Teehraology for Large Space Systems
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https://ntrs.nasa.gov/search.jsp?R=19860015242 2020-03-20T15:23:10+00:00Z NASA SP-7046(13) Teehraology for March 1986 NASA Large Space Systems • A Bibliography with Indexes {NASA-SP-70U6 (13) ) TECHNOLOGY FOB LARGE N86-24713 SPACE SYSTEHS: A BIBLJOGHAPHY HUH INDEXES {National Aeronautics and Space Administration) 111 p HC A06 CSCI 22A Onclas H1/12 13361 NASA SP-7046(13) TECHNOLOGY FOR LARGE SPACE SYSTEMS A BIBLIOGRAPHY WITH INDEXES Supplement 13 Compiled by Technical Library Branch and Edited by Space Systems Division NASA Langley Research Center Hampton, Virginia A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system between January 1 and June 30,1985 in Scientific and Technical Aerospace Reports (STAR) International Aerospace Abstracts (IAA) Scientific and Technical Information Branch 1986 National Aeronautics and Space Administration Washington, DC NOTE TO AUTHORS OF PROSPECTIVE ENTRIES The compilation of this bibliography results from a complete search of the STAR and IAA files Many times a report or article is not identified because either the title, abstract, or key words did not contain appropriate words for the search A number of words are used, but to best insure that your work is included in the bibliography, use the words Large Space Structures somewhere in your title or abstract, or include them as a key word This supplement is available from the National Technical Information Service (NTIS), Springfield, Virginia 22161 at the price code A07 ($16 95 domestic; $33 90 foreign) INTRODUCTION This bibliography is designed to be helpful to the researcher and manager engaged in developing technology within the discipline areas of the Large Space Systems Technology (LSST). Also, the designers of large space systems for approved missions (in the future) will utilize the technology described in the documents referenced herein This literature survey lists 399 reports, articles and other documents announced between January 1, 1985 and June 30, 1985 in Scientific and Technical Aerospace Reports (STAR), and International Aerospace Abstracts (IAA). The coverage includes documents that define specific missions that will require large space structures to achieve their objectives. The methods of integrating advanced technology into system configurations and ascertaining the resulting capabilities is also addressed. A wide range of structural concepts are identified. These include erectable structures which are earth fabricated and space assembled, deployable platforms and deployable antennas which are fabricated, assembled, and packaged on Earth with automatic deployment in space, and space fabricated structures which use pre-processed materials to build the structure in orbit. The supportive technology that is necessary for full utilization of these concepts is also included These technologies are identified as analysis and design techniques, structural and thermal analysis, structural dynamics and control, electronics, advanced materials, assembly concepts, and propulsion A separate companion document "Space Station Systems Bibliography" (NASA SP-7056) incorporates space station technology not applicable to large space systems Space station systems technology that is also applicable to large space systems may be documented in both bibliographies Robert L Wright, Space Systems Divison Sue K Seward, Technical Library Branch TABLE OF CONTENTS Page Category 01 Systems 1 Includes mission and program concepts and requirements, focus missions, conceptual studies, technology planning, systems analysis and integration, and flight experiments. Category 02 Analysis and Design Techniques 6 Includes interactive techniques, computerized technology design and development programs, dynamic analysis techniques, environmental modeling, thermal modeling, and math modeling. Category 03 Structural Concepts 10 Includes erectable structures (joints, struts, and columns), deployable platforms and booms, solar sail, deployable reflectors, space fabrication techniques and protrusion processing Category 04 Structural and Thermal Analysis 13 Includes structural analysis and design, thermal analysis and design, analysis and design techniques, and thermal control systems Category 05 Structural Dynamics and Control 17 Includes modeling, systems identification, attitude and control techniques, surface accuracy measurement and control techniques and systems, sensors and actuators. Category 06 Electronics 29 Includes techniques for power and data distribution, antenna RF performance analysis, communications systems, and spacecraft charging effects Category 07 Advanced Materials 35 Includes matrix composites, polyimide films and thermal control coatings, bonding agents, antenna components, manufacturing techniques, and space environmental effects on materials Category 08 Assembly Concepts 41 Includes automated manipulator techniques, EVA, robot assembly, teleoperators, and equipment installation. Category 09 Propulsion 43 Includes propulsion concepts and designs utilizing solar sailing, solar electric, ion, and low thrust chemical concepts. Category 10 General 50 Includes either state-of-the-art or advanced technology which may apply to Large Space Systems and does not fit within the previous categories. Publications of conferences, seminars, and workshops are covered in this area. 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 PRECEDING PAGE BLANK NOT FILMED TECHNOLOGY FOR LARGE SPACE SYSTEMS A Bibliography (Suppl. 13) MARCH 1986 01 A85-13016# UTILIZATION AND ECONOMICS OF A EUROPEAN LOW EARTH ORBIT SPACE PLATFORM SYSTEMS R C PARKINSON and I V FRANKLIN (Bntish Aerospace, PLC, Space and Communications Drv, Stevenage, Herts , England) Includes mission and program concepts and requirements, focus International Astronautical Federation, International Astronautical missions, conceptual studies, technology planning, systems Congress, 35th, Lausanne, Switzerland, Oct 7-13, 1984 7 p analysis and integration, and flight experiments (IAF PAPER 84-57) In addition to the manned, core station, the facilities of the Space Station are to include also a Teleoperated Service Vehicle, A85-12502# a cryogenic Orbit Transfer Vehicle, and unmanned Space Platforms SPACE EXPLOITATION - SPACELAB AN EASY APPROACH Following President Reagan's invitation for international FOR DEVELOPING COUNTRIES: PROSPECTIVES AND participation in the Space Station program, the Space Platform is SUGGESTIONS BY AERITALIA of particular interest to Europe A Space Platform is defined as E VALLERANI (Aentaha SpA, Turin, Italy) IN International an unmanned orbiting facility in which essential services are Scientific Conference on Space, 23rd, Rome, Italy, March 24, 25, supplied by a common Resources Module while payloads can be 1983, Proceedings Rome, Rassegna Internazionale Elettronica attached or recovered on a temporary basis The present Nucleate ed Aerospaziale, 1984, p 45-49 investigation is concerned with the extent of potential interest in The problem of access by developing countries to space Europe in using such a Platform, the associated costs of information and resources is discussed from the Italian point of development and operation, and the economic attractions to view The international cooperation involved in the development Europe of undertaking such a development It is concluded that of IRIS, Spacelab, and Eureca is considered, the ongoing the Space Platform (or Platforms) appears to represent a commercialization of space in the STS, Anane, and Space Station cost-effective area of participation in the U S Space Station programs is examined, and the need for careful planning and program, at a cost Europe could afford, and with a function useful preparation in the developing countnes to take advantage of future both to Europe and the U S G R space-exploitation opportunities is stressed It is proposed that Italian universities and industry provide assistance in training personnel and designing payloads to meet the needs of developing countnes T K A85-13045# A85-130090 SOME RESULTS OF THE MSAT PHASE B STUDIES AND THEIR UTILIZATION OF A TELEOPERATED SERVICE VEHICLE FOR IMPACT ON SYSTEM DESIGN SPACECRAFT SERVICING J L MCNALLY, H R RAINE, and J D B KENT (Canadian C COUGNET (Matra, SA, Toulouse, France) and C BERGER Department of Communications, Communications Research Centre, (Matra, S A, Velizy-Villacoublay, Yvelmes, France) International Nepean, Ontano, Canada) International Astronautical Federation, Astronautical Federation, International Astronautical Congress, International Astronautical Congress, 35th, Lausanne, Switzerland, 35th, Lausanne, Switzerland, Oct 7-13, 1984 15 p Research Oct 7-13, 1984 10 p. refs supported by the European Space Agency (IAF PAPER 84-89) (IAF PAPER 84-48) In 1980, the Department of Communications (DOC) decided to Potential, commercially oriented European space missions are commence Phase A feasibility studies for a mobile satellite system discussed in terms of the required capabilities, equipment, and in the 800 MHz band The considered system would use a applications A trend toward heavier lift launch vehicles is foreseen, geostationary satellite to provide direct communication with vehicles together with an interface with a long-life orbital base of operations in nonurban areas throughout Canada including offshore coverage and teleoperated