, KEVIN J. KRECIC, M. E. LEE, W. D. Space Shuttle Orbiter oxygen partial pressure sensing Aminohydroxytautane bisphosphonate and clenbuterol Hybrid oxygen system and control system improvements prevent bone changes and retard muscle atrophy [AD-A262417] p 317 N93-28464 [SAE PAPER 921347] p 305 A93-41506 respectively in tail-suspended rats p 271 A93-39703 LEHNERT, BRUCE E. KEYSER, PAUL I. KROTOV, V. P. Potential health hazards from thermal degradation The application of filtration technology within the Water Oxygen regime in the frontal cerebral cortex of monkeys events - Paniculate vs. gas phase effects Processor on board Space Station Freedom during a two-week space flight p 272 A93-40773 [SAE PAPER 921388) . p 282 A93-41546 [SAE PAPER 921270] p 300 A93-41440 KUBO, K. Evaluation of NO(x)-induced toxicity KHARAZMI, A. High-altitude pulmonary edema with pulmonary [AD-A261034] p 283 N93-28122 Influence of in vivo hypobaric hypoxia on function of thromboembolism p 278 A93-39709 LEINENWEVER, ROGER W. lymphocytes, neutrocytes, natural killer cells, and KUBO, T. Low-cost helmet-mounted displays cytoKines p 280 A93-41123 Neuropharmacology of motion sickness and emesis - [AD-A262616] p317 N93-28479 A review p 271 A93-39711 KIKUCHI, K. LEIRER, V. Motion sickness induced by sinusoidal linear Development of the nitrogen fixation system for Influence of aging and practice on piloting tasks acceleration in rats p 272 A93-39712 CELSS p 286 A93-39708 KUCHAR, JAMES K. [SAE PAPER 921238] p 297 A93-41411 LEITER, JAMES C. An exploratory study of plan-view terrain displays for KILDUFF, PATRICIA W. Response of genioglossus EMG activity to passive tilt air carrier operations p 289 A93-39573 in men p 279 A93-41118 A study of the effects of lens focal length on remote KULL, ROBERT LEONIDA, ANDREI driver performance Anaerobic treatment of organic wastes from Controlled [AD-A263191] p 321 N93-28941 A low pressure electrolyzer for the next generation Ecological Life Support Systems submarine KIMCHI, RUTH (SAE PAPER 921272] p 301 A93-41442 [SAE PAPER 921125] p 291 A93-41316 Performance under dichoptic versus binocular viewing KUMAR, ANOOPA conditions - Effects of attention and task requirements Altered immunological response in mice subjected to LEVY, B. I. p287 A93-40772 stress and exposed to fungal spores Microgravity and orthostatic intolerance - Carotid KLISS, M. H. [SAE PAPER 921215] P 274 A93-41391 hemodynamics and peripheral responses Design and evaluation of a payfoad to support plant KUNYAEV, V. YU. p 278 A93-39716 growth onboard COMET 1 Oxygen regime in the frontal cerebral cortex of monkeys LEWIS, J. L. [SAE PAPER 921389] p 308 A93-41547 during a two-week space flight p 272 A93-40773 Man-systems distributed system for Space Station KUSS, MARK KUOPPA, K. Freedom p 312 N93-27788 A novel membrane device for the removal of water vapor Use of RNA hybridization in the diagnosis of a case of LIMERO, THOMAS and water droplets from air ulceroglandular tularemia First entry operations for spacecraft (SAE PAPER 921322] p 304 A93-41484 [FOA-B-40422-4.4] p 275 N93-28212 (SAE PAPER 921384] p 308 A93-41542

B-6 PERSONAL AUTHOR INDEX MITANI, KENJI

LIMERO, THOMAS F. MALHOTRA, RAVI M. MCGAUGH, JAMES L Setting Spacecraft Maximum Allowable Concentrations Body fluid compartments, renal blood flow, and Analysis of neural systems involved in modulation of for 1 hour or 24 hour contingency exposures to airborne hormones at 6,000 m in normal subjects memory storage chemicals p281 A93-41125 [AD-A262418] p 283 N93-27654 |SAE PAPER 921410) p310 A93-41564 WANDERS, JULIAN H. MCGHEE, JERRY R. The role of Environmental Health System air quality Flow cytometric analysis of lymphocyte surface markers Lunar base thermal management/power system monitors in Space Station Contingency Operations following a 1-Gy dose of gamma radiation analysis and design p 315 N93-27985 [SAE PAPER 921414] p310 A93-41565 p281 A93-41170 MCKEE, JAMES W. LIN, CHIN MARKHAM, R. L The ECLSS advanced automation project evolution and Overview ol NASA's 1991 Life Support Systems Analysis Evaluation and optimization of a flexible filtration system technology assessment p312 N93-27723 for respiratory protection system 21 Workshop MCLAUCHLAN, PHILIP F. | SAE PAPER 921118) p 290 A93-41310 [AD-A262467] p 284 N93-28758 A modular head/eye platform for real-time reactive LOBASCIO, CESARE MARSH, ROBERT W. vision The effects of a reduced pressure scenario on the The application of filtration technology within the Water [OUEL-1941/92] p320 N93-28897 Processor on board Space Station Freedom Columbus APM environmental control system MCLEAN, GARNET [SAE PAPER 921270] p 300 A93-41440 ISAEPAPER921247J p298 A93-41418 Comparison of portable crewmember protective Space Station Condensing Heat Exchanger biofilm Environmental control of the Mini Pressurized Logistic breathing equipment (CPBE) designs formation and control evaluation Module [DOT/FAA/AM-93/6] p 310 N93-27121 [SAE PAPER 921383] p 308 A93-41541 | SAE PAPER 921281] p 302 A93-41449 MEEHAN, R. T. LORENZ, CHRISTINE H. MARTEL, ADRIAN Intraocular pressure and retinal vascular changes during A feasibility study of hand kinematics for EVA analysis Ergonomic development of digital map displays transient exposure to microgravity p 278 A93-39710 p 320 N93-28866 using magnetic resonance imaging MEEHAN, RICHARD T. MARTIN, CHARLES E. [SAE PAPER 921253) p 298 A93-41423 Cerebral blood velocity and other cardiovascular EVA Glove Research Team Air Handling and Atmosphere Conditioning systems for responses to 2 days of head-down tilt (NASA-CR-193014J p 313 N93-27847 manned spacecraft - A design and performance data p280 A93-41122 survey A feasibility study of hand kinematics for EVA analysis [SAE PAPER 921350] p 306 A93-41509 MELCHIOR, FRANCOIS M. using magnetic resonance imaging p 313 N93-27848 Orthostatic intolerance during a 13-day bed rest does MASLEY, AMY S. LUBIN, JEFFREY not result from increased leg compliance A study of the effects of lens focal length on remote Visualization and modeling of factors influencing visibility p280 A93-41119 driver performance in computer-aided crewstation design [AD-A263191 ] p 321 N93-28941 MENENDEZ, V. [SAE PAPER 921135] p 292 A93-41323 Development of a 500 hPa shoulder joint for the MATSUNAGA, T. LUCK, STEPHEN European EVA Space Suit System Neuropharmacology of motion sickness and emesis - [SAE PAPER 921257] p 299 A93-41427 Hermes ECLSS - Main requirements and technical A review p 271 A93-39711 solutions MERHAV, S. J. [SAE PAPER 921400] p 309 A93-41555 Motion sickness induced by sinusoidal linear Visual field information in nap-of-the-Earth flight by acceleration in rats p 272 A93-39712 LUCOT, JAMES B. teleoperated helmet-mounted displays 8-OH-DPAT does not interfere with habituation to MATTHEWS, GERALD p311 N93-27177 motion-induced emesis in cats p 271 A93-38451 Cognitive predictors of vigilance p 287 A93-40771 MEYLOR, JOHN LUKEFAHR, BRENDA D. MAY, L L. Norepinephrine content in discrete brain areas and neurohypophysial vasopressin in rats after a 9-d spaceflight The ECLSS advanced automation project evolution and Relative resistance of biofilms and planktonic cells of (SLS-1) p273 A93-41167 technology assessment p 312 N93-27723 common molds and yeasts to antimicrobials (SAE PAPER 921212] p 273 A93-41388 MIAN, ARSHAD LUTTGES, M. W. Dark cycle monitoring of biological specimens on Space Design and evaluation of a payload to support plant MCCORMACK, A. Station Freedom growth onboard COMET 1 Tests characterizing bioprocessor hardware for [SAE PAPER 921393] p 274 A93-41551 [SAE PAPER 921389] p 308 A93-41547 analytical modeling [SAE PAPER 921357] p 307 A93-41516 MIDORIKAWA, YOSHINORI LYDICK, L. N. MCCORMACK, ANN C. A trade study method for determining the design Head-steered sensor flight test results and Plant canopy transpiration in bioregenerative life support parameter of CELSS subsystems implications p 318 N93-28859 systems - The link between mechanistic and empirical [SAE PAPER 921198] p 295 A93-41374 models MIGNON, GEORGE M [SAE PAPER 921355] p 306 A93-41514 Closed ecological systems: From test tubes to Earth's MCCORMICK, ARTHUR K., Ill biosphere p315 N93-27976 Air Handling and Atmosphere Conditioning systems for MILLARD, DOUGLAS L. MACK, GARY W. manned spacecraft - A design and performance data Operation of a breadboard Effects of dynamic exercise on cardiovascular regulation liquid-sorbent/membrane-contactor system, for removing survey during lower body negative pressure carbon dioxide and water vapor from air [SAE PAPER 921350] p 306 A93-41509 p281 A93-41168 [SAE PAPER 921321] p 304 A93-41483 MADER, T. H. MCCRAY, SCOTT B. MILLER, ADAM M. Intraocular pressure and retinal vascular changes during Operation of a breadboard Computer modeling of the Variable Pressure Growth liquid-sorbent/membrane-contactor system for removing transient exposure to microgravity p 278 A93-39710 Chamber using the CASE/A simulation package carbon dioxide and water vapor from air [SAE PAPER 921354] p 306 A93-41513 MADER, THOMAS H. [SAE PAPER 921321] p 304 A93-41483 Cerebral blood velocity and other cardiovascular Plant growth modeling at the JSC variable pressure responses to 2 days of head-down tilt A novel membrane device for the removal of water vapor growth chamber - An application of experimental design and water droplets from air p280 A93-41122 [SAE PAPER 921356] p 307 A93-41515 [SAE PAPER 921322] p 304 A93-41484 MAIN, JOHN A. MILLER, CAROLYN L. MCCULLOUGH, ROBERT E. A feasibility study of hand kinematics for EVA analysis Recovering potable water from wastewater in space Hypoxic ventilatory responsiveness in Tibetan compared using magnetic resonance imaging platforms by lyophilization with Han residents of 3,658 m p 280 A93-41120 [SAE PAPER 921253] p 298 A93-41423 [SAE PAPER 921323] p 304 A93-41485 Minimal hypoxic pulmonary hypertension in normal MILLER, MARK R. Power assist EVA glove development Tibetans at 3,658 m p 280 A93-41121 Structured interviews for pilot selection - No incremental [SAE PAPER 921255] p 299 A93-41425 MCCULLOUGH, ROSANN G. validity p 286 A93-39572 EVA Glove Research Team Hypoxic ventilatory responsiveness in Tibetan compared MINTON, SILVIA [NASA-CR-193014] p313 N93-27847 with Han residents of 3,658 m p 280 A93-41120 The analytical control program for the NASA Space A feasibility study of hand kinematics for EVA analysis Minimal hypoxic pulmonary hypertension in normal Station Freedom Environmental Control and Life Support using magnetic resonance imaging p 313 N93-27848 Tibetans at 3,658 m p 280 A93-41121 System (ECLSS) Water Recovery Test A preliminary structural analysis of space-based MCELROY, J. F. [SAE PAPER 921269] p 300 A93-41439 inflatable tubular frame structures p 313 N93-27849 SPE water electrolyzers in support of the lunar MISHANKIN, B. N. Characterization and classification of strains of Power assist EVA glove development outpost p315 N93-27977 p 314 N93-27850 Francisella tularensis isolated in the central Asian focus MCELROY, JAMES F. MAIRBAEURL, HEIMO of the Soviet Union and in Japan A low pressure electrofyzer for the next generation Interactions between Hb, Mg, DPG, ATP, and Cl [FOA-B-40421-4.4] p 275 N93-28200 submarine determine the change in Hb-O2 affinity at high altitude MISHRA, S. K. [SAE PAPER 921125] p 291 A93-41316 p279 A93-41117 Microbiology operations and facilities aboard MAISONBLANCHE, P. MCFAODEN, CARL D. restructured Space Station Freedom Microgravity and orthostatic intolerance - Carotid Analysis of the Variable Pressure Growth Chamber using [SAE PAPER 921213] p 296 A93-41389 hemodynamics and peripheral responses the CASE/A simulation package Effects of refrigerating preinoculated Vitek cards on p278 A93-39716 [SAE PAPER 921122] p 291 A93-41314 microbial physiology and antibiotic susceptibility MAKI, JAMES S. Computer modeling of the Variable Pressure Growth [SAE PAPER 921214] p 273 A93-41390 Biodeterioration of materials in water reclamation Chamber using the CASE/A simulation package Altered immune-logical response in mice subjected to systems [SAE PAPER 921354] p 306 A93-41513 stress and exposed to fungal spores [SAE PAPER 921311] p 303 A93-41473 MCFETERS, GORDON A. [SAE PAPER 921215] p 274 A93-41391 MALACINSKI, G. M. Microbiological concerns and methodological MITANI, KENJI Altering the position of the first horizontal cleavage approaches related to bacterial water quality in Experimental and theoretical study on membrane furrow of the amphibian (Xenopus) egg reduces embryonic spaceflight distillation using thermopervaporation survival p 272 A93-39717 [SAE PAPER 921232] p 297 A93-41406 [SAE PAPER 921397] p 309 A93-41554

B-7 MITCHELL, GARY A. PERSONAL AUTHOR INDEX

MITCHELL, GARY A. NAKAGAWA, S. O Biomass productivity and sustainability of a High-altitude pulmonary edema with pulmonary • bioregenerative life-support system thromboembolism p 278 A93-39709 O'LEARY, JARROD D. Instrumentation for microbial monitoring of (SAE PAPER 921359 ] p 307 A93-41518 NAKAMURA, YOUICHIROU MITCHELL, RALPH Manned lunar surface site: Conceptual study on decontamination or biocide system effectiveness Biodeterioration of materials in water reclamation pressurized lunar surface operation rover [SAE PAPER 921233] p 297 A93-41407 systems p316 N93-28032 OBENHUBER, D. C. [SAE PAPER 921311 ] p 303 A93-41473 Aquatic biofilms and their responses to disinfection and MITTELMAN, MICHAEL H. NALETTE, TIMOTHY A. invading species Development of a regenerable metal oxide sheet matrix Contact lenses in aviation - The Marine Corps [SAE PAPER 921211] p 296 A93-41387 experience p 289 A93-41172 CO2 removal system OBERDORSTER, GUNTER MOLLOY, ROBERT [SAE PAPER 921298] p 302 A93-41463 Potential health effects of fume particles on the crew Performance consequences of automation-induced NAVARRO, CHRISTINE of spacecrafts 'complacency' p 286 A93-39571 Absence of a growth hormone effect on rat soleus [SAE PAPER 921387] p 308 A93-41545 MOLNAR, O. E. atrophy during a 4-day spaceflight p 272 A93-40548 Potential health hazards from thermal degradation Evaluation of test methods and requirements for NEALY, JOHN E. events - Paniculate vs. gas phase effects respiratory protection systems 21 Radiation exposure predictions for short-duration stay [SAE PAPER 921388] p 282 A93-41546 [AO-A262466J p 317 N93-28757 Mars missions OELZ, OSWALD MOORE, KEVIN C. [AAS PAPER 92-107] p 277 A93-39261 Interactions between Hb, Mg, DPG, ATP. and Cl Pressure, composition, and temperature control of cabin determine the change in Hb-O2 affinity at high altitude NEARY, C. atmosphere on Space Station Freedom p279 A93-41117 Oculo-motor responses and virtual image displays OKA, YURIKO [SAE PAPER 921216] p 296 A93-41392 p319 N93-28862 MOORE, LORNA G. Lunar surface experiment system p316 N93-28034 Hypoxic ventilatory responsiveness in Tibetan compared NEFF, A. W. OKUDA1RA, TOSHIAKI with Han residents of 3,658 m p 280 A93-41120 Altering the position of the first horizontal cleavage Conceptual study of manned lunar surface site Minimal hypoxic pulmonary hypertension in normal furrow of the amphibian (Xenopus) egg reduces embryonic p316 N93-28031 Tibetans at 3,658 m p280 A93-41121 survival p 272 A93-39717 OLIVADOTI, J. T. MOORE, NATHAN R. NELSON, PHILIP E. Regenerable Microbial Check Valve - Life cycle tests A study to explore locomotion patterns in partial gravity Biomass productivity and sustainability of a results environments bioregenerative life-support system [SAE PAPER 921316] p 303 A93-41478 [SAE PAPER 921157] p 293 A93-41340 [SAE PAPER 921359] p 307 A93-41518 OLLIVIER, Y. MORGENTHALER, GEORGE W, NEWBOLD, DAVID D. Development of a 500 hPa shoulder joint for the NASA Specialized Center for Research and Training Operation of a breadboard European EVA Space Suit System (NSCORT) in space environmental health liquid-sorbent/membrane-contactor system for removing [SAE PAPER 921257] p 299 A93-41427 [SAE PAPER 921358] p 307 A93-41517 carbon dioxide and water vapor from air ONEAL, MELVIN R. MORITA, M. [SAE PAPER 921321 ] p 304 A93-41483 Armstrong Laboratory space visual function tester program p 284 N93-28739 Neuropharmacology of motion sickness and emesis - A novel membrane device for the removal of water vapor A review p 271 A93-39711 Effect of microgravity on several visual functions during and water droplets from air STS Shuttle missions: Visual Function Tester-Model 1 Motion sickness induced by sinusoidal linear [SAE PAPER 921322] p 304 A93-41484 acceleration in rats p 272 A93-39712 (VFT-1) P284 N93-28740 NICE, DAVID A. MORK, MICHAEL R. Effect of microgravity on visual contrast threshold during Development of the Hermes EVA Space Suit Glove STS Shuttle missions: Visual Function Tester-Model 2 Prevalence of corrective lens wear in Royal Australian [SAE PAPER 921256] p 299 A93-41426 (VFT-2) p 284 N93-28741 Air Force flight crews p 289 A93-41173 Effect of microgravity on the visual near point: Visual MORROW, D. NIELSEN, S. S. Biomass productivity and sustainability of a Function Tester-Model 4 (VFT-4) p 284 N93-28742 .Influence of aging and practice on piloting tasks bioregenerative life-support system ONKEN, R. p286 A93-39708 [SAE PAPER 921359] p 307 A93-41518 Pilot intent and error recognition as part of a knowledge MORROW, R. C. based cockpit assistant p 318 N93-28855 NISHIYASU, TAKESHI A matrix-based porous tube water and nutrient delivery OOSTERVELD, W. J. Effects of dynamic exercise on cardiovascular regulation system Barotrauma in Boeing 737 cabin crew during lower body negative pressure [SAE PAPER 921390] p 309 A93-41548 p 278 A93-39706 p281 A93-41168 MUDGETT, PAUL D, ORLANDO, ROBERTO Evaluation of capillary electrophoresis for in-flight ionic NITTA, K. Effects of air bubble contamination in recirculating water Development of the nitrogen fixation system for contaminant monitoring of SSF potable water loop [SAE PAPER 921268] p 300 A93-41438 CELSS [SAE PAPER 921282] p 302 A93-41450 [SAE PAPER 921238] p 297 A93-41411 Biofilm formation and control in a simulated spacecraft OSER, RANDALL water system - Three year results NITTA, KEIJI Increasing hits and reducing misses in CRM/LOS [SAE PAPER 921310] p 303 A93-41472 A trade study method for determining the design scenarios - Guidelines for simulator scenario MULTER, JORDAN parameter of CELSS subsystems development p 286 A93-39575 [SAE PAPER 921198] p 295 A93-41374 Instrument-approach-plate design considerations for OSTROM, l_ T. displaying radio frequencies p 289 A93-39574 Concept of waste transferring mechanisms Crucial role of detailed function, task, timeline, link, and MURALI, PAZHAYANNUR S. [SAE PAPER 921239] p 297 A93-41412 human vulnerability analyses in HRA Altered immunological response in mice subjected to NIU, WILLIAM [DE93-001923] p 321 N93-28942 stress and exposed to fungal spores The development of an atmosphere composition monitor OSTROWSKI, STANISLAW [SAE PAPER 921315) p 274 A93-41391 for the Environmental Control and Life Support System 13 C NMR spectra of allosteric effectors of MURPHY, OLIVER G. [SAE PAPER 921149] p 292 A93-41333 hemoglobin Water purification, microbiological control, sterilization NOBLE, LAWRENCE D., JR. [AD-A262979] p 284 N93-28293 and organic waste decomposition using an electrochemical An update on the readiness of vapor compression OUELLETTE, FRED A. advanced ozonation process distillation for spacecraft wastewater processing Design of a Shuttle air and water prefilter for reduced [SAE PAPER 92)234] p 297 A93-41408 [SAE PAPER 921114] p 290 A93-41307 gravity operation MURPHY, OLIVER J. NOEVER, DAVID A. [SAE PAPER 921161 ] p 294 A93-41343 Post-treatment of reclaimed waste water based on an Process for selectively recovering algae and protozoa electrochemical advanced oxidation process [NASA-CASE-MFS-26124-1-NPO] p 276 N93-29174 [SAE PAPER 921275] p 301 A93-41444 NORLANDER, L. MURRAY, DAVID W. Plasmid encoded virulence of Yersinia A modular head/eye platform for real-time reactive [FOA-B-40419-4.4] p 275 N93-28199 PACKHAM, NIGEL J. C. vision NORTHRUP, V. M. An assessment of waste processing/resource recovery [OUEL-1941/92] p 320 N93-28897 Evaluation and optimization of a flexible filtration system technologies for lunar/Mars life applications [SAE PAPER 921271] p 300 A93-41441 MUSSO, GIORGIO for respiratory protection system 21 Labels and visual cues to reproduce an earthlike [AD-A262467] p 284 N93-28758 A hybrid regenerative water recovery system for environment in space - Going ahead in designing Columbus NOVOTNY, J. lunar/Mars life support applications APM interior architecture Process Control Water Quality Monitor for Space Station [SAE PAPER 921276] p 301 A93-41445 [SAE PAPER 921193] p 295 A93-41371 Freedom - Development update PANNIER, B. M. [SAE PAPER 921264] p 299 A93-41434 Microgravity and orthostatic intolerance - Carotid NOVOTNY, JOHN hemodynamics and peripheral responses N Continuous monitoring of effluent iodine levels of Space P278 A93-39716 Station water using solid state technology PARASURAMAN, RAJA NACHEFF-BENEDICT, MAURENA S. [SAE PAPER 921265] p 299 A93-41435 Performance consequences of automation-induced Immobilized cell bioreactors for water reclamation - NOYES, GARY P. 'complacency' p 286 A93-39571 Process stability and effect of reactor design Assessment of the state of the art in life support PARAZYNSKI, S. E. [SAE PAPER 921277] p 301 A93-41446 environmental control for SEI p 315 N93-27978 Direct measurement of capillary blood pressure in the NADEL, ETHAN R. NUMAGUCHI, T. human lip p 279 A93-40550 Effects of dynamic exercise on cardiovascular regulation Development of the nitrogen fixation system for PARRISH, CLYDE F. during lower body negative pressure CELSS Lightweight passive microclimate cooling device p281 A93-41168 [SAE PAPER 921238] p 297 A93-41411 [AD-A262262] p317 N93-28112

B-8 PERSONAL AUTHOR INDEX ROSENBERG,CRAIG

PASTOR, M. POTEAT, JERE REED, K. M. European involvement in CELSS - Definition of a Closed Development of membrane gas removal technology for Evaluation of test methods and requirements for Ecological Systems Test Bed microgravity liquid flow systems respiratory protection systems 21 (SAE PAPER 921200] p 295 A93-41376 [SAE PAPER 9211621 p 294 A93-41344 [AD-A262466] p 317 N93-28757 PAVLOVICH, N. V. PREISS, H. REEVES, JOHN T. Characterization and classification of strains of Recent regenerative ECLSS technology developments Hypoxic ventilator/ responsiveness in Tibetan compared Francisella tularensis isolated in the central Asian focus in Europe with Han residents of 3,658 m p 280 A93-41120 of the Soviet Union and in Japan [SAEPAPER921332] p304 A93-41493 REGAL, DAVID M. [FOA-B-40421-4.4) p 275 N93-28200 PREVOST, MICHAEL Toward a flight deck automation philosophy for the PEARSON, JACQUELYN Y. Visualization and modeling of factors influencing visibility Boeing High Speed Civil Transport The use of electrophysiological and cognitive variables in computer-aided crewstation design [SAE PAPER 921133] p 291 A93-413Z1 in the assessment of degradation during periods of (SAE PAPER 921135) p 292 A93-41323 REID, IAN D. sustained wakefulness PRICE, D. L. A modular head/eye platform for real-time reactive [AD-A263033] p 283 N93-27923 Relative resistance of biofilms and planktonic cells of vision PEOERSEN, B. K. common molds and yeasts to antimicrobials [OUEL-1941/92] p320 N93-28897 [SAE PAPER 921212] p 273 A93-41388 Influence of in vivo hypobaric hypoxia on function of REMINGTON, BRIAN PRIEBE, WALDEMAR lymphocytes, neutrocytes. natural killer cells, and Enhanced softgoods structures for spacesuit 13 C NMR spectra of allosteric effectors of cytokines p 280 A93-41123 micrometeoroid/debris protective systems hemoglobin [SAE PAPER 921258] p 299 A93-41428 PEOUIGNOT, JEAN-MARC [AD-A262979J p 284 N93-28293 Norepinephrine content in discrete brain areas and PRINCE, CAROLYN RENDON, LISA R. neurohypophysial vasopressin in rats after a 9-d spacellight Increasing hits and reducing misses in CRM/LOS Metabolic responses to simulated extravehicular (SLS-1) p273 A93-41167 scenarios - Guidelines for simulator scenario activity PERLOT, SUSAN development p 286 A93-3957S [SAE PAPER 921303] p 282 A93-41468 The role of Environmental Health System air quality PRUTCHI, DAVID RETHKE, DONALD W. monitors in Space Station Contingency Operations New technologies for in-flight pasteless bioelectrodes Test of the Shuttle Extended Duration Orbiter (EDO) [SAE PAPER 921414] p 310 A93-41565 p289 A93-41174 Waste Collection Subsystem (WCS) PERRY, J. l_ PYLE, BARRY H. [SAE PAPER 921346] p 305 A93-41505 Computerized atmospheric trace contaminant control Microbiological concerns and methodological RICHARD, ELIZABETH E. simulation for manned spacecraft approaches related to bacterial water quality in Space Station Freedom Environmental Health Care [NASA-TM-108409] p 321 N93-28977 spaceflight Program PERRY, M. R. [SAE PAPER 921232) p 297 A93-41406 [SAE PAPER 921138] p 292 A93-41325 Evaluation of test methods and requirements for RIJKEN, P. J. respiratory protection systems 21 Inhibition of EGF-induced signal transduction by [AD-A262466] p317 N93-28757 microgravity is independent of EGF receptor redistribution PETERSON, STEVEN W. in the plasma membrane of human A431 cells RABIN, ROBERT A feasibility study of hand kinematics for EVA analysis p272 A93-39715 NASA Specialized Center for Research and Training using magnetic resonance imaging RIMPILAEINEN, M. (NSCORT) in space environmental health (SAE PAPER 921253] P 298 A93-41423 Plasmid encoded virulence of Yersinia [SAE PAPER 921358] p 307 A93-41517 [FOA-B-40419-4.4] p 275 N93-28199 Power assist EVA glove development RADOMSKI, M. W. [SAE PAPER 921255] P 299 A93-41425 Effects of sleep deprivation and exercise on glucose RITTER, ROXANE M. EVA Glove Research Team tolerance p 281 A93-41165 Variations of time-to-incapacitation and [NASA-CR-193014] P 313 N93-27847 RAM, DAVID carboxyhemoglobin values in rats exposed to two carbon A feasibility study of hand kinematics for EVA analysis Performance under dichoptic versus binocular viewing monoxide concentrations using magnetic resonance imaging p313 N93-27848 conditions - Effects of attention and task requirements [DOT/FAA/AM-93/7] p 274 N93-27152 A preliminary structural analysis of space-based p 287 A93-40772 Variations in time-to-incapacitation and blood cynanide inflatable tubular frame structures p313 N93-27849 RAJULU, SUDHAKAR L values for rats exposed to two hydrogen cyanide gas Power assist EVA glove development A comparison of two Shuttle launch and entry suits - concentrations p314 N93-27850 Reach envelope, isokinetic strength, and treadmill tests [DOT/FAA/AM-93-8] p 283 N93-27158 PETRIE, GLENN E. [SAE PAPER 921154] p 293 A93-41337 ROBERSON, WILLIAM C. Immobilized cell bioreactors for water reclamation - A study to explore locomotion patterns in partial gravity A study of decision making and performance in rejected Process stability and effect of reactor design environments takeoffs [SAE PAPER 921277] P 301 A93-41446 [SAE PAPER 921157] p 293 A93-41340 [SAE PAPER 921134] p 287 A93-41322 Anthropometric survey of the astronaut applicants and PIERSON, D. L ROBINSON, M. C. astronauts from 1985 to 1991 Human performance and physiological function during Design and evaluation of a payload to support plant [NASA-RP-1304] p321 N93-29324 a 24-hr exposure to 1 percent bromotrifluoromethane growth onboard COMET 1 RAMESH, B. (Halon 1301) P277 A93-39704 [SAE PAPER 921389) p 308 A93-41547 Body fluid compartments, renal blood flow, and Toxicokinetics of inhaled bromotrifluoromethane (Halon ROCHOWIAK, DANIEL M. hormones at 6,000 m in normal subjects 1301) in human subjects p 278 A93-39705 The ECLSS advanced automation project evolution and p281 A93-41125 PIERSON, DUANE L. technology assessment p312 N93-27723 RAMIREZ, T. L. Microbiology operations and facilities aboard RODGERS, E. B. Evaluation of test methods and requirements for restructured Space Station Freedom Aquatic biofilms and their responses to disinfection and respiratory protection systems 21 [SAE PAPER 921213] P 296 A93-41389 invading species [AD-A262466] p317 N93-28757 Effects of refrigerating preinoculated Vitek cards on [SAE PAPER 921211 ] p 296 A93-41387 RAO, SUDHAKAR K. microbial physiology and antibiotic susceptibility RODGERS, MARK D. Body fluid compartments, renal blood flow, and [SAE PAPER 921214] P 273 A93-41390 Accident proneness: A research review hormones at 6,000 m in normal subjects Altered immunological response in mice subjected to [DOT/FAA/AM-93/9] p 288 N93-28622 p281 A93-41125 stress and exposed to fungal spores ROGERS, JOHN S. RAPMUND, GARRISON [SAE PAPER 921215) P 274 A93-41391 The ECLSS advanced automation project evolution and Minimal hypoxtc pulmonary hypertension in normal Bcofilm formation and control in a simulated spacecraft technology assessment p312 N93-27723 Tibetans at 3,658 m p 280 A93-41121 water system - Three year results ROGERS, TOM D. RAUP, DAVID M. [SAE PAPER 921310] p303 A93-41472 Water purification, microbiological control, sterilization Geography of end-Cretaceous marine bivalve PIJPERS, E. W. and organic waste decomposition using an electrochemical extinctions p 273 A93-41075 Overview of cockpit technology research and advanced ozonation process RAY, CHARLES development programs for improvement of the [SAE PAPER 921234] p 297 A93-41408 Environmental control and life support system man/machine interface: Review of the AGARD AVP Post-treatment of reclaimed waste water based on an p311 N93-27718 Symposium held in Madrid, May 1992 electrochemical advanced oxidation process RAY, CHARLES D. p 320 N93-28872 [SAE PAPER 921275] p 301 A93-41444 Environmental control and life support systems PLAGHKI, LEON Alternative processes for water reclamation and solid p314 N93-27858 Development of the Hermes EVA Space Suit Glove waste processing in a physical/chemical bioregeneratrve RAY, ROD [SAE PAPER 921256] P 299 A93-41426 life support system p311 N93-27721 Operation of a breadboard ROHATGI, NARESH POORMAN, TOM liquid-sorbent/membrane-contactor system for removing Continuous monitoring of effluent iodine levels of Space Human life support during interplanetary travel and carbon dioxide and water vapor from air Station water using solid state technology domicile. VI - Generic modular flow schematic for hybrid [SAE PAPER 921321) p 304 A93-41483 [SAE PAPER 921265] P 299 A93-41435 physical/chemical-biological life support systems A novel membrane device for the removal of water vapor POPE, ALAN T. [SAE PAPER 921120] p 290 A93-41312 Identification of hazardous awareness states in and water droplets from air ROHATGI, NARESH K. [SAE PAPER 921322] p 304 A93-41484 monitoring environments Human life support during interplanetary travel and [SAE PAPER 921136] P 287 A93-41324 REBA, R. C. domicile. V - Mars expedition technology trade study for Method of encouraging attention by correlating video Proceedings of a Workshop on Molecular Nuclear solid waste management game difficulty with attention level Medicine (SAE PAPER 921119] p 290 A93-41311 [NASA-CASE-LAR-15022-1] P 288 N93-28128 [DE93-010828] p 285 N93-28835 ROSENBERG, CRAIG POPE, J. C. D. REE, MALCOLM J. The effect of geometric field of view and tunnel design Oculo-motor responses and virtual image displays Structured interviews for pilot selection - No incremental for perspective flight-path displays p319 N93-28862 validity p 286 A93-39572 [SAE PAPER 921131] p 291 A93-41319

B-9 ROSQVIST, R. PERSONAL AUTHOR INDEX

ROSQVIST, R. SATO, MIKIO SCHWEICKART, RANDOLPH W. Plasmid encoded virulence of Yersinia A trade study method for determining the design Measurement of free and dissolved gas content of water [FOA-B-40419-4.4] p 275 N93-28199 parameter of CELSS subsystems samples on Space Station Freedom ROSQVIST, ROLAND [SAE PAPER 921198] p 295 A93-41374 [SAE PAPER 921267] p 300 A93-41437 Intracellular targeting of the Yersinia YopE cytotoxin in SAUER, RICHARD L SCOTT, BRYAN mammalian cells induces actin microfilament disruption A systems approach to water recovery testing for space Catalytic oxidation for treatment of ECLSS and PMMS [FOA-B-40420-4.4] p 275 N93-27989 life support - Initial biomedical results from the ECLSS waste streams ROTHERAM, MARY Water Recovery Test and plans for testbed utilization [SAE PAPER 9212741 p 301 A93-41443 The development of an atmosphere composition monitor [ SAE PAPER 921210 ] p 295 A93-41386 SEKIGUCHI, M. for the Environmental Control and Life Support System The development and testing of a volatile organics High-altitude pulmonary edema with pulmonary [ SAE PAPER 921149 ] p 292 A93-41333 concentrator for use in monitoring Space Station water thromboembolism p 278 A93-39709 ROUEN, MICHAEL N. quality SELCON, S. J. Extravehicular activity system p312 N93-27787 [SAE PAPER 921266] p 300 A93-41436 Operator and automation capability analysis: Picking the right team p319 N93-28864 ROUSE, WILLIAM B. Evaluation of capillary electrophoresis for in-flight ionic SELVAKUMAR, S. Specification of adaptive aiding systems contaminant monitoring of SSF potable water [SAE PAPER 921268] p 300 A93-41438 Mathematical model for the exchange of gases in the [AD-A263071] P314 N93-27927 Biofilm formation and control in a simulated spacecraft lungs with special reference to carbon monoxide ROWLEY, DENNIS A. p 271 A93-39707 Flow cytometric analysis of lymphocyte surface markers water system - Three year results [SAEPAPER921310] p303 A93-41472 SESHAN, P. K. following a 1-Gy dose of gamma radiation Overview of NASA's 1991 Life Support Systems Analysis p281 A93-41170 Regenerable Microbial Check Valve - Life cycle tests results Workshop ROY, ROLAND R. [SAE PAPER 921316] p 303 A93-41478 [SAE PAPER 921118] p 290 A93-41310 Absence of a growth hormone effect on rat soleus SAVAGE, C. Human life support during interplanetary travel and atrophy during a 4-day spaceflight p 272 A93-40548 Recent regenerative ECLSS technology developments domicile. V - Mars expedition technology trade study for RUBIN, YIFAT in Europe solid waste management Performance under dichoptic versus binocular viewing [SAE PAPER 921332] p 304 A93-41493 [SAE PAPER 921119] p 290 A93-41311 conditions - Effects of attention and task requirements SAVAGE, P. D. Human life support during interplanetary travel and p 287 A93-40772 The General Purpose Work Station, a spacious domicile. VI - Generic modular flow schematic for hybrid RUDISILL, MARIANNE microgravity workbench physical/chemical-biological life support systems Evolving technologies for Space Station Freedom [SAE PAPER 921394] p 309 A93-41552 [SAE PAPER 921120] p 290 A93-41312 computer-based workstations p313 N93-27794 SAWA, TOSHIO SEXAUER, ROGER N. RUSSO, DANE M. Experimental and theoretical study on membrane A low pressure electrolyzer for the next generation Space Station Freedom Environmental Health Care distillation using thermopervaporation submarine Program [SAE PAPER 921397] p 309 A93-41554 [SAE PAPER 921125] p 291 A93-41316 [SAE PAPER 921138] p 292 A93-41325 SCARINGE, ROBERT P. SHANSKY, JANET RUTZ, JEFFREY A. Lightweight passive microclimate cooling device Mechanical stimulation of skeletal muscle increases Biofilm formation and control in a simulated spacecraft [AD-A262262] p 317 N93-28112 prostaglandin F2(alpha) synthesis and cydooxygenase water system - Three year results SCHAEFER, REINHARD activity by a pertussis toxin sensitive mechanism [SAE PAPER 921310] p 303 A93-41472 Hermes ECLSS - Main requirements and technical [ NASA-CR-193041] p282 N93-27102 RYAN, T. G. solutions SHARAN, M. Mathematical model for the exchange of gases in the Crucial role of detailed function, task, timeline, link, and [SAE PAPER 921400] p 309 A93-41555 lungs with special reference to carbon monoxide human vulnerability analyses in HRA SCHAFER, LAUREN E. p 271 A93-39707 [OE93-001923] p 321 N93-28942 A comparison of two Shuttle launch and entry suits - SHARER, PETER J. RYKIEL, EDWARD J., JR. Reach envelope, isokinetic strength, and treadmill tests [SAE PAPER 921154] p 293 A93-41337 Metabolic responses to simulated extravehicular Growing wheat to maturity in reduced gas pressures activity [NASA-CR-193245] p 277 N93-29216 SCHIAFFINO, STEFANO Myosin and troponin changes in rat soleus muscle after [SAE PAPER 921303] p 282 A93-41468 hindlimb suspension p 273 A93-41124 SHARKEY, PAUL M. SCHINK, BERNHARD A modular head/eye platform for real-time reactive Ferrous iron oxidation by anoxygenic phototrophic vision bacteria p 271 A93-39280 [OUEL-1941/92] p 320 N93-28897 SAFAR, M. E. SCHMEGNER, I. F. SHAW, R. G. Microgravity and orthostatic intolerance - Carotid Influence of the Cold Buster (tm) sports bar on heat Space Station Water Processor - Current flight design hemodynamics and peripheral responses debt, mobilization and oxidation of energy substrates [ SAE PAPER 921112] p 289 A93-41306 p 278 A93-39716 [AD-A262762] p 285 N93-28939 SHEBELA, A. SAQI-DOLEV, ALYSIA M. SCHMIDT, GREG K. Oxygen regime in the frontal cerebral cortex of monkeys New technologies for in-flight pasteless bioelectrodes The General Purpose Work Station, a spacious during a two-week space flight p 272 A93-40773 p289 A93-41174 microgravity workbench SHEPARD, D. R. SALAS, EDUARDO [SAE PAPER 921394] p 309 A93-41552 Aminohydroxybutane bisphosphonate and clenbuterol Increasing hits and reducing misses in CRM/LOS SCHNELL, SYLVIA prevent bone changes and retard muscle atrophy scenarios - Guidelines for simulator scenario Ferrous iron oxidation by anoxygenic phototrophic respectively in tail-suspended rats p 271 A93-39703 development p 286 A93-39575 bacteria p 271 A93-39280 SHERMAN, LOUIS A. SALINAS, CARLOS E. SCHOPF, J. W. Biomass productivity and sustainability of a Water purification, microbiological control, sterilization Microfossils of the Earty Archean Apex chert - New bioregenerative life-support system and organic waste decomposition using an electrochemical evidence of the antiquity of life p 272 A93-40308 [SAE PAPER 921359] p 307 A93-41518 advanced ozonation process SCHUBERT, FRANZ H. SHETTY, K. J. [SAE PAPER 921234] p 297 A93-41408 An update on the readiness of vapor compression Body fluid compartments, renal blood flow, and Post-treatment of reclaimed waste water based on an distillation for spacecraft wastewater processing hormones at 6,000 m in normal subjects electrochemical advanced oxidation process [SAE PAPER 921114] p 290 A93-41307 p281 A93-41125 [SAE PAPER 921275] p 301 A93-41444 SCHULTZ, JOHN R. SHI, XIANGRONG Effects of dynamic exercise on cardiovascular regulation SANDERS, DONALD C. Evaluation of capillary electrophoresis for in-flight ionic during lower body negative pressure Variations of time-to-incapacitation and contaminant monitoring of SSF potable water p281 A93-41168 carboxyhemoglobin values in rats exposed to two carbon [SAE PAPER 921268] p 300 A93-41438 monoxide concentrations Biofilm formation and control in a simulated spacecraft SHIELDS, BOBBY L. [DOT/FAA/AM-93/7] p 274 N93-27152 water system - Three year results EVA Glove Research Team [SAE PAPER 921310] p 303 A93-41472 [NASA-CR-193014] p 313 N93-27847 Variations in time-to-incapacitation and blood cynanide SCHULZ, JON R. SHIRAISHI, ATSUSHI values for rats exposed to iwo hydrogen cyanide gas Contaminant distribution and accumulation in water Concept of waste transferring mechanisms concentrations recycle systems [SAE PAPER 921239] p 297 A93-41412 [DOT/FAA/AM-93-8] p 283 N93-27158 [SAE PAPER 921360] p 307 A93-41519 SHONTZ, WILLIAM D. SANDUN, DORAL E. SCHWARTZKOPF, S. A study of decision making and performance in rejected Recovering potable water from wastewater in space Crop interactions in potyculture and their implications takeolls platforms by lyophilization for CELSS design [SAE PAPER 921134] p 287 A93-41322 [SAE PAPER 921323] p 304 A93-41485 [SAE PAPER 921197] p 295 A93-41373 SICONOLFI, S. F. SANDSTROEM, G. Hazard and risk assessment for surface components Program development for exercise countermeasures Characterization and classification of strains of of a lunar base Controlled Ecological Life Support [SAE PAPER 921140] p 292 A93-41327 Franctsella tularensis isolated in the central Asian focus System SIEGEL, BRIAN of the Soviet Union and in Japan [SAE PAPER 921285] p 302 A93-41451 Contact lenses in aviation - The Marine Corps [FOA-B-40421-4.4] p 275 N93-28200 SCHWARTZKOPF, S. H. experience p 289 A93-41172 SANTEE, W. R. Gray water recycling with a unique vapor compression SILVERSTEIN, JOANN Biophysical model for handwear insulation testing distillation (VCD) design Contaminant distribution and accumulation in water [AD-A262926] p 320 N93-28884 (SAE PAPER 921318] p 304 A93-41480 recycle systems SATO, KOZO SCHWARTZKOPF, STEVEN H. [SAE PAPER 921360] p 307 A93-41519 A trade study method for determining the design Anaerobic treatment of organic wastes from Controlled Inactivation of a model coliphage virus in water by parameter of CELSS subsystems Ecological Life Support Systems iodine [SAE PAPER921198] p295 A93-41374 [SAE PAPER 921272] p 301 A93-41442 [SAE PAPER 921361] p 274 A93-41520 B-10 PERSONAL AUTHOR INDEX TRUZHENNIKOV, A. N.

Generation of iodine disinfection by-products (IDP's) in STODIECK, L. S. TAN, G. a water recycle system Design and evaluation of a payload to support plant Recent regenerative ECLSS technology developments [SAE PAPER 921362] p 307 A93-41521 growth onboard COMET 1 in Europe SIMONDS, CHARLES H. [SAE PAPER 921389] p 308 A93-41547 [SAE PAPER 921332] p 304 A93-41493 Assessment of the state of the art in life support STOLKI, THOMAS J. TAN, M. N. environmental control for SEI p315 N93-27978 The development and testing of a volatile organics Human performance and physiological function during SIMONSEN, LISA C. concentrator for use in monitoring Space Station water a 24-hr exposure to 1 percent bromotrifluoromethane Radiation exposure predictions for short-duration stay quality (HalOn1301) p277 A93-39704 Mars missions [SAE PAPER 921266] p 300 A93-41436 Toxicokinetics of inhaled bromotrifluoromethane (Halon [AAS PAPER 92-107] p 277 A93-39261 STOLLE, MICHAEL F. 1301) in human subjects p 278 A93-39705 SINGH, INDRAMANI L. Hyperbaric treatment operations aboard Space Station TANAKA, KIYOSHI Freedom Performance consequences of automation-induced Conceptual study of manned lunar surface site 1 [ SAE PAPER 9211421 p 292 A93-41328 •complacency p 286 A93-39571 p316 N93-28031 SINGH, M. P. STOYCOS, LARA E. TASK, H. LEE Mathematical model for the exchange of gases in the Anthropometric data from launch and entry suited test Armstrong Laboratory space visual function tester lungs with special reference to carbon monoxide subjects for the design of a recumbent seating system program p 284 N93-28739 p 271 A93-39707 [NASA-TM-104769] p 321 N93-29044 SIRKO, ROBERT J. STRAUSS, ALVIN M. Effect of microgravity on several visual functions during Plant canopy transpiration in bioregenerative life support A feasibility study of hand kinematics for EVA analysis STS Shuttle missions: Visual Function Tester-Model 1 systems - The link between mechanistic and empirical using magnetic resonance imaging (VFT-1) p 284 N93-28740 models [SAE PAPER 921253] p 298 A93-41423 Effect af microgravity on visual contrast threshold during [SAE PAPER 921355] p 306 A93-41514 Power assist EVA glove development STS Shuttle missions: Visual Function Tester-Model 2 Plant growth modeling at the JSC variable pressure [SAE PAPER 921255] p 299 A93-41425 (VFT-2) p 284 N93-28741 growth chamber - An application of experimental design EVA Glove Research Team Effect of microgravity on the visual near point: Visual (SAE PAPER 921356] p 307 A93-41515 [NASA-CR-193014] p313 N93-27847 Function Tester-Model 4 (VFT-4) p 284 N93-28742 SITLER, GLENN A. A feasibility study of hand kinematics for EVA analysis TATARA, JAMES D. Dew point analysis for Space Station Freedom using magnetic resonance imaging p313 N93-27848 The analytical control program for the NASA Space [SAE PAPER 921227] p 296 A93-41401 A preliminary structural analysis of space-based Station Freedom Environmental Control and Life Support SJOESTEDT, A. inflatable tubular frame structures p 313 N93-27849 System (ECLSS) Water Recovery Test Characterization and classification of strains of Power assist EVA glove development [SAE PAPER 921269] p 300 A93-41439 Francisella tularensis isolated in the central Asian focus p 314 N93-27850 TATE, ISAO of the Soviet Union and in Japan STRIEPE, SCOTT A. Manned lunar surface site: Conceptual study on [FOA-B-40421-4.4] p 275 N93-28200 Radiation exposure predictions for short-duration stay pressurized lunar surface operation rover Use of RNA hybridization in the diagnosis of a case of Mars missions p316 N93-28032 [AAS PAPER 92-107] p 277 A93-39261 ulceroglandular tularemia TAYLOR, G. [FOA-B-40422-4.4] p 275 N93-28212 STROUP, T. Intraocular pressure and retinal vascular changes during SKWERES, JOYCE A. Crop interactions in polyculture and their implications transient exposure to microgravity p 278 A93-39710 Effects of refrigerating preinoculated Vitek cards on for CELSS design TAYLOR, R. M. microbial physiology and antibiotic susceptibility [SAE PAPER 921197] p 295 A93-41373 Operator and automation capability analysis: Picking the [SAE PAPER 921214] p 273 A93-41390 STYCZYNSKI, T. E. right team p 319 N93-28864 SLADE, HOWARD Gray water recycling with a unique vapor compression Evolving EVA system capability for the evolving Space distillation (VCD) design THEIS, RONALD L. A. Station Freedom requirements p312 N93-27791 [SAE PAPER 921318] p 304 A93-41480 Consumables and wastes estimations for the First Lunar SMITH, DAMON C. SUN, SHINFU Outpost Measurement of free and dissolved gas content of water Hypoxic ventilatory responsiveness in Tibetan compared [SAE PAPER 921287] p 302 A93-41453 samples on Space Station Freedom with Han residents of 3,658 m p 280 A93-41120 THILLY, W. G. [SAE PAPER 921267] p 300 A93-41437 Minimal hypoxic pulmonary hypertension in normal Comparative mutagenesis of human cells in vivo and SMITHERS, G. A. Tibetans at 3,658 m p 280 A93-41121 in vitro Aquatic biofilms and their responses to disinfection and SUN, SIDNEY C. [DE93-012269] p 276 N93-28651 invading species The Centrifuge Facility Life Sciences Glovebox THOMAS, MARK [SAE PAPER 921211] p 296 A93-41387 configuration study OCAM - A CELSS modeling tool: Description and SNYDER, GORDON [SAE PAPER 921158] p 293 A93-41341 results Instrumentation for microbial monitoring of SUTTON, JOHN R. [SAE PAPER 921241] p 298 A93-41413 decontamination or biocide system effectiveness Minimal hypoxic pulmonary hypertension in normal THOMPSON, JOHN [SAE PAPER 921233] p 297 A93-41407 Tibetans at 3,658 m p 280 A93-41121 Catalytic oxidation for treatment of ECLSS and PMMS SOLERSSI, ROSA SUVANTO, S. waste streams Mechanical stimulation of skeletal muscle increases The prediction of the adaptation of circadian rhythms [SAE PAPER 921274] p 301 A93-41443 prostaglandin F2(alpha) synthesis and cyclooxygenase to rapid time zone changes p 278 A93-39714 THONNARD, JEAN-LOUIS activity by a pertussis toxin sensitive mechanism SYMONS, J. D. Development of the Hermes EVA Space Suit Glove [NASA-CR-193041] p 282 N93-27102 Effects of sleep deprivation and exercise on glucose [SAE PAPER 921256] p 299 A93-41426 SON, CHANG H. tolerance p 281 A93-41165 TIBBITTS, T. W. Comparative test data assessment and simplified math SYMONS, J. M. A matrix-based porous tube water and nutrient delivery modelling for Sabatier CO2 reduction subsystem Use of sorption technology for treatment of humidity system [SAE PAPER 921228] p 296 A93-41402 condensate for potable water [SAE PAPER 921390] p 309 A93-41548 STANTON, CRAIG [SAE PAPER 921312] p 303 A93-41474 TILLOTSON, BRIAN Pressure, composition, and temperature control of cabin TRIALSS - Tool for Rapid and Intelligent Advanced Life atmosphere on Space Station Freedom Support System Selection and Sizing [SAE PAPER 921216] p 296 A93-41392 [SAE PAPER 921123] p 291 A93-41315 STAVERT, D. M. TINKLENBERG, J. Potential health hazards from thermal degradation TAERNVIK, A. Influence of aging and practice on piloting tasks events - Paniculate vs. gas phase effects Use of RNA hybridization in the diagnosis of a case of p 286 A93-39708 [SAE PAPER 921388] p 282 A93-41546 ulceroglandular tularemia TLEIMAT, B. W. STEELE, JOHN W. [FOA-B-40422-4.4] p 275 N93-28212 Gray water recycling with a unique vapor compression Space Station Water Processor - Current flight design TAKADA, MASAHARU distillation (VCD) design [SAE PAPER 921112] p 289 A93-41306 Manned lunar surface site: Conceptual study on [SAE PAPER 921318] p 304 A93-41480 The application of filtration technology within the Water pressurized lunar surface operation rover TLEIMAT, M. C. Processor on board Space Station Freedom p 316 N93-28032 Gray water recycling with a unique vapor compression [SAE PAPER 921270] p 300 A93-41440 TAKAHASHI, SHUUJI distillation (VCD) design Space Station Condensing Heat Exchanger biofilm Manned lunar surface site: Conceptual study on [SAE PAPER 921318] p 304 A93-41480 formation and control evaluation pressurized lunar surface operation rover TORN, HIROYUKI [SAE PAPER 921383] p 308 A93-41541 p 316 N93-28032 Manned lunar surface site p316 N93-28033 TRABANINO, RUDY STEPHENS, ROBERT L. TAKAMI, MASAKAZU The development and testing of a volatile organics The use of electrophysiological and cognitive variables Lunar surface experiment system p 316 N93-28034 in the assessment of degradation during periods of concentrator for use in monitoring Space Station water TAKANO, YUTAKA sustained wakefulness quality Conceptual study on manned lunar surface site [AD-A263033] p 283 N93-27923 [SAE PAPER 921266] p 300 A93-41436 p316 N93-28029 STERN, L. S. TRAUSCH, STEPHANIE V. Aminohydroxybutane bisphosphonate and clenbuterol TAKEDA, N. Performance evaluation of candidate space suit prevent bone changes and retard muscle atrophy Neuropharmacology of motion sickness and emesis - elements for the next generation orbital EMU respectively in tail-suspended rats p 271 A93-39703 A review p 271 A93-39711 [SAE PAPER 921344] p 305 A93-41503 STEWART, D. F. Motion sickness induced by sinusoidal linear TREDICI, G. Program development for exercise countermeasures acceleration in rats p 272 A93-39712 Long-lasting neuropsychological changes after a single [ SAE PAPER 921140 ] p 292 A93-41327 TAMPONNET, C. high altitude climb p 278 A93-39713 STILL, DAVID L. European involvement in CELSS - Definition of a Closed TRUZHENNIKOV, A. N. Contact lenses in aviation - The Marine Corps Ecological Systems Test Bed Oxygen regime in the frontal cerebral cortex of monkeys experience p 289 A93-41172 [SAE PAPER 921200] p 295 A93-41376 during a two-week space flight p 272 A93-40773

B-11 CORPORATE SOURCE INDEX

AEROSPACE MEDICINE AND BIOLOGY / A Continuing Bibliography (Supplement 379) September 1993

Typical Corporate Source Index Listing Army Research Inst. of Environmental Medicine, Domier Lufrfahit G.m.b.H., Friedrichshafen (Germany). Natlck, MA. Symbology for head up and head down applications for Biophysical model for handwear insulation testing highly agile fighter aircraft: To improve spatial awareness, | AD-A262926] p 320 N93-28884 trajectory control, and unusual attitude recovery, part 1 [CORPORATE SOURCE | Army Research Lab., Aberdeen Proving Ground, MD. p 318 N93-28857 A study of the effects of lens focal length on remote driver performance [AD-A263191] p 321 N93-28941 Air Force Systems Command, Brooks AFB, TX. — Introduction to training decisions modeling technol- ogies: The training decisions system B Edgerton, Germeshausen and Grier, Inc., Idaho Falls, [AD-A249862] p 27 N93-12252 ID. Bechtel National, Inc., San Francisco, CA. Crucial role of detailed function, task, timeline, link, and Oxygen production on the Lunar materials processing human vulnerability analyses in HRA frontier p315 N93-27967 [DE93-001923] p 321 N93-28942 <— TITLE Boeing Defense and Space Group, Huntsvllle, AL. Lunar base thermal management/power system Elliott-Automation Space and Advanced Military analysis and design p 315 N93-27985 Systems Ltd., Camberiey (England). British Aerospace Public Ltd. Co., Bristol (England). Pilot decision aiding for weapon delivery: A novel Oculo-motor responses and virtual image displays approach to fire control cueing using parallel computing Listings In this Index are arranged alphabetically by p319 N93-28862 p317 N93-28853 corporate source. The title of the document Is used to British Aerospace Public Ltd. Co., European Space Agency, Paris (France). provide a brief description of the subject matter. The Kingston-upon-Thames (England). Photobiological investigations on spores of page number and the accession number are Included Ergonomic development of digital map displays streptomyces griseus p 320 N93-28866 [ESA-TT-1269] p277 N93-29274 In each entry to assist the user In locating the abstract Brown Univ., Providence, Rl. In the abstract section. If applicable, a report number Mechanical stimulation of skeletal muscle increases Is also Included as an aid In Identifying the document. prostaglandin F2(alpha) synthesis and cyclooxygenase activity by a pertussis toxin sensitive mechanism [NASA-CR-193041] p 282 N93-27102 Growth factor involvement in tension-induced skeletal Federal Aviation Administration, Washington, DC. muscle growth Index of international publications in aerospace [NASA-CR-193023] p 282 N93-27113 medicine [AD-A262908] p 284 N93-28306 Federal Aviation Agency, Oklahoma City, OK. Comparison of portable crewmember protective California Univ., Irvine. breathing equipment (CPBE) designs Analysis of neural systems involved in modulation of [DOT/FAA/AM-93/6] p310 N93-27121 memory storage [AD-A262418] p 283 N93-27654 California Univ., San Diego, La Jolla. Wound healing and connective tissue metabolism: The role of hyperbaric oxygen therapy General Dynamics Corp., Fort Worth, TX. Advanced Aviation Concepts, Jupiter, PL. [AD-A262483] p 285 N93-28759 Head-steered sensor flight test results and How expert pilots think: Cognitive processes in expert Chemical Warfare/Chemical and Biological Defense implications p 318 N93-28859 decision making Information Analysis Center, Edgewood, MD. General Electric Co., Gilbert, AZ. [DOT/FAA/RD-93/9] p 288 N93-27103 Evaluation of test methods and requirements for Low-cost helmet-mounted displays respiratory protection systems 21 Advisory Group for Aerospace Research and [AD-A262616] p317 N93-28479 Development, Neuilly-Sur-Selne (France). [AD-A262466] p 317 N93-28757 Combat Automation for Airborne Weapon Systems: Evaluation and optimization of a flexible filtration system Georgia Univ., Athens. Man/Machine Interface Trends and Technologies for respiratory protection system 21 Expertise, text coherence, and constraint satisfaction: [AGARD-CP-520] p317 N93-28850 [AD-A262467] p 284 N93-28758 Effects on harmony and settling rate [AD-A262703] p 288 N93-28901 Aerospace Medical Research Labs., Wright-Patterson Civil Aeromedlcal Inst., Oklahoma City, OK. AFB, OH. Variations of time-to-incapacitation and Theory of signal detection and its application to visual carboxyhemoglobin values in rats exposed to two carbon target acquisition: A review of the literature monoxide concentrations H [AD-A262920) p 288 N93-28307 [DOT/FAA/AM-93/7] p 274 N93-27152 Variations in time-to-incapacitation and blood cynanide Hamilton Standard, Windsor Locks, CT. Armstrong Laboratory space visual function tester values for rats exposed to two hydrogen cyanide gas program p 284 N93-28739 Evolution of Space Station EMU PLSS technology concentrations recommendations p 312 N93-27790 Effect of microgravity on several visual functions during [DOT/FAA/AM-93-8] p 283 N93-27158 STS Shuttle missions: Visual Function Tester-Model 1 Accident proneness: A research review Harvard Univ., Cambridge, MA. (VFT-1) p284 N93-28740 [DOT/FAA/AM-93/9] p 288 N93-28622 Wide-bandwidth high-resolution search for extraterrestrial intelligence Effect of microgravity on visual contrast threshold during [NASA-CR-193137] p 322 N93-28895 STS Shuttle missions: Visual Function Tester-Model 2 (VFT-2) p 284 N93-28741 Hilton Systems, Inc., Cherry Hill, NJ. Age 60 Project: Consolidated database experiments Effect of microgravity on the visual near point: Visual Defence and Civil Inst. of Environmental Medicine, [HS-TR-8025-3C(R2(] p 314 N93-27851 Function Tester-Model 4 (VFT-4) p 284 N93-28742 Downsvlew (Ontario). Hunter Coll., New York, NY. Influence of the Cold Buster (tm) sports bar on heat Cognitive interface considerations for intelligent Gene transcription and electromagnetic fields debt, mobilization and oxidation of energy substrates cockpits p319 N93-28865 [DE93-010854] p276 N93-28848 AIResearch Mfg. Co., Los Angeles, CA. [AD-A262762] p 285 N93-28939 Dust protection for environmental control and life support Defence Research Agency, Bedford (England). systems in the lunar environment p 315 N93-27979 The design and development of the new RAF standard Arizona Univ., Tucson. HUD format p318 N93-28856 Closed ecological systems: From test tubes to Earth's Defence Research Agency, Famborough (England). biosphere p315 N93-27976 The quest for an integrated frying helmet IshlkawaJima-Harima Heavy Industries Co. Ltd., Tokyo (Japan). Army Aeromedlcal Research Lab., Fort Rucker, AL. p319 N93-28860 Manned lunar surface site: Conceptual study on The use of electrophysiological and cognitive variables Department of Energy, Washington, DC. in the assessment of degradation during periods of Proceedings of a Workshop on Molecular Nuclear pressurized lunar surface operation rover sustained wakefulness Medicine p 316 N93-28032 [AD-A263033] p 283 N93-27923 [DE93-010828] p 285 N93-28835 Lunar surface experiment system p316 N93-28034 C-1 JPL CORPORA TE SOURCE

Altered immunological response in mice subjected to National Aeronautics and Space Administration. John stress and exposed to fungal spores F. Kennedy Space Center, Cocoa Beach, FL. Jet Propulsion Lab., California Inst of Tech., [SAE PAPER 921215] p 274 A93-41391 Mapping of electrical muscle stimulation using MRI Pasadena. A feasibility study of hand kinematics for EVA analysis p279 A93-40549 Overview of NASA's 1991 Life Support Systems Analysis using magnetic resonance imaging OCAM - A CELSS modeling tool: Description and Workshop [SAE PAPER 921253] p 298 A93-41423 results [SAE PAPER 921118] p 290 A93-41310 Power assist EVA glove development [SAE PAPER 921241] p 298 A93-41413 Human life support during interplanetary travel and (SAE PAPER 921255] p 299 A93-41425 Advanced life support systems in lunar and Martian domicile. V - Mars expedition technology trade study for environments utilizing a higher plant based engineering NASA Specialized Center for Research and Training solid waste management paradigm (NSCORT) in space environmental health [SAE PAPER 921119) p 290 A93-41311 [SAE PAPER 921286] p 302 A93-41452 [SAEPAPER921358] p307 A93-41517 Human life support during interplanetary travel and National Aeronautics and Space Administration. domicile. VI - Generic modular flow schematic for hybrid Inactivation of a model coliphage virus in water by Lyndon B. Johnson Space Center, Houston, TX. iodine physical/chemical-biological life support systems Human performance and physiological function during [SAE PAPER 921120) p 290 A93-41312 [SAE PAPER 921361] p 274 A93-41520 a 24-hr exposure to 1 percent bromotrifluoromethane Joint Publications Research Service, Arlington, VA. Potential health effects of fume particles on the crew (Halon 1301) p277 A93-39704 JPRS report: Science and technology. Central Eurasia: of spacecrafts Toxicokinetics of inhaled bromotrifluoromethane (Halon Life sciences [SAE PAPER 921387] p 308 A93-41545 1301) in human subjects p 278 A93-39705 [JPRS-ULS-93-005J p276 N93-28683 Potential health hazards from thermal degradation Orthostatic intolerance during a 13-day bed rest does JPRS report: Science and technology. Central Eurasia: events - Paniculate vs. gas phase effects not result from increased leg compliance Life sciences [SAE PAPER 921388] p 282 A93-41546 P280 A93-41119 [JPRS-ULS-92-027] p276 N93-28684 Design and evaluation of a payload to support plant Cerebral blood velocity and other cardiovascular growth onboard COMET 1 responses to 2 days of head-down tilt [SAE PAPER 921389] p 308 A93-41547 P280 A93-41122 K Dark cycle monitoring of biological specimens on Space Overview of NASA's 1991 Life Support Systems Analysis Station Freedom Workshop Kawasaki Heavy Industries Ltd., Kobe (Japan). [SAE PAPER 921393] p 274 A93-41551 (SAE PAPER 921118] p 290 A93-41310 Manned lunar surface site p 316 N93-28033 EVA/manned systems p 312 N93-27789 Analysis of the Variable Pressure Growth Chamber using National Aeronautics and Space Administration. Ames the CASE/A simulation package Research Center, Morten Reid, CA. [SAE PAPER 921122) p 291 A93-41314 8-OH-DPAT does not interfere with habitation to Space Station Freedom Environmental Health Care Little (Arthur 0.), Inc., Cambridge, MA. motion-induced emesis in cats p 271 A93-38451 Program Hybrid oxygen system Direct measurement of capillary blood pressure in the (SAE PAPER 921138] p 292 A93-41325 [AD-A262417] p 317 N93-28464 human lip p279 A93-40550 Program development for exercise countermeasures Lockheed Engineering and Sciences Co., Houston, TX. Performance under dichoptic versus binocular viewing [SAE PAPER 921140] p 292 A93-41327 Assessment of the state of the art in life support conditions - Effects of attention and task requirements A comparison of two Shuttle launch and entry suits - environmental control for SEI p315 N93-27978 p287 A93-40772 Reach envelope, isokinetic strength, and treadmill tests Lockheed Missiles and Space Co., Sunnyvale, CA. Norepinephrine content in discrete brain areas and [SAE PAPER 921154] p 293 A93-41337 neurohypophysial vasopressin in rats after a 9-d spaceflight Simplified Aid For Crew Rescue (SAFR) Pilot investigation - Nominal crew induced forces in p 313 N93-27793 (SLS-1) p273 A93-41167 Performance and mood-state parameters during 30-day zero-g Los Alamos National Lab., NM. [SAE PAPER 921155] p 293 A93-41338 Evaluation of NO(x)-induced toxicity 6 deg head-down bed rest with exercise training Operational space human factors - Methodology for a [AD-A261034] p 283 N93-28122 p281 A93-41169 Overview of NASA's 1991 Life Support Systems Analysis DSO Workshop [SAE PAPER 921156] p 293 A93-41339 M [SAE PAPER 921118] p 290 A93-41310 A study to explore locomotion patterns in partial gravity Recycling and source reduction for long duration space environments Mainstream Engineering Corp., Rockledge, Fl_ habitation (SAE PAPER 921157) p 293 A93-41340 Lightweight passive microclimate cooling device [SAE PAPER 921121] p 290 A93-41313 Design of a Shuttle air and water prefilter for reduced [AD-A262262] p317 N93-28112 Visualization and modeling of factors influencing visibility gravity operation Massachusetts Inst. of Tech., Cambridge. in cornputer-aided crewstation design (SAE PAPER 921161] p 294 A93-41343 Comparative mutagenesis of human cells in vivo and [SAE PAPER 921135] p 292 A93-41323 Conceptual design of ECLSS microgravity test beds in vitro The Centrifuge Facility Life Sciences Glovebox [SAE PAPER 921164] p 294 A93-41346 [OE93-012269] p 276 N93-28651 configuration study A systems approach to water recovery testing for space McDonnell-Douglas Space Systems Co., Huntlngton [SAE PAPER 921158] p 293 A93-41341 life support - Initial biomedical results from the ECLSS Beach, CA. An approach to the functional optimization of the CELSS Water Recovery Test and plans for testbed utilization Evolving EVA system capability for the evolving Space Test Facility [SAE PAPER 921210] p 295 A93-41386 Station Freedom requirements p312 N93-27791 [SAE PAPER 921199] p 295 A93-41375 Microbiology operations and facilities aboard McDonnell-Douglas Space Systems Co., Huntsvllle, Al_ Consumables and wastes estimations for the First Lunar restructured Space Station Freedom Technologies for ECLSS evolution Outpost [SAE PAPER 921213] p 296 A93-41389 p311 N93-27720 [SAE PAPER 921287] p 302 A93-41453 Effects of refrigerating preinoculated Vitek cards on Mitre Corp., Bedford, MA. Metabolic responses to simulated extravehicular Head mounted displays for virtual reality activity microbial physiology and antibiotic susceptibility [AD-A263498] p 322 N93-29340 [SAE PAPER 921303] p 282 A93-41468 [SAE PAPER 921214] p 273 A93-41390 Mount Sinai School of Medicine, New York, NY. Biodeterioration of materials in water reclamation Altered immunological response in mice subjected to NASA supporting studies for microgravity research on systems stress and exposed to fungal spores eye movements [SAE PAPER 921311] p 303 A93-41473 [SAE PAPER 921215] p 274 A93-41391 [NASA-CR-193233] p 285 N93-29041 A novel membrane device for the removal of water vapor Microbiological concerns and methodological and water droplets from air approaches related to bacterial water quality in [SAE PAPER 921322] p 304 A93-41484 spaceflight N Water reclamation technology development for future [SAE PAPER 921232] p 297 A93-41406 long range missions Space Station Freedom food management National Aeronautics and Space Administration, [SAE PAPER 921351] p 306 A93-41510 [ SAE PAPER 921248 ] p 298 A93-41419 Washington, DC. Plant canopy transpiration in bioregenerative life support Enhanced softgoods structures for spacesuit Performance consequences of automation-induced systems - The link between mechanistic and empirical micrometeoroid/debris protective systems 'complacency' p 286 A93-39571 models [SAE PAPER 921258] p 299 A93-41428 Microfossils of the Early Archean Apex chert - New [SAE PAPER 921355] p 306 A93-41514 The development and testing of a volatile organics evidence of the antiquity of life p 272 A93-40308 Tests characterizing bioprocessor hardware for concentrator for use in monitoring Space Station water Absence of a growth hormone effect on rat soleus analytical modeling quality atrophy during a 4-day spaceflight p 272 A93-40548 [SAE PAPER 921357] p 307 A93-41516 [SAE PAPER 921266] p 300 A93-41436 Defining contamination control requirements for Direct measurement of capillary blood pressure in the Evaluation of capillary electrophoresis for in-flight ionic non-human research on Space Station Freedom human lip p279 A93-40550 contaminant monitoring of SSF potable water [SAE PAPER 921386] p 308 A93-41544 Geography of end-Cretaceous marine bivalve [SAE PAPER 921268] p 300 A93-41438 Design and evaluation of a payload to support plant extinctions p 273 A93-41075 An assessment of waste processing/resource recovery growth onboard COMET 1 OrthostaUc intolerance during a 13-day bed rest does [SAE PAPER 921389] p 308 A93-41547 technologies for lunar/Mars life applications not result from increased leg compliance [SAE PAPER 921271 ] p 300 A93-41441 Dark cycle monitoring of biological specimens on Space p280 A93-41119 Station Freedom Post-treatment of reclaimed waste water based on an Performance and mood-state parameters during 30-day [SAE PAPER 921393] p 274 A93-41551 electrochemical advanced oxidation process 6 dfsg head-down bed rest with exercise training The General Purpose Work Station, a spacious [SAE PAPER 921275] p 301 A93-41444 p281 A93-41169 microgravity workbench A hybrid regenerative water recovery system for Overview of NASA's 1991 Life Support Systems Analysis [SAE PAPER 921394) p 309 A93-41552 lunar/Mars life support applications Workshop Extravehicular activity technology discipline [SAE PAPER 921276] p 301 A93-41445 (SAE PAPER 921118) p 290 A93-41310 p314 N93-27859 Development of a regenerable metal oxide sheet matrix Program development for exercise countermeasures Manned systems technology discipline CO2 removal system [SAE PAPER 921140] p 292 A93-41327 p314 N93-27860 [SAE PAPER 921298] p 302 A93-41463

C-2 CORPORA TE SOURCE Veterans Administration Hospital

Portable life support system regenerative carbon dioxide Evaluation of the carbon dioxide removal assembly and water vapor removal by metal oxide absorbents requirements for the Space Station Freedom in the Manned preprototype hardware development and testing Tended Capability through Permanently Manned Capability Pennsylvania State Univ., University Park. [SAE PAPER 921299] p 303 A93-41464 configurations Electrophoretic separation of cells and particles from Biofilm formation and control in a simulated spacecraft [SAE PAPER 921231 ] p 297 A93-41405 rat pituitary and rat spleen water system - Three year results Development of a test protocol for evaluating EVA glove [NASA-CR-193073] p 276 N93-28415 [SAE PAPER 921310] p 303 A93-41472 performance Use of sorption technology for treatment of humidity [ SAE PAPER 921254 ] p 298 A93-41424 condensate for potable water The analytical control program for the NASA Space (SAE PAPER 921312] p 303 A93-41474 Station Freedom Environmental Control and Life Support Regenerable Microbial Check Valve - Life cycle tests System (ECLSS) Water Recovery Test Rockwell International Corp., Los Angeles, CA. results [SAE PAPER 921269] p 300 A93-41439 Virtual interface applications for airborne weapons [SAE PAPER 921316] p 303 A93-41478 Catalytic oxidation for treatment of ECLSS and PMMS systems p 318 N93-28858 Operation of a breadboard waste streams Requirements for pilot assistance in a thrust-vectoring liquid-sorbent/membrane-contactor system for removing [SAE PAPER 921274] p 301 A93-41443 combat aircraft p 320 N93-28870 carbon dioxide and water vapor from air Biodeterioration of materials in water reclamation Royal Air Force Inst of Aviation Medicine, [SAE PAPER 921321] p 304 A93-41483 systems Famborough (England). Performance evaluation of candidate space suit [SAE PAPER 921311) p 303 A93-41473 The physiological limitations of man in the high G elements for the next generation orbital EMU Determination of organic carbon and ionic accountability environment p 319 N93-28861 [SAE PAPER 921344] p 305 A93-41503 of various waste and product waters derived from ECLSS Operator and automation capability analysis: Picking the Space Shuttle crew compartment water recovery tests and Spacelab humidity condensate right team p 319 N93-28864 debris-contamination [SAE PAPER 921313] p 303 A93-41475 [SAE PAPER 921345] p 305 A93-41504 Environmental control and life support system Space Shuttle Orbiter oxygen partial pressure sensing p311 N93-27718 and control system improvements Environmental control and life support system [SAE PAPER 921347] p 305 A93-41506 evolution p311 N93-27719 Search Technology, Inc., Norcross, GA. Shuttle Orbiter Environmental Control and Life Support The ECLSS advanced automation project evolution and Specification of adaptive aiding systems System - Flight experience technology assessment p312 N93-27723 [AD-A263071] p314 N93-27927 [SAE PAPER 921348] p 305 A93-41507 Marshall Space Flight Center ECLSS technology Modeling of membrane processes for air revitalization activities p 312 N93-27724 and water recovery Man-systems integration and the man-machine [SAE PAPER 921352] p 306 A93-41511 interface p 313 N93-27795 Plant canopy transpiration in bioregenerative life support Technlon - Israel Inst. of Tech., Haifa. Environmental control and life support systems Visual field information in nap-of-the-Earth flight by systems - The link between mechanistic and empirical p 314 N93-27858 models teleoperated helmet-mounted displays [SAE PAPER 921355] p 306 A93-41514 Amino acid sequences for the binding regions in serum p311 N93-27177 albumin proteins Plant growth modeling at the JSC variable pressure Technische Univ., Berlin (Germany). [NASA-CASE-MFS-28402-1 ] p 276 N93-28952 growth chamber - An application of experimental design DOKMA: A document oriented communication model [SAE PAPER 921356] p 307 A93-41515 Computerized atmospheric trace contaminant control for medical applications as a basis of a role system in ASDA - Advanced Suit Design Analyzer computer simulation for manned spacecraft the medical field program [NASA-TM-108409] p 321 N93-28977 [ETN-93-93799] p 284 N93-28469 [SAE PAPER 921381 ] p 308 A93-41539 Process for selectively recovering algae and protozoa Texas MM Univ., College Station. First entry operations for spacecraft [NASA-CASE-MFS-26124-1-NPO] p 276 N93-29174 Alternative processes for water reclamation and solid [SAE PAPER 921384] p 308 A93-41542 National Aerospace Lab., Amsterdam (Netherlands). waste processing in a physical/chemical bioregenerative Regenerative Life Support Systems Test Bed Overview of cockpit technology research and life support system p311 N93-27721 performance - Lettuce crop characterization development programs for improvement of the Growing wheat to maturity in reduced gas pressures [SAE PAPER 921391) p 309 A93-41549 man/machine interface: Review of the AGARD AVP [NASA-CR-193245] p 277 N93-29216 Setting Spacecraft Maximum Allowable Concentrations Symposium held in Madrid, May 1992 Texas Technological Univ., Lubbock. for 1 hour or 24 hour contingency exposures to airborne p320 N93-28872 Human capabilities and limitations in situation chemicals National Defence Research Establishment, Umea awareness P 319 N93-28863 [SAE PAPER 921410] p 310 A93-41564 (Sweden). Texas Univ., Houston. The role of Environmental Health System air quality Intracellular targeting of the Yersinia YopE cytotoxin in 13 C NMR spectra of allosteric effectors of monitors in Space Station Contingency Operations mammalian cells induces actin microfilament disruption hemoglobin [SAE PAPER 921414] p 310 A93-41565 [FOA-B-40420-4.4] p 275 N93-27989 [AD-A262979] p 284 N93-28293 JSC ECLSS R/T program overview Plasmid encoded virulence of Yersinia p312 N93-27725 [FOA-B-40419-4.4] p 275 N93-28199 Extravehicular activity system p312 N93-27787 Characterization and classification of strains of u Man-systems distributed system for Space Station Francisella tularensis isolated in the central Asian focus Freedom p312 N93-27788 of the Soviet Union and in Japan Umea Univ. (Sweden). Evolving technologies for Space Station Freedom [FOA-B-40421-4.4] p 275 N93-28200 computer-based workstations p313 N93-27794 Plasmid encoded virulence of Yersinia Use of RNA hybridization in the diagnosis of a case of Anthropometn'c data from launch and entry suited test [FOA-B-40419-4.4] p 275 N93-28199 ulceroglandular tularemia subjects for the design of a recumbent seating system Umpqua Research Co., Myrtle Creek, OR. [FOA-B-40422-4.4] p 275 N93-28212 [NASA-TM-104769] p 321 N93-29044 Regenerable biocide delivery unit, volume 1 Anthropometric survey of the astronaut applicants and National Space Development Agency, Tokyo (Japan). [NASA-CR-185701] p 274 N93-27122 astronauts from 1985 to 1991 Conceptual study on manned lunar surface site Regenerable biocide delivery unit, volume 2 [NASA-RP-1304] p 321 N93-29324 p 316 N93-28029 [NASA-CR-185701-VOL-2] p 275 N93-27360 National Aeronautics and Space Administration. Nippon Electric Co. Ltd., Tokyo (Japan). United Technologies Corp., Farmlngton, CT. Langley Research Center, Hampton, VA. Conceptual study of manned lunar surface site SPE water electrolyzers in support of the lunar Radiation exposure predictions for short-duration stay p316 N93-28031 outpost p315 N93-27977 Mars missions Unlversitaet der Bundeswehr Muenchen, Neubiberg [AAS PAPER 92-107J p 277 A93-39261 (Germany). Performance consequences of automation-induced Pilot intent and error recognition as part of a knowledge 'complacency' p 286 A93-39571 based cockpit assistant p318 N93-28855 Identification of hazardous awareness states in Oak Ridge National Lab., TN. Utah Univ., Salt Lake City. monitoring environments Introductions to the Proceedings of the Fourteenth Sudden loading and fatigue effects on the human [SAE PAPER 921136] p287 A93-41324 Symposium on Biotechnology for Fuels and Chemicals spine EVA and telerobot interaction p312 N93-27792 [DE93-006235] p 276 N93-28890 [PB93-167526] p 286 N93-29199 Method of encouraging attention by correlating video Ohio State Univ., Columbus. game difficulty with attention level 13 C NMR spectra of allosteric effectors of [NASA-CASE-LAR-15022-1] p 288 N93-28128 hemoglobin National Aeronautics and Space Administration. [AD-A262979] p 284 N93-28293 Marshall Space Flight Center, Huntsvllle, Al_ Regulation of alternative CO2 fixation pathways in Vanderbllt Univ., Nashville, TN. Phase III Integrated Water Recovery Testing at MSFC procaryotic and eucaryotic photosynthetic organisms EVA Glove Research Team - Closed hygiene and potable loop test results and lesson [DE93-012109] p 276 N93-29181 [NASA-CR-193014] p 313 N93-27847 learned Orbital Technologies Corp., Madison, Wl. [SAE PAPER 921117] p 290 A93-41309 A feasibility study of hand kinematics for EVA analysis 1991 NASA Life Support Systems Analysis workshop using magnetic resonance imaging p 313 N93-27848 Initial accomplishments of the Environmental Control [NASA-CR-4466] p 310 N93-27100 and Life Support System (ECLSS) atmosphere A preliminary structural analysis of space-based revitalization (AR) predevelopment operational system test 1992 NASA Life Support Systems Analysis workshop inflatable tubular frame structures p 313 N93-27849 (POST) for the Space Station Freedom (SSF) [NASA-CR-4467] p310 N93-27101 Power assist EVA glove development [SAE PAPER 921186) p 294 A93-41365 Oxford Univ. (England). p 314 N93-27850 Aquatic biofilms and their responses to disinfection and A modular head/eye platform for real-time reactive Veterans Administration Hospital, San Francisco, CA. invading species vision Secondary injury factors and preventative treatment [SAE PAPER 921211 ] p 296 A93-41387 [OUEL-1941/92] p320 N93-28897 [PB93-176014] p283 N93-27409

C-3 Wright Lab. CORPORATE SOURCE w Wright Lab., Wright-Patterson AFB, OH. System automation and pilot-vehicle-interface for unconstrained low-altitude night attack p320 N93-28867 Wyle Labs., Inc., Huntsville, Al_ Increased fire and toxic contaminant detection responsibility by use of distributed, aspirating sensors p311 N93-27722

C-4 FOREIGN TECHNOLOGY INDEX

AEROSPACE MEDICINE AND BIOLOGY / A Continuing Bibliography (Supplement 379) September 1993

Typical Foreign Technology Index Listing Development of a 500 hPa shoulder joint for the European EVA Space Suit System [SAE PAPER 921257] p 299 A93-41427 JAPAN Design and preliminary testing of a membrane based High-altitude pulmonary edema with pulmonary [COUNTRY OF INTELLECTUAL ORIGIN | water recycling system for European manned space thromboembolism p 278 A93-39709 missions Neuropharmacology of motion sickness and emesis - [SAE PAPER 921396] p 309 A93-41553 A review p 271 A93-39711 Combat Automation for Airborne Weapon Systems: Motion sickness induced by sinusoidal linear ARMENIA Man/Machine Interface Trends and Technologies acceleration in rats p 272 A93-39712 — The response of medulla/ respiratory neurons lo the [AGARD-CP-520] p317 N93-28850 A trade study method for determining the design stimulation ol the amygdaloid nuclei under hypoxia parameter of CELSS subsystems 2 A93-12860 [SAE PAPER 921198] p 295 A93-41374 Development of the nitrogen fixation system for CELSS ^ TITLE GERMANY [SAE PAPER 921238] p 297 A93-41411 Concept of waste transferring mechanisms Ferrous iron oxidation by anoxygenic phototrophic (SAE PAPER 921239] p 297 A93-41412 bacteria p 271 A93-39280 Experimental and theoretical study on membrane Recent regenerative ECLSS technology developments distillation using thermopervaporation Listings In this Index are arranged alphabetically by in Europe [SAE PAPER 921397] p 309 A93-41554 country of Intellectual origin. The title of the document [SAE PAPER 921332] p 304 A93-41493 Conceptual study on manned lunar surface site is used to provide a brie) description of the subject Hermes ECLSS - Main requirements and technical p316 N93-28029 matter. The page number and accession number are solutions Conceptual study of manned lunar surface site Included In each entry to assist the user In locating the [SAE PAPER 921400] p 309 A93-41555 p 316 N93-28031 DOKMA: A document oriented communication model abstract In the abstract section. If applicable, a report Manned lunar surface site: Conceptual study on for medical applications as a basis of a role system in pressurized lunar surface operation rover number is also Included as an aid in Identifying the the medical field p316 N93-28032 document. [ETN-93-93799] p 284 N93-28469 Manned lunar surface site p 316 N93-28033 Pilot intent and error recognition as part of a knowledge Lunar surface experiment system p 316 N93-28034 based cockpit assistant p318 N93-28855 Symbology for head up and head down applications for highly agile fighter aircraft: To improve spatial awareness, N trajectory control, and unusual attitude recovery, part 1 p318 N93-28857 NETHERLANDS Photobiological investigations on spores of Barolrauma in Boeing 737 cabin crew streptomyces griseus p 278 A93-39706 [ESA-TT-12691 p 277 N93-29274 Inhibition of EGF-induced signal transduction by microgravity is independent of EGF receptor redistribution in the plasma membrane of human A431 cells p272 A93-39715 INDIA Overview of cockpit technology research and Mathematical model for the exchange of gases in the development programs for improvement of the lungs with special reference to carbon monoxide man/machine interface: Review of the AGARD AVP p 271 A93-39707 Symposium held in Madrid, May 1992 CANADA Body fluid compartments, renal blood flow, and p 320 N93-28872 Effects of long-term weightlessness on roll hormones at 6,000 m in normal subjects NORWAY circularvection p 279 A93-39725 p281 A93-41125 The psychological effects of isolation on a space station Effects of sleep deprivation and exercise on glucose - A simulation study tolerance p 281 A93-41165 INTERNATIONAL ORGANIZATION European involvement in CELSS - Definition of a Closed [SAE PAPER 921191] p 287 A93-41369 Influence of the Cold Buster (tm) sports bar on heat Ecological Systems Test Bed debt, mobilization and oxidation of energy substrates [SAE PAPER 921200] p 295 A93-41376 [AD-A262762] p 285 N93-28939 CHINA ISRAEL Performance under dichoptic versus binocular viewing Hypoxic ventilatory responsiveness in Tibetan compared conditions - Effects of attention and task requirements RUSSIA with Han residents of 3.658 m p 280 A93-41120 p287 A93-40772 Oxygen regime in the frontal cerebral cortex of monkeys New technologies for in-flight pasteless bioelectrodes during a two-week space flight p 272 A93-40773 p289 A93-41174 New technology for the analysis of the results of an Visual field information in nap-ot-the-Earth flight by ultrasound experiment performed in aviation-medicine DENMARK teleoperated helmet-mounted displays medical examination p 279 A93-40774 Influence of in vivo hypobaric hypoxia on function of p311 N93-27177 Functions simulation model of integrated regenerable lymphocytes, neutrocytes, natural killer cells, and ITALY life support system cytokines P 280 A93-41123 Long-lasting neuropsychological changes after a single [SAE PAPER 921201] p 295 A93-41377 high altitude climb p 278 A93-39713 JPRS report: Science and technology. Central Eurasia: Myosin and troponin changes in rat soleus muscle after Life sciences hindlimb suspension p 273 A93-41124. [JPRS-ULS-93-005] p 276 N93-28683 Labels and visual cues to reproduce an earthlike JPRS report: Science and technology. Central Eurasia: environment in space - Going ahead in designing Columbus FINLAND Life sciences APM interior architecture The prediction of the adaptation of circadian rhythms [JPRS-ULS-92-027] p 276 N93-28684 [SAE PAPER 921193] p 295 A93-41371 to rapid time zone changes p 278 A93-39714 The effects of a reduced pressure scenario on the FRANCE Columbus APM environmental control system Microgravity and orthostatic intolerance - Carotid [SAE PAPER 921247] p 298 A93-41418 hemodynamics and peripheral responses System integration and verification approach for the p278 A93-39716 environmental control system of the Columbus Attached SAUDI ARABIA Dynamic analysis of human visuo-oculo-manual Pressurised Module Case report - Chronic sub-dural hematoma following coordination control in target tracking tasks (SAE PAPER 921261) P 299 A93-4U31 high-speed ejection p 282 A93-41171 p287 A93-41166 Environmental control of the Mini Pressurized Logistic SWEDEN Norepinephrine content in discrete brain areas and Module Intracellular targeting of the Yersinia YopE cytotoxin in neurohypophysial vasopressin in rats after a 9-d spaceflight (SAE PAPER 921281] p 302 A93-41449 mammalian cells induces actin microfilament disruption (SLS-1) p273 A93-41167 Effects of air bubble contamination in recirculating water [FOA-B-40420-4.4] p 275 N93-27989 Development of the Hermes EVA Space Suit Glove loop Plasmid encoded virulence of Yersinia [SAE PAPER 921256] P 299 A93-41426 [SAE PAPER 921282] p 302 A93-41450 [FOA-B-40419-4.4] p 275 N93-28199

D-1 UNITED KINGDOM FOREIGN TECHNOLOGY INDEX

Characterization and classification of strains of Francisella tularensis isolated in the central Asian focus of the Soviet Union and in Japan [FOA-B-40421-4.4J p 275 N93-28200 Use of RNA hybridization in the diagnosis of a case of ulceroglandular tularemia (FOA-B-40422-4.4) p 275 N93-28212 u UNITED KINGDOM Cognitive predictors of vigilance p 287 A93-40771 Lile Support and Habitability Manual ESA PSS-03-406 [SAE PAPER 921338] p 305 A93-41497 Pilot decision aiding for weapon delivery: A novel approach to fire control cueing using parallel computing p317 N93-28853 The design and development of the new RAF standard HUD format p 318 N93-28856 The quest for an integrated flying helmet p319 N93-28860 The physiological limitations of man in the high G environment p 319 N93-28861 Oculo-motor responses and virtual image displays p319 N93-28862 Operator and automation capability analysis: Picking the right team p 319 N93-28864 Ergonomic development of digital map displays p 320 N93-28866 A modular head/eye platform for real-time reactive vision [OUEL-1941/92] p320 N93-28897

D-2 CONTRACT NUMBER INDEX

AEROSPACE MEDICINE AND BIOLOGY / A Continuing Bibliography (Supplement 379) September 1993

Typical Contract Number NAS2-13345 p304 A93-4U84 Index Listing NAS8-36407 p311 N93-27720 NAS8-38038 p 301 A93-41443 NAS8-38490 p 301 A93-41443 NAS8-50000 p294 A93-41365 NAS9-17822 p 302 A93-41463 NAS9-17900 p303 A93-41464 p 321 N93-29044 AFPROJ. 1121 p27 N93-12252 p 321 N93-29324 NAS9-18348 p 304 A93-41483 NAS9-18361 p303 A93-41478 p 274 N93-27122 p275 N93-27360 NCC2-229 p 271 A93-38451 NCC2-541 P292 A93-41323 NCC2-628 p303 A93-41473 NCC8-17 p 303 A93-41473 Listings In this Index are arranged alphanumerically NGR-05-007-407 p 272 A93-40308 by contract number. Under each contract number the NIH-ES-01247 p 308 A93-41545 accession numbers denoting documents that have NIH-ES-04872 p 308 A93-41545 been produced as a result of research done under the NIH-HD-00681 p 280 A93-41120 contract are shown. The accession number denotes p280 A93-41121 NIH-HL-01998 p 279 A93-41118 the number by which the citation Is Identified In the NIH-HL-07449 p 279 A93-41118 abstract section. Preceding the accession number Is NIH-HL-14985 p 280 A93-41120 the page number on which the citation may be found. p280 A93-41121 NIH-HL-20634 p 281 A93-41168 NIH-HL-39818 p 281 A93-41168 NIH-MO1-RR-00073 p 280 A93-41122 NSF BNS-89-19645 p 280 A93-41120 p280 A93-41121 NSF BSR-86-13583 p 272 A93-40308 AF-AFOSR-0413-91 p 285 N93-28759 NSF CDA-88-06866 p 291 A93-41319 DAPROJ. 1L1-62716-AH-70 p 321 N93-28941 NSF DMC-88-57851 p 291 A93-41319 DAPROJ. 3M1-61102-BS-15 p 283 N93-28122 NSF EAR-90-05744 p 273 A93-41075 DA PROJ. 3M1-62787-A-897 p 283 N93-27923 NSF INT-86-2045 p 273 A93-41075 N00014-90-J-1626 p 283 N93-27654 DAM017-87-C-7202 p 280 A93-41120 N00014-90-J-1648 p 284 N93-28293 p280 A93-41121 N00019-88-C-0288 p 320 N93-28870 DAMD17-91-C-1105 p297 A93-41408 PHS-R03-OHO-2821-01 p 286 N93-29199 DE-AC02-83CH-10093 p 276 N93-28890 RTOP 199-14-11-13 p280 A93-41119 DE-AC05-84OR-21400 p 276 N93-28890 RTOP 199-15-11-14 p280 A93-41119 DE-AC07-76ID-01570 p 321 N93-28942 RTOP 199-21-12 p281 A93-41169 DE-FG01-89CE-34023 p 276 N93-28848 RTOP 199-22-12 p 281 A93-41169 DE-FG02-86ER-60448 p 276 N93-28651 RTOP 199-22-22 p 281 A93-41169 DE-FG02-91ER-20033 p 276 N93-29181 RTOP 199-22-32 p 281 A93-41169 DHHS-R59-CCR-902269 p 283 N93-27409 RTOP 199-22-44 p 281 A93-41169 DLA900-86-C-2045 p317 N93-28757 RTOP 476-14-03 p 274 A93-41551 p 284 N93-28758 SMRC-07490-5A p 275 N93-27989 DTFA01-90-C-00042 p 288 N93-27103 SNSF-3,200,0092.85 p 279 A93-41117 DTFA02-90-90125 P 314 N93-27851 SNSRC-4426-3011 p 275 N93-27989 DTRS-57-88-C-00078 P 289 A93-39573 EPA-CR-818696-01-0 P 273 A93-41388 ESA-9254/90/NL/FG P 309 A93-41553 FFWF PROJECT P-6221 p 279 A93-41117 F19628-89-C-0001 P 322 N93-29340 F33615-86-C-4505 P 317 N93-28464 F33615-88-C-0014 p317 N93-28479 F33615-88-C-3612 p 314 N93-27927 NAGW-1197 p308 A93-41547 NAGW-1508 p273 A93-41075 NAGW-1527 p273 A93-41075 NAGW-17 p286 A93-39571 NAGW-1998 P 285 N93-29041 NAGW-2147 P 272 A93-40308 NAGW-2356 p307 A93-41517 p308 A93-41545 p282 A93-41546 NAGW-2546 p313 N93-27847 NAGW-2872 p 322 N93-28895 NAGW-825 p 272 A93-40308 NAG1-1296 p286 A93-39571 NAG2-410 p281 A93-41169 NAG2-414 p282 N93-27102 p282 N93-27113 NAG8-807 p276 N93-28415 NAG9-241 p297 A93-41406 NAG9-284 p 303 A93-41474 NAG9-505 p 297 A93-41406 NAG9-582 p 277 N93-29216 NASW-4470 p 310 N93-27100 p310 N93-27101 NAS10-11624 p279 A93-40549 NAS2-12852 p 292 A93-41323

E-1 REPORT NUMBER INDEX

AEROSPACE MEDICINE AND BIOLOGY / A Continuing Bibliography (Supplement 379) September 1993

Typical Report Number Index Listing DOT/FAA/AM-93/3 p 284 N93-28306 # S-718 p 321 N93-29324 • # DOT/FAA/AM-93/6 p 310 N93-27121 # S-720 p 321 N93-29044 * # DOT/FAA/AM-93/7 p 274 N93-27152 # SAE PAPER 921112 p 289 A93-41306 DOT/FAA/AM-93/9 p 288 N93-28622 # NASA ON SAE PAPER 921114 p 290 A93-41307 SPONSORED MICROFICHE SAE PAPER 921117 p 290 A93-41309 ' DOT/FAA/RD-93/9 p 288 N93-27103 # SAE PAPER 921118 p 290 A93-41310 SAE PAPER 921119 P 290 A93-41311 * NASA-CR-184429 . EGG-M-92402 p 321 N93-28942 # SAE PAPER 921120 p 290 A93-41312 ' SAE PAPER 921121 p 290 A93-41313 ' ESA-TT-1269 p277 N93-29274 # REPORT I SAE PAPER 921122 p 291 A93-41314 • SIUMBER | SAE PAPER 921123 p 291 A93-41315 ETN-93-93715 p 277 N93-29274 # U SAE PAPER 921125 p 291 A93-41316 ETN-93-93764 p 275 N93-28199 # SAE PAPER 921129 p 291 A93-41317 ETN-93-93765 p 275 N93-27989 # SAE PAPER 921131 p 291 A93-41319 ETN-93-93766 p 275 N93-28200 # SAE PAPER 921132 p 291 A93-41320 ETN-93-93767 p 275 N93-28212 # Listings In this index are arranged alphanumerically SAE PAPER 921133 p 291 A93-41321 ETN-93-93799 p 284 N93-28469 # SAE PAPER 921134 p 287 A93-41322 by report number. The page number indicates the ETN-93-93877 p 320 N93-28897 # page on which the citation Is located. The accession SAE PAPER 921135 p 292 A93-41323 ' SAE PAPER 921136 p 287 A93-41324 ' number denotes the number by which the citation Is FOA-B-40419-4.4 p 275 N93-28199 # SAE PAPER 921138 p 292 A93-41325 * Identified. An asterisk (*) Indicates that the item is a FOA-B-40420-4.4 p 275 N93-27989 # SAE PAPER 921139 p 292 A93-41326 NASA report. A pound sign (#) indicates that the Item FOA-B-40421-4.4 p 275 N93-28200 # SAE PAPER 921140 p 292 A93-41327 FOA-B-40422-4.4 p 275 N93-28212 # Is available on microfiche. SAE PAPER 921142 p 292 A93-41328 SAE PAPER 921149 p 292 A93-41333 HS-TR-8025-3C(R2) p 314 N93-27851 # SAE PAPER 921151 p 293 A93-41335 SAE PAPER 921154 p 293 A93-41337 • ISBN-92-835-0706-1 p317 N93-28850 # SAE PAPER 921155 p 293 A93-41338 ' AAS PAPER 92-107 p 277 A93-39261 ' SAE PAPER 921156 p 293 A93-41339 * JPRS-ULS-92-027 p 276 N93-28684 SAE PAPER 921157 p 293 A93-41340 ' AD-A261034 p 283 N93-28122 # JPRS-ULS-93-005 p 276 N93-28683 SAE PAPER 921158 p 293 A93-41341 * AD-A262262 p317 N93-28112 # SAE PAPER 921160 p 293 A93-41342 AD-A262417 p 317 N93-28464 # MTR-93B0000015 p 322 N93-29340 # SAE PAPER 921161 p 294 A93-41343 * AD-A262418 p 283 N93-27654 # SAE PAPER 921162 p 294 A93-41344 AD-A262466 p 317 N93-28757 # MAS 1.15:104769 p 321 N93-29044 ' SAE PAPER 921163 p 294 A93-41345 AD-A262467 p 284 N93-28758 # MAS 1.15:108409 p 321 N93-28977 ' SAE PAPER 921164 p 294 A93-41346 ' AD-A262483 p 285 N93-28759 # NAS 1.26:185701-VOL-2 p 275 N93-27360 SAE PAPER 921186 p 294 A93-41365 ' AD-A262616 p 317 N93-28479 # MAS 1.26:185701 p 274 N93-27122 SAE PAPER 921188 p 294 A93-41367 AD-A262703 p 288 N93-28901 # NAS 1.26:193014 p313 N93-27847 SAE PAPER 921189 p 294 A93-41368 AD-A262762 p 285 N93-28939 # NAS 1.26:193023 p 282 N93-27113 SAE PAPER 921191 p 287 A93-41369 AO-A262908 p 284 N93-28306 # NAS 1.26:193041 p 282 N93-27102 SAE PAPER 921193 p 295 A93-41371 AD-A262920 p 288 N93-28307 # NAS .26:193073 p276 N93-28415 SAE PAPER 921197 p 295 A93-41373 AD-A262926 p 320 N93-28884 # NAS .26:193137 p 322 N93-28895 SAE PAPER 921198 p 295 A93-41374 AD-A262979 p 284 N93-28293 # NAS .26:193233 p 285 N93-29041 SAE PAPER 921199 p 295 A93-41375 • AD-A263033 p 283 N93-27923 # NAS .26:193245 p 277 N93-29216 SAE PAPER 921200 p 295 A93-41376 AD-A263071 p 314 N93-27927 # NAS .26:4466 p310 N93-27100 SAE PAPER 921201 p 295 A93-41377 AD-A263191 p321 N93-28941 # NAS 1.26:4467 p310 N93-27101 ' SAE PAPER 921210 p 295 A93-41386 ' AD-A263498 p 322 N93-29340 # NAS 1.61:1304 p 321 N93-29324 SAE PAPER 921211 P 296 A93-41387 ' NAS 1.71 :LAR-15022-1 p 288 N93-28128 ' SAE PAPER 921212 p 273 A93-41388 AFOSR-93-0202TR p 285 N93-28759 # NAS 1.71 :MFS-26124-1-NPO p 276 N93-29174 SAE PAPER 921213 p 296 A93-41389 ' NAS 1.71 :MFS-28402-1 p 276 N93-28952 SAE PAPER 921214 p 273 A93-41390 ' AGARD-CP-520 p317 N93-28850 # SAE PAPER 921215 p 274 A93-41391 NASA-CASE-LAR-15022-1 p 288 N93-28128 ' # SAE PAPER 921216 p 296 A93-41392 AL-TR-1992-0014 p317 N93-28464 # SAE PAPER 921227 p 296 A93-41401 AL-TR-1992-0083 p 288 N93-28307 # NASA-CASE-MFS-26124-1 -NPO p276 N93-29174 ' SAE PAPER 921228 p 296 A93-41402 AL-TR-1993-0008 p 317 N93-28479 # NASA-CASE-MFS-28402-1 p276 N93-28952 ' SAE PAPER 921230 p 296 A93-41404 SAE PAPER 921231 p 297 A93-41405 * ARL-TR-25 p 321 N93-28941 # NASA-CR-185701 -VOL-2 p 275 N93-27360 ' SAE PAPER 921232 p 297 A93-41406 " NASA-CR-185701 p274 N93-27122 ' SAE PAPER 921233 p 297 A93-41407 CBIAC-SS-335 p 317 N93-28757 # NASA-CR-193014 p313 N93-27847 ' SAE PAPER 921234 p 297 A93-41408 CBIAC-SS-373 p 284 N93-28758 # NASA-CR-193023 p 282 N93-27113 ' SAE PAPER 921238 p 297 A93-41411 NASA-CR-193041 p 282 N93-27102 ' SAE PAPER 921239 p 297 A93-41412 CONF-920113-7 p 285 N93-28835 # NASA-CR-193073 p 276 N93-28415 SAE PAPER 921241 p 298 A93-41413 * CONF-920508-6 p 276 N93-28890 # NASA-CR-193137 p 322 N93-28895 SAE PAPER 921247 p 298 A93-41418 CONF-930661-1 p 321 N93-28942 # NASA-CR-193233 p 285 N93-29041 SAE PAPER 921248 p 298 A93-41419 • NASA-CR-193245 p 277 N93-29216 ' SAE PAPER 921249 p 298 A93-41420 DCIEM-92-60 p 285 N93-28939 # NASA-CR-4466 p310 N93-27100 ' SAE PAPER 921253 p 298 A93-41423 * NASA-CR-4467 p 310 N93-27101 ' SAE PAPER 921254 p 298 A93-41424 * DE93-001923 p 321 N93-28942 SAE PAPER 921255 p 299 A93-41425 * DE93-006235 p 276 N93-28890 NASA-RP-1304 p321 N93-29324 ' SAE PAPER 921256 p 299 A93-41426 DE93-010828 p 285 N93-28835 SAE PAPER 921257 p 299 A93-41427 DE93-010854 p 276 N93-28848 NASA-TM-104769 p 321 N93-29044 ' SAE PAPER 921258 p 299 A93-41428 * DE93-012109 p 276 N93-29181 NASA-TM-108409 : p 321 N93-28977 ' SAE PAPER 921261 p 299 A93-41431 DE93-012269 p 276 N93-28651 SAE PAPER 921264 p 299 A93-41434 NATICK-TR-93/OU p317 N93-28112 SAE PAPER 921265 p 299 A93-41435 DLR-FB-91-14 p 277 N93-29274 # SAE PAPER 921266 p 300 A93-41436 * NAWCADWAR-92086-60 p314 N93-27927 SAE PAPER 921267 p 300 A93-41437 DOE/CE-34023/T1 p 276 N93-28848 # SAE PAPER 921268 p 300 A93-41438 * OUEL-1941/92 p320 N93-28897 SAE PAPER 921269 p 300 A93-41439 * SAE PAPER 921270 p 300 A93-41440 DOE/ER-20033/1 p 276 N93-29181 # PB93-167526 p 286 N93-29199 DOE/ER-60448/T6 p 276 N93-28651 # PB93-176014 p283 N93-27409 SAE PAPER 921271 p 300 A93-41441 • SAE PAPER 921272 p 301 A93-41442 DOT/FAA/AM-93-8 p 283 N93-27158 # REPT-56913-10 p317 N93-28464 SAE PAPER 921274 p 301 A93-41443 •

F-1 SAE PAPER 921275 REPORT NUMBER INDEX

SAE PAPER 921275 p 301 A93-41444 ' SAE PAPER 921276 p 301 A93-41445 • SAE PAPER 921277 p 301 A93-41446 SAE PAPER 921281 p 302 A93-41449 SAE PAPER 921282 p 302 A93-41450 SAE PAPER 921285 p 302 A93-41451 SAE PAPER 921286 p 302 A93-41452 • SAE PAPER 921287 p 302 A93-41453 ' SAE PAPER 921298 p 302 A93-41463 ' SAE PAPER 921299 p 303 A93-41464 • SAE PAPER 921303 p 282 A93-41468 ' SAE PAPER 921310 p 303 A93-41472 * SAE PAPER 921311 p 303 A93-41473 SAE PAPER 921312 p 303 A93-41474 • SAE PAPER 921313 p 303 A93-41475 * SAE PAPER 921316 p 303 A93-41478 * SAE PAPER 921318 p 304 A93-41480 SAE PAPER 921320 p 304 A93-41482 SAE PAPER 921321 p 304 A93-41483 * SAE PAPER 921322 p 304 A93-41484 • SAE PAPER 921323 p 304 A93-41485 SAE PAPER 921332 p 304 A93-41493 SAE PAPER 921338 p 305 A93-41497 SAE PAPER 921344 p 305 A93-41503 ' SAE PAPER 921345 p 305 A93-41504 • SAE PAPER 921346 p 305 A93-41505 SAE PAPER 921347 p 305 A93-41506 * SAE PAPER 921348 p 305 A93-41507 • SAE PAPER 921350 p 306 A93-41509 SAE PAPER 921351 p 306 A93-41510 ' SAE PAPER 921352 p 306 A93-41511 ' SAE PAPER 921353 p 306 A93-41512 SAE PAPER 921354 p 306 A93-41513 SAE PAPER 921355 p 306 A93-41514 SAE PAPER 921356 p 307 A93-41515 * SAE PAPER 921357 p 307 A93-41516 ' SAE PAPER 921358 p 307 A93-41517 ' SAE PAPER 921359 p 307 A93-41518 SAE PAPER 921360 p 307 A93-41519 SAE PAPER 921361 p 274 A93-41520 ' SAE PAPER 921362 p 307 A93-41521 SAE PAPER 921376 p 308 A93-41534 SAE PAPER 921381 p 308 A93-41539 * SAE PAPER 921383 p 308 A93-41541 SAE PAPER 921384 p 308 A93-41542 • SAE PAPER 921386 p 308 A93-41544 • SAE PAPER 921387 p 308 A93-41545 ' SAE PAPER 921388 p 282 A93-41546 ' SAE PAPER 921389 p 308 A93-41547 SAE PAPER 921390 p 309 A93-41548 SAE PAPER 921391 p 309 A93-41549 ' SAE PAPER 921393 p 274 A93-41551 SAE PAPER 921394 p 309 A93-41552 ' SAE PAPER 921396 p 309 A93-41553 SAE PAPER 921397 p 309 A93-41554 SAE PAPER 921400 p 309 A93-41555 SAE PAPER 921410 p310 A93-41564 ' SAE PAPER 921414 p310 A93-41565 *

STI-TR-8925-001 p314 N93-27927 #

URC-80356 p 274 N93-27122 * # URC-80356 p 275 N93-27360 ' #

US-PATENT-APPL-SN-024547 p 276 N93-28952 • # US-PATENT-APPL-SN-029808 p 288 N93-28128 ' # US-PATENT-APPL-SN-045142 p 276 N93-29174 ' #

USAARL-93-5 p 283 N93-27923 #

USARIEMT7-93 p 320 N93-28884 #

F-2 ACCESSION NUMBER INDEX

AEROSPACE MEDICINE AND BIOLOGY / A Continuing Bibliography (Supplement 379) September 1993

Typical Accession Number Index Listing

A93-41411 p297 N93-27101 '# p310 N93-28859 # p318 A93-41412 p297 N93-27102 '# p282 N93-28860 # p319 A93-41413 ' p298 N93-27103 tt P288 N93-28861 # p319 NASA ON N93-27113 '# p282 N93-28862 # p319 A93-41418 p298 [SPONSORED! MICROFICHE N93-27121 # p310 N93-28863 # p319 A93-41419 ' p298 N93-27122 '# p274 N93-28864 # p319 p298 A93-41420 N93-27152 # P274 N93-28865 # p319 A93-41423 ' p298 N93-10890 • tt p31 N93-27158 # P283 N93-28866 tt p320 p298 A93-41424 ' N93-27177 p311 N93-28867 # p320 p299 A93-41425 * N93-27360 • # P275 N93-28870 # p320 ACCESSION PAGE A93-41426 p299 I NUMBER NUMBER N93-27409 # p283 N93-28872 # p320 A93-41427 p299 N93-27654 # P283 N93-28884 # p320 A93-41428 ' p299 N93-27718 '# P311 N93-28890 tt p276 A93-41431 p299 N93-27719 '# p311 N93-28895 ' # p322 A93-41434 p299 N93-27720 • # P311 N93-28897 # p320 A93-41435 p299 Listings In this Index are arranged alphanumerically N93-27721 't p311 N93-28901 # p288 A93-41436 ' p300 N93-27722 ' # p311 N93-28939 # p285 by accession number. The page number-Indicates the A93-41437 p300 N93-27723 ' # p312 N93-28941 # p321 page on which the citation Is located. The accession p300 A93-41438 ' N93-27724 • # P312 N93-28942 # p321 p300 number denotes the number by which the citation Is A93-41439 ' N93-27725 * # p312 N93-28952 ' # p276 p300 identified. An asterisk (•) Indicates that the Item Is a A93-41440 N93-27787 ' # P312 N93-28977 ' # p321 A93-41441 ' p300 NASA report. A pound sign (#} Indicates that the item N93-27788 ' # P312 N93-29041 •# p285 A93-41442 p301 N93-27789 ' # P312 N93-29044 * # p321 is available on microfiche. p301 A93-41443 ' N93-27790 •# P312 N93-29174 •# p276 A93-41444 ' p301 N93-27791 '# P312 N93-29181 # p276 p301 A93-41445 * N93-27792 " # P312 N93-29199 # p286 p301 A93-41446 N93-27793 ' # P313 N93-29216 '# p277 p302 A93-41449 N93-27794 * # P313 N93-29274 # p277 p302 A93-38451 ' P271 A93-41309 ' p290 A93-41450 N93-27795 " # p313 N93-29324 * # p321 A93-41451 p302 A93-39261 ' P277 A93-41310 p290 N93-27847 ' # P313 N93-29340 # p322 A93-41452 * p302 A93-41311 ' p290 N93-27848 ' # p313 A93-39280 p271 p302 A93-41312 * p290 A93-41453 ' N93-27849 • # p313 A93-39571 P286 p302 A93-41313 ' p290 A93-41463 ' N93-27850 ' # p314 A93-39572 P286 A93-41464 ' p303 A93-41314 ' p291 N93-27851 # p314 A93-41468 ' p282 A93-39573 p289 A93-41315 p291 N93-27858 ' # p314 p289 A93-41472 * p303 A93-39574 A93-41316 p29l N93-27859 '# P314 p286 A93-41473 p303 A93-39575 A93-41317 p291 N93-27860 * # p314 A93-41474 * p303 A93-39703 P271 A93-41319 p291 N93-27923 # P283 A93-41475 " p303 A93-39704 ' p277 A93-41320 p291 N93-27927 # p314 A93-41478 ' p303 A93-39705 ' P278 A93-41321 p291 N93-27967 ' # P315 A93-41480 p304 A93-39706 p278 A93-41322 p287 N93-27976 ' # p315 A93-41482 p304 A93-39707 P271 A93-41323 " p292 N93-27977 ' # P315 A93-41483 ' p304 A93-39708 p286 A93-41324 ' p287 N93-27978 ' # p315 A93-41484 ' p304 A93-39709 P278 A93-41325 * p292 N93-27979 ' # P315 A93-41485 p304 A93-39710 P278 A93-41326 p292 N93-27985 ' # p315 A93-41493 p304 A93-39711 P271 A93-41327 p292 N93-27989 # P275 A93-41497 p305 A93-39712 P272 A93-41328 p292 N93-28029 # p316 A93-41503 ' p30S A93-39713 P278 A93-41333 p292 N93-28031 # P316 A93-41504 ' p305 A93-39714 p278 A93-41335 p293 N93-28032 # p316 A93-41505 p305 A93-39715 P272 A93-41337 ' p293 N93-28033 # P316 A93-41506 ' p305 A93-39716 p278 A93-41338 ' p293 N93-28034 # p316 A93-41507 ' p305 A93-39717 P272 A93-41339 * p293 N93-28112 # P317 A93-41509 p306 A93-39725 P279 A93-41340 * p293 N93-28122 # p283 A93-41510 ' p306 A93-40308 " P272 A93-41341 ' p293 N93-28128 '# P288 A93-41511 ' p306 A93-40548 ' P272 A93-41342 p293 N93-28199 # P275 A93-41512 p306 A93-40549 ' P279 A93-41343 ' p294 N93-28200 # P275 A93-41513 p306 A93-40550 P279 A93-41344 p294 N93-28212 # P275 A93-41514 p306 A93-40771 P287 A93-41345 p294 N93-28293 # P284 A93-41515 ' p307 A93-40772 ' P287 A93-41346 * p294 N93-28306 # P284 p307 A93-40773 P272 A93-41365 * p294 A93-41516 ' N93-28307 # P288 A93-41517 ' p307 A93-40774 P279 A93-41367 p294 N93-28415 '# P276 p307 A93-41075 ' p273 A93-41368 p294 A93-41518 N93-28464 # P317 A93-41519 p307 A93-41117 P279 A93-41369 p287 N93-28469 # p284 A93-41520 * p274 A93-41118 p279 A93-41371 p295 N93-28479 # p3!7 A93-41521 p307 A93-41119 P280 A93-41373 p295 N93-28622 # P288 A93-41534 p308 A93-41120 P280 A93-41374 p295 N93-28651 # P276 p308 A93-41121 P280 A93-41375 " p295 A93-41539 " N93-28683 # p276 p308 A93-41122 ' P280 A93-41376 p295 A93-41541 N93-28684 # P276 A93-41542 • p308 A93-41123 P280 A93-41377 p295 N93-28739 '# p284 A93-41544 ' p308 A93-41124 P273 A93-41386 ' p295 N93-28740 ' # P284 p308 A93-41125 p281 A93-41387 * p296 A93-41545 ' N93-28741 ' # P284 p282 A93-41165 P281 A93-41388 p273 A93-41546 ' N93-28742 ' # P284 A93-41547 p308 A93-41166 p287 A93-41389 ' p296 N93-28757 # P317 p309 A93-41167 ' P273 A93-41390 ' p273 A93-41548 N93-28758 # P284 A93-41549 * p309 A93-41168 P281 A93-41391 p274 N93-28759 # P28S A93-41551 p274 A93-41169 P281 A93-41392 p296 N93-28835 # P28S A93-41552 ' p309 A93-41170 P281 A93-41401 p296 N93-28848 tt P276 p309 A93-41171 p282 A93-41402 p296 A93-41553 N93-28SSO # p317 P289 A93-41554 p309 A93-41172 A93-41404 p296 N93-28853 # P317 A93-41173 p289 A93-41555 p309 A93-41405 • p297 N93-288S5 tt P318 A93-41174 P289 A93-41564 ' p310 N93-28856 tt P318. A93-41175 p289 A93-41406 ' p297 A93-41565 ' p310 A93-41306 P289 A93-41407 p297 N93-28857 # P318 A93-41307 P290 A93-41408 p297 N93-27100'# p310 N93-28858 tt P318 G-1 AVAILABILITY OF CITED PUBLICATIONS

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PUBLIC COLLECTION OF NASA DOCUMENTS An extensive collection of NASA and NASA-sponsored publications is maintained by the British Library Lending Division, Boston Spa, Wetherby, Yorkshire, England for public access. The British Library Lending Division also has available many of the non-NASA publications cited in STAR. European requesters may purchase facsimile copy or microfiche of NASA and NASA-sponsored documents, those identified by both the symbols # and * from ESA — Information Retrieval Service European Space Agency, 8-10 rue Mario-Nikis, 75738 CEDEX 15, France.

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APP-2 ADDRESSES OF ORGANIZATIONS

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APP-3 CASI PRICE TABLES (Effective August 1,1993)

STANDARD PRICE DOCUMENTS

NORTH PRICE AMERICAN FOREIGN CODE PRICE PRICE

A01 $9.00 $18.00 A02 12.50 25.00 A03 17.50 35.00 A04-A05 19.50 39.00 A06-A09 27.00 54.00 A10-A13 36.50 73.00 A14-A17 44.50 89.00 A18-A21 52.00 104.00 A22-A25 61.00 122.00 A99 Call For Price Call For Price

MICROFICHE

NORTH PRICE AMERICAN FOREIGN CODE PRICE PRICE A01 $9.00 $18.00

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IMPORTANT NOTICE

CASI Shipping and Handling Charges U.S.—ADD $3.00 per TOTAL ORDER Canada and Mexico—ADD $3.50 per TOTAL ORDER All Other Countries—ADD $7.50 per TOTAL ORDER Does NOT apply to orders requesting CASI RUSH HANDLING. CASI accepts charges to American Express, Diners Club, MasterCard and VISA.

Diners Club International" J

APP-5 REPORT DOCUMENT PAGE 1. Report No. 2. Government Accession No. 3. Recipient's Catalog No. NASA SP-7011 (379)

4. Tide and Subtitle 5. Report Date Aerospace Medicine and Biology September 1993 A Continuing Bibliography (Supplement 379) 6. Performing Organization Code JTT 7. Author(s) 8. Performing Organization Report No.

10. Work Unit No. 9. Performing Organization Name and Address

NASA Scientific and Technical Information Program 11. Contract or Grant No.

12. Sponsoring Agency Name and Address 13. Type of Report and Period Covered National Aeronautics and Space Administration Special Publication Washington, DC 20546-0001 14. Sponsoring Agency Code

15. Supplementary Notes

16. Abstract This report lists 305 reports, articles and other documents recently announced in the NASA STI Database.

17. Key Words (Suggested by Author(s)) 18. Distribution Statement Aerospace Medicine Unclassified - Unlimited Bibliographies Subject Category - 52 Biological Effects

19. Security Classif. (of this report) 20. Security Classif. (of this page) 21. No. of Pages 22. Price Unclassified Unclassified 110 A06/HC

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