Literaturverzeichnis

In Erganzung zum Literaturverzeichnis, bei dem meist nur einzelne Arbeiten zitiert werden, Se! 1m fol• genden eine V"bersicht iiber einen Teil der bereits erschienenen Biicher gegeben, die sich direkt oder am Rand.. mit Raketentreibstoffen befassen_

ALEMASOW, 'V. E.: Teoria raketnich dwigatelei, Moskau 1962. ALTMAN, D., J. M. CARTER, S. S. PENNER, and M. SUMMERFIELD: Liquid Propellant Rockets, Princeton Aero• nautical Paperbacks No.1, Princeton University Press, 189 p. (1960). B.-I.RRlmE, M., A. JAUI\WTTE, B. FRAEIJS DE VEUBEKE und J. VANDENKERCKHOVE: Raketenantriebe (Deutsche iibC)rarbeitl'te und erweiterte Ausga1~' von: La Propulsion par Fuse~·s). Elsevier Publishing Company. Amsterdam. 907 p. (19fl1). BOLLINGER, L. E .. M. GOLDS:lHTH, and A. \V. LEM~WN (Editors): Liquid Rockets and Propellants, Progress in Astronautics and Rocketry Vol. 2, Academic Press, New York-London, 682 p. (1960). -, and A. W. LE~moN (Editors): Proceedings of the Prop311ant Therm:liynamics and Handling Conference July 20 to 21,1959, Engng. Exp. Station, Ohio State Univ., Columbus 10, Ohio, Special Rep:lrt No. 12, 590 p. (1960). CARTON, O. S., W. R. l\L-I.XWELL, and D. HURD EN (Editors): Rocket Propulsion Technology, Vol. 1, Cranfield Symposium 1961. Plenum Press, New York, 374 p. (1961). GOULD, R. F. (Editor): Advanced Propellant Chemistry, ACS Advances in Chemistry Series, Vol. 54, Washing• ton, 290 p. (1966). HESSE, W. J., and N. Y. S. MUMFORD: Jet Propulsion for Aerospace Applications, Pitman Publ. Corp., New York (1964). HtTGGETT. C., C. E. BARTLEY, and M. M. MILLS: Solid Propellant Rockets, Princeton Aeronautical Paperbacks No.2, Princeton University Press, 167 p. (1960). KOELLE, H. H.: Handbook of Astronautical Engineering, McGraw Hill Book CJmp., Inc., New York (1961). MEBUS, H. G.: B3rechnung von Raketentriebwerken, C. F. Winter'sche Verlagshawllung, Fussen, 120 S. (1957). MELEK-PASHAYEV, N. 1.: Liquid-Propellant Engines, Translated by W. E. JONES and B. P. MULLINS, Pergamon Press, New York - London - Paris, 175 p. [1962]. PENNER, S. S.: Chemical Reactions in Flow Systems, AGARDograph No.7, Butt:Jr\vorths Scientific Publi• cations, London, 86 p. (1955). -- Chemistry Problems in Jet Propulsion, Pergamon Press, New York-London-Paris, 394 p. (1957). - -, and J. DUCARME (Editors): The Chemistry of Propellants, Pergamon Press, Oxford-London-New York, 651 p. (1960). -. and F. A. WILLIAMS (Editors): Detonation and Two-Phase Flow, Progress in Astronautics and Rocketry Vol. 6, Academic Press, New York - London, 368 p. (1962). HAGOZIN, N. A.: Jet Propulsion FuelR, Edited by B. P. MULLINS, International Series on Aeronautics and Astro• nautics, Vol. 3. Pergamon Press, Oxford - London - New York - Paris, 168 p. (1961). HING, E. (Editor): and Pressurization Systems, Prentice-Hall Space Technology Sm·ips. Prentice-Hall, Inc., Englewood Cliff8, N. J., 310 p. (1964). SAR~ER, S. F.: Propellant Chemistry, Reinhold Publ. Corp., New York, 400 p. (1966). SIEGEL, B., and L. SCHIELER: Energetics of Propellant Chemistry, J. \Viley & Sons, New York - London -- Sydney, 240 p. (1964). SSINJAREW, G. B., i M. \Y. DOBROWOLSSKIJ: Sehidkostnije raketnije dwigateli, Oborongis, Moskau, 580 S. (1957). STE~DmR, J.: R'1ketenantriebe, Schweizer Druck- und Verlagshaus AG., Zurich, 523 S. (1952). SUMMERFIELD, M. (Editor): Solid Prop3llant Rocbt R9search, Progress in Astronautics and Rocketry, Vol. 1, Academic Press, New York - London, 692 p. (1960). SUTTON, G. P.: RockC't Propulsion Elem3nts, J. Wiley & Sons, New York - London, 3rd Edition, 464 p. (1963). WARREN, F. A.: Rocket Prop3llants, Reinhold Publishing Corp., New York, 218 p. (1958). WILKINS, R. L.: Theoretical Evaluation of Ch?mical Prop311ants, Prentice-Hall International Series in Space Technology, Prentic3-Hall, In;:., Englewood Cliffs, N. J., 463 p. (1963). \VOLFHARD, H. G., I. GLASS}TA'!'!, and L. GREE (Editors): HeterogencousCombustion, Progress in Astronautics and Aeronautics Vol. 15, Academic Press. New York - London, 76;') p. (1964). 716 Literaturverzeichnis A

Verzeichnis der Abkiirzungen

AEC Atomic Energy Commission AGRR Arbeitsgemeinschaft fiir Raketentechnik und Raumfahrt, TH Stuttgart ASME American Society of Automotive Engineers BAM Bundesanstalt fiir Materialpriifung DFL Deutsche Forschungsanstalt fiir Luft- und Raumfahrt, Braunschweig DLR Deutsche Luft- und Raumfahrt DVL Deutsche Versuchsanstalt fiir Luft- und Raumfahrt, Porz-Wahn ELDO European Launcher Development Organization, Paris ESRO European Space Research Organization ICC Interstate Commerce Commission JPL Jet Propulsion Laboratory, Pasadena, Calif. NACA National Advisory Committee for Aeronautics, 'Vashington NASA National Aeronautics and Space Administration, Washington NBS National Bureau of Standards USAF US Air Force WADC Wright Air Development Center, Dayton, Ohio

Die Abkiirzung der Zeitschriften entspricht dem im wissenschaftlichen Schrifttum iiblichen Modus. Bei Adv. Cryog. Engng. handelt es sich jedoch nicht urn eine Zeitschrift, sondern urn die von K. D. TIMMERHAUS herausgegebene Serie von Jahrbiichern der Cryogenic Engineering Conference, Verlag Plenum Press, New York. Zahlen nach N- oder AD- bezeichnen die Referat-Nummer in NASA Scientific and Aerospace Reports bzw. ASTIA Technical Abstracts Bulletin.

A

1. ARMSTRONG, G. T., and R. S. JESSUP: J. Res. Nat. Bur. Stand. 64 A, 49-59 (1960). 2. ARMSTRONG, G. T., S. MARANTZ, and C. F. COYLE: Nat. Bur. Stand. Rept. No. 6584, Washington, D. C. (1959). 3. Allied Chemical: Oxygen Difluoride, Product Data Sheet. 4. Allied Chemical: Chlorine Trifluoride and Other Halogen Fluorides, Tech. Bulletin TA-8532-2. 5. Air Products and Chemicals Inc., Allentown, Pa., Defense and Space Division: Data Sheets DS 100-111 (N2F4) and DS 100-112 (NF3). 6. ALLEN, H., and M. L. PINNS: Relative Ignitability of Typical Solid Propellants With Chlorine Trifluoride, NASA TN D-1533 (Jan. 1963), 24 p. 7. ARMSTRONG, G. T.: J. Am. Chem. Soc. 81, 3798 (1959). 8. ANDERSON, R., and R. O. McLAREN: Thermochemistry of Oxygen-Fluorine-Bonding, United Technology Corp., Quart. Techn. Summ. Rept. a) No.1 (July 1961) 13 p. AD 267307, b) No.2 (Oct. 1961) 12 p. AD 266688, c) No.3 (Febr. 1961) 28 p. AD 272311. 9. ADRIAN, F. J., E. L. COCHRAN, and V. A. BOWERS: Am. Chern. Soc., Advances in Chemistry Series 36, 50-67 (1962). 10. ALBERT, A. A., et al.: Electronic Configuration and Behavior of the NF2-GroUP, Hercules Powder Co., Quart. Rep. No.1 (June 15,1963),46 p., Ref.: NASA STAR N 63-17603. 11. ALLEY, C. W., A. W. HAYFOR.D, and H. F. SCOTT: Studies on Nitrogen Tetroxide Corrosion, Wright Air Dev. Ccnter, Tech. Rept. 60-384 (1960), 64 p., OTS PB Rept. 171301 (1960), Ref.: CA 57, 14871 (1962) und in: Werkstoffe-Korrosion 14,200 (1963). 12. Allied Chemical, Nitrogen Division: Nitrogen Tetroxide, Product Development Booklet NT-1. 13. Allied Chemical, Product Development Department: Nitrogen Tetroxide as an Oxidizer in Rocket Propul- sion, Product Development Booklet. 14. Anonym: Nitrogen Tetroxide Characteristics, Aviation Age 30: 3, 63-4 (Sept. 1958). 15. ALLEY, C. W., A. W. HAYFORD, and H. F. SCOTT: Corrosion 17,479 (1961), Ref.: CZ 1962,16479. 16. ADDISON, C. C.: Angew. Chemie 72, 193-7 (1960). 17. ADDISON, C. C., et al.: J. Chern. Soc. London 1951, 1289-93. 18. Army Chemical Center: A Test Series Conducted to Determine the Feasibility of Using Water Fog or a Thermal Updraft to Control or Disperse the Fumes Resulting from Spills of N20 4 , Edwards AFB 6593 TEst Group (Nov. 1962), 16 p., Contract AF-l\HPR-(33-616) 60-20, Rd.: XASA STAR N 63-111 34; AD291813. Literaturverzeichnis A 717

19. Aerojet-Gen. Corp.: Heat Transfer Characteristics of Unsymm. Dimethylhydrazine, Aerojet Rept. TCR-147 (Dec. 11, 1958). 20. ASTON, J. G., J. L. WOOD, and T. P. ZOLKI: J. Am. Chern. Soc. 75. 6203 (1953). 21. Army Chemical Center, Md.: Modified Type A-18 UDMH + Hydrazine Servicing Trailer, Edwards AFB, 6593th Test Group (Nov. 1962), 206 p., SSD-TDR-62-176, Ref.: NASA STAR N 63-11133. 22. ASHMORE, P. G., B. P. LEVITT, and B. A. TRUSH: Trans. Farad. Soc. 52, 830-48 (1956) and Naturc 176. 1013-5 (1955). 23. AUDRIETH, L. F.: J. Am. Chern. Soc. 76, 1428-30 (1954). 24. AUDRIETH, L. F., and B. ACKERSON-OGG: The Chemistry of Hydrazine, J. Wiley& Sons, New York (1951). 25 .•\erojet-Gen. Nucleonics, Chern. and Engng. N"ews 41: 37, 88-9 (16 Sept. 1963). 26. AUDRIETH, L. F., W. NESPITAL, and H. ULICII: J. Am. Chern. Soc. 55,673 (1933). 27. ASKEY, P. J.: J. Am. Chern. Soc. 52, 970-4 (1930). 28. ARNOLD and JOHNSON: US Pat. 2771343 (20 Nov. 1956), Inh.: Olin Mathieson C. C. 29. AUDRIETH, L. F., and P. H. MOHR: Ind. Engng. Chern. 43,1774-9 (1951). 30. ASTON, J. G., et al.: J. Am. Chern. Soc. 73, 1939-43 (1951). 31. ASHLEY, E.: Heat Transfer Measurements for WFNA, Bell Aircr. Corp. Rept. 56-982-016 (16. Feb. 1953). 32. Army Chemical Center, Edgewood, Md. and Edwards AFB 6593 Test Group: Modified Type B-2 Fuming Nitric Acid Servicing Semi-Trailer, Final Rept. SSD-TDR-62-174 (Nay. 19(2) 96 p., Ref.: NASA STAR N 63-11022. 33. AYLETT, B. J.: J. Chern Soc. [London] 1957, 4152-4. 34. ASTON, J. G., E. J. ROCK, and S. ISSEROW: J. Am. Chern Soc. 74, 2484-6 (1952). 35. ASTON, J. G., et al.: J. Am. Chern. Soc. 73, 1943-5 (1951). 36. ADAM, A. R., et al.: Anal. Chern. 32,1319-20 (1960). 37. American Petrol. Inst.: Tables of Thermodynamic Propertics, Res. Project No. 44, Vol. I-Y (1947). 38. ALLEN, S.: J. BIS 14, 165-8 (1955). 39. ABEL, E.: Monatsh. f. Chemie 83, 422-39 (1952). 40. ANDERSON, W. A., J. G. KAUFMAN, and J. Eo KANE: Adv. Cryog. Engng. 9,104-11 (1964). 41. ADKINS, A. W., 1. A. BLACK, et al.: Storage, Servicing, Transfer, and Handling of Hydrogen; A. D. Little Inc., Cambridge, Rept. AFFTC TRol-18, ContractAF 33(616)7330, Proj. D(1-8119) (May 1961) 162 p., AD 268201. 42. ARRICK, C. D.: Adv. Cryog. Engng. 3, 218-25 (1960). 43. Allied Chemical: Fluorine, Elemental. Product Information; Technical Bulletin TA-85411, Fluorine, Product Data Sheet PD-TA-85413 (19i58), Liquid Fluorine Unloading Procedure, Product Data Sheet PD-TB-85411 (7-58). 44. ADAMS, D. F.: Anal. Chern. 32, 1312-5 (1960). 45. ANDERSON, R., et al.: J. Phys. Chern. 56, 473-4 (1952). 46. AYERS, A. L., and C. R. SCOTT: US Pat. 2842936 (15.7.1958), Inh.: Phillips Petrol. Co. 47. AYERS, A. L., and C. R. SCOTT: US Pat. 2874535 (24. FebI'. 1959), Inh.: Phillips Petrol. Co., Ref.: CA 53, 9621 b (1959). 48. ALTMAN: Thermodynamic Properties and Calculated Rocket Performance of Hydrogen up to 20000 oK, JPL Rept. 20-106 (Sept. 1956) 28 p. 49. AGRON, P. A., et al.: Science 139, 842-3 (1963). 50. ARMSTRONG, D. L.: Liquid Propellants for gockets, in: The Chemistry of Propellants, ed. by S. S. PENNER and J. DUCARME, Pergamon Press 1960, p. 121-68. 51. ANSCHUTZ, R. H.: Adv. Cryog. Engng. 5, 62-8 (1960). 52. ARNETT, R. W.: Adv. Cryog. Engng. 7, 214-8 (1962). 53. AUBLE, C. M.: A Study of Injection Processes for Liquid Oxygen and Gaseous Hydrogen in a 200 Pound Thrust Rocket Engine, NACA gM E56-1 25a (9. Jan. 1957), 32 p. 54. ABRAMSON, A. E.: Investigation of Internal Film Cooling of Exhaust Nozzle of a 1000-pound-Thrust Liquid Ammonia/Liquid Oxygen Rocket, NACA RM E52-C 26 (June 1952), 18 p. 55. ARP, V., et al.: Cryogenics 2, 230-5 (Junc 19(2). 56. ARNETT, R. W., D. R. MILLHISER, and W. H. PROBERT: Adv. Cryog. Engng. 8, 256-62 (1963). 57. ANDREWS, D. G. R., and O. GRAY: Comb. and Flame 8,113-26 (1964). 58. ADELMAN: Ignition Lag Characteristics of Some Hydrazine-Nitric Acid Propellant Systems, CIT JPL Progr. Rept. 20-164 (Jan. 1952), 10 p. 59. AYERS, A. L., and C. R. SCOTT: US Pat. 2859587 (11.11.1958), Inh.: Phillips Petrol. Co., Ref.: CA53, 4703f. (1959). 60. AYERS, A. L., and C. R. SCOTT: US Pat. 2932941, Inh.: Phillips Petrol. Co. (8.11. 1951/19.4.1960). 61. ADAMS, G. K., W. G. PARKER, and H. G. WOLFHARD: Discuss. Farad. Soc. 1953, No. 14, 97-103. 62. ALTlIIAN, D., J. M. CARTER, S. S. PENNER, and M. SUMMERFIELD: Liquid Propellant Rockets, Princeton Aeronautical Paperbacks, No.1, Princeton Univ. Press 1960. 63. ADELMAN, B.: A Study of Ignition Lag Characteristics of Some Liquid Rocket Fuels with RFNA, Including Additives to the Oxidizer, CIT JPL ProgI'. Rept. 20-138 (April 1951), 14 p. 64. ADAMS, G. K., and G. B. COOK: Comb. and Flame 4,9-18 (1960). 718 Literaturverzeichnis A

65. ADAMS, G. K., and G. W. STOCKS: 4th Sympos. on Comb., Cambridge, Mass., p. 239-48 (Pub. 1953). 66. ANTOINE, A. C.: 8th Symp. on Combust., Williams & Wilkins, Baltimore 1962, p. 1057 -9. 67. ANTOINE, A. C.: Comb. and Flame 6,364-5 (1962). 68. AUDRIETH, L. F., and D. W.RYKER: US Pat. 2943927 (5 July 1960), Inh.: Olin Mathieson C. C., Ref.: CA 54, 21763e; CZ 1962,6272. 69. ARS Commitee on Monopropellant Test Methods: Card Gap Test for Shock Sensitivity of Liquid Mono• propellants, Recommended Test No.1, ARS-Preprint 287 -56 (1956), Minimum Pressure for Vapor• Phase Ignition, Recommended Test No.2, ARS-Preprint 386-57 (1957). 70. ANGELOFF, G. T.: Research and Development of the Ballistic Bomb as a Tool Determining Experimental Performance of Liquid and Solid Rocket Propellants, Olin Mathieson C. C., Quart. Progr. Rapt. No.5, 1 June-31 Aug. 1959 (1 Sept. 1959), 7 p., AD 226841 see also AD 220072. 71. ALTMAN, D., and D. D. THOMAS: Evaluation of Hydrazine as a Monopropellant and a Gas Generant, CIT JPL Progr. Rept. 9-36 (17 April 1949). 72. ALTMAN, D., and D. D. THOMAS: Evaluate Nitromethane for Rockets, Aviation Week 1949, p. 27-37 (16 May 1949). 73 ...\RDEN, E. A., and J. POWLING: Comb. and Flame 2, 55-68 (1958), and: 6thSympos. on Comb., Yale Univ. 1956, 177-83 (1957). 74. AMSTER, A. B., G. D. EDWARDS, et al.: Research on the Safety Characteristics of Normal Propyl Nitrate, NAVORD Progress Rept. No.1, Oct. 1955-15 March 1956, NAVORD Rept. 4309 (5 June 1956), 27 p., AD 103726. 75. AMSTER, A. B., G. D. EDWARDS, and J. B. LEVY: Research on the Safety Characteristics of Normal Propyl Nitrate, Part II, NAVORD Terminal Rept. 15 March - 1 July 1956, NAVORD Rept. 4493 (13 March 1957),23 p., AD 132758. 76. AlliSTER, A. B., and J. B. LEVY: ARS-J. 30, 280-1 (1960). 77. AllISTER, A. B., and J. B. LEVY: ARS-J. 29, 870-1 (1959). 78. ALTSHULLER, A. P.: Calculated Heats of Formation and Combustion of Boron Compounds (Boron, Hydro- gen, Carbon, Silicon), NACA RM E55-G26 (4 Oct. 1955), Declass., 17 July 1958. 79. ANDERSON, W. E., and E. F. BARKER: J. Chem. Phys. 18,698-705 (1950). 80. ALLEN, H., and S. TANNENBAU:I1: Anal. Chem. 31, 265-8 (1959), vgl. auch NACA RM E54-L15 (1955). 81. ALTWICKER, E. R., et al.: US Pat. 3038012 (28.3. 1955/5. 6. 1962), Inh.: Olin Mathieson C. C.; US Pat. 3052725 (12. 10. 1955/4. 9. 1962), Inh.: Olin Mathieson C. C. 82. ALTWICKER, E. R., et al.: US Pat. 2999117 (28.3.1955/5.9.1961), Inh.: Olin Mathieson C. C., Ref.: CZ 1963, 10312. 83. AUDRIETH, L. F., and W. L. JOLLY: J. Phys. ColI. Chem. 55, 524-31 (1951). 84. ARMOND, J. W.: DAS 1125960 (24.2.1959/22.3. 1962), Engl. Prior. vom 24.2. 1958, Inh.: British Oxygen Co. Ltd., Ref.: CZ 1963, 9460. 85. AHLERT, R. C., G. L. BAUERLE, and J. V. LECCE: J. Chem. Engng. Data 7,158-60 (1962). 86. ARMSTRONG, D. L., and VY. P. KNIGHT: US Pat. 3108431 (11. 11. 1956/29. 10. 1963), Ref.: CA 60, 1530 g (1964). 87. ADKINS, A. W., and I. A. BLACK: Handbook for Hydrogen Handling Equipment, Suppl. I, A. D. Little Inc. (May 1961), 144p., AD 258562. 88. c\DKINS, A. W., and I. A. BLACK: More Power for Take-Off: SPRITE, Aeroplane 1950,100-2 (Jan. 1950)_ 89. AVERY, H. E., and J. N. BRADLEY: Trans. Farad. Soc. 60, 857-64 (1964). 90. ANDRUS SOW, L.: Explosivstoffe 6,285-9 (1958). 91. ALLEN, H., and E. A. FLETCHER: Combustion of Highly Reactive Fuels in a Mach 2 Wind Tunnl'l, NASA Memo 1-15-59E (1959), 28 p., supersedes NACA RM E57-E 15. 92. ALSPACH, W. J., and T. M. FLYNN: Adv. Cryog. Engng. 10, 246-52 (1965). 93. ANTOINE, A. C.: Effect of Pressure on Rate of Burning (Decomposition with Flame) of Liquid Hydrazine. NASA-TN-D-2694 (March 1965), 11 p., N65-17463. 94. ALLEN, H., and E. A. FLETCHER: A Study of the Combustion of Aluminumborohydride in a Small Super• sonic Wind Tunnel, NASA TN D-296 (July 1960), 15 p. 95. ANCTIL, A. A., and E. B. KULA: Adv. Cryog. Engng. 10, 102 (1965.) 96. AUKERMAN, C., and B. E. CHURCH: Experimental Hydrogen-Fluorine Rocket Performance at Low Pres• sures and High Ratios, NASA-TM-X-724 (Sept. 1963),35 p., Declassified N 66-33325. 97. ARBIT, H. A., and S. D. CLAPP: Fluorinc-Hydrogen Performance Evaluation, Rocketdyne Rept. R-6636-1, Contract NASw-1229, NASA-CR-54978 (Aug. 1966), 224 p., N 66-32923. 98. Al\]STER, A. B., et al.: Evaluation of Ozone Difluoride as a Liquid Propellant Additive, Stanford Research Inst., Menlo Park, Calif., Proj. SRI-5075, NASA CR-54833, NAS 3-4187 (1 Dec. 1966), Nfl7-38655. 99. AMSTER, A. B., et al.: Explosivstoffe 14, 33-5 (1966). 100. Anonym: Design Equation Analysis for Heat Transfer to Cryogenic Hydrogen at Pressures from 600 to 1500 psia and Wall to Bulk Temperature Ratios to 20, Aerojet Gen. Co., Sacramento, RN-S-0274. NASACR-87 511 (June 1966) 65 p., N67-34804. Literaturverzeichnis B 719

B 1. BURG, A. B.: Volatile Inorganic Fluorides, in: Fluorine Chemistry, edited by J. H. SIMMONS, Vo!' 1, p. 86-9, Academic Press, New York 1950. 2. BRAUER, G.: Handbuch del' praparativen anorganischen Chemic, 2. Auf!., 1. Bd., F. Enke Verlag, Stutt- gart 1960. 3. BOOTH, H. S., and J. T. PINKSTON: Chern. Rev. 41,421-39 (1947). 4. BANKS A. A., A.DAVIES, and A. J. RUDGE: J. Chern. Soc. [Lond.] 1903, 732. 5. BANKS, A. A.: J. Chern. Soc. [Lond.] 1900,191-3. 6. BANKS, A. A .. H. J. EMELEUS, and A. A. WOLF: J. Chem. Soc. [Lond.] 1949, 2861. 7. BENEDICT, W. S., et a!.: J. Opt. Soc. Am. 43, 1106 (1953). 8. BARTZ, D. R: Jet Propulsion 28, 46-53 (1958), auch erschienen als ARS Preprint 417 -57. 9. BRANSFORD, J. W., A. C. KUNKLE, and A. W. JACHE: J. Inorg. Nuc!. Chern. 14,159-60 (1960). 10. BREAZEALE, J. D.: Thermochemistry of Oxygen-Fluorine-Bonding, United Techno!. Corp., Contract Nom. 3433(00) ARPA 184-62. a) Quart. Summ. Rept. No.6 (1962), 21 p., NASA TPA N62-16350, b) Quart. Summ. Rept. No.7 (7 Jan. 1963),22 p., NASA STAR N63-11690. 11. BENDER, O. C.: Titan II Propellant Handling and Compatibility Problems, AIAA Preprint 63-086 (1963). 12. BRICE, D. B., and N. FISHMAN: ARS J. 29, 354-7 (1959). 13. BEATTI, J. R, and A. J. VOSPER: J. Chem. Soc. [Lond.] 1961, 2106. 14. BROCKAW, R S.: Correlation of Turbulent Heat Transfer in a Tube for the Dissociating System N 20 4 ;=, 2N02, NACA RM E57-K19a (1958),17 p. 15. BRADLEY, R S.: Trans. Farad. Soc. 02, 1255-9 (Sept. 1956). 16. BARUA, A. K., and P. K. CHAKRABORTI: J. Chern. Phys. 36, 2817-20 (1962).

17. BOROK, M. T.: Methode zur Messung del' N02·Konzentration in Gasgemischen nach dem Warmeeffekt del' Dissoziationsreaktion (in Russisch), Betriebslaboratorien USSR 27, 426-31 (1961), Ref.: CZ 1963, 11 758. 18. BIRDSEYE: Experimental Investigation of Heat Transfer Characteristics of Liquid Nitrogen Tetroxide, JPL Tech. Rep. 32-37 (14 Oct. 1960), 20 p. 19. BURGESS, D., J. GRuMER,and M. G. ZABETAKIS: Rescarch on the Fire and Explosion Hazards Associated With New Liquid Propellants, US Bur. Mines, Final Progr. Rept. No.9 (31 Aug. 1961), 18 p. 20. BOST, J. J., and R. E. BERNARD (Aerojet-Gen. Corp.): Chemical Cleaning of Titan II Engines, Proc. 4th Symp. of the Soc. of Aerospace Materials Process Engineers (SAMPE), Hollywood (1962), 24 p.

21. BERMAN, L. D.: Compatibility of Materials With Storage Propellants (N20 4 and Aerozine-50), Proc. 4th Symp. of the Soc. of Aerospace Materials Process Engineers (SAMPE), Hollywood (1962), 19 p. 22. BACK, K. C., and A. A. THOMAS: Pharmacology and Toxicology of UDMH, Wright Patterson AFB, 6570th Aerospace Med. Res. LabR .. Final Rept. AMRL TDR 62-118 (Oct. 19(2), 12 p., Ref.: NASA STAR N63-11226. 23. BACK, K. C., et a!.: Absorption, Distribution and Excretion of UDMH, 'Wright Patterson AFB, Aerospace Med. Res. Labs., Rept. MRL TDR 62-30 (May 1962), 17 p., Ref.: NASA TPA N62-15432. 24. BURGESS, D. S., A. STRASSER und J. GRUlILER: Diffuse Verbrennung ftiissiger Brennstoffe in offenen Be• haltem (in Englisch). Fire Res. Abstr. Rev. 3,177-92 (1961), Ref.: CZ1962, 14978. 25. BURNS: The Analysis of Red Fuming Nitric Aeid II: Determination of Water by the Karl-Fischer-Titra- tion, CIT JPL Progr. Rept. 20-344 (Jan. 1958), 8 p. 26. BREDEMANN. G.: Biochemic und Physiologie des Flnors, Akademie-Verlag, Berlin 1955. 27. BILTZ. W., W. FISCHER und E. WUNNENBERG: Z. anorg. Chem. 193, 351 (1930). 28. BOCK, H.: Z. anorg. allg. Chem. 293, 264-73 (1958). 29. BARRICK, L. D., G. W. DRAKE, and H. L. LOCHTE: J. Am. Chcm. Soc. 08,160 (1936). 30. BARRERE, M., A. JAUMOTTE, B. FRAEI.JS DE VEUBEKE und J. VANDENKERCKHOVE: Raketenantriebe, Elsevier Pub!. Corp., Amsterdam 19tH. 31. BYRKIT. G. D., and G. A. MICHALEK: Ind. Engng. Chem. 42, 1862-75 (1950). 32. BOWEN, E. J., and A. W. BIRLEY: Trans. Farad. Soc. 47, 580-3 (1951). 33. BELTRAMI, R T., and E. R. BISSEL: J. Am. Chern. Soc. 78,2467-8 (1956). 34. BROIHAN, F.: Zentr. Arbeitsmedizin u. Arbeitsschutz 7, 62-6 (1957). 35. BOOMAN, K., G. W. ELVERUM, and D. M. MASON: J. Phys. Chem. 09, 516-9 (1955). 36. BERL, E., und H. H. SAENGER: Monatshefte f. Chemie 03-04, 1036-56 (1929). 37. BURTON, J. M.: US Pat. 2994190 (1 Aug. 1961), 1nh.: Phillips Petrol. Co., Ref.: CA 55,22826. 38. BIONDOLILLO, S.: Handling and Storability of Liquid Rocket Propellants, Bell Aircraft Co., Buffalo, N. Y., Contract NOrd 13947, Part I Rept. 989-019 (April 1955) 9 p., AD 86412, Part II Rept. 02-989-011 (June 1955) AD 86330, Part III Rept. 02-989-010 (July 1955) 7 p .. AD 86329, Part IV Rept. 02-989-012 (Sept. 1955) 14 p., AD 86411. 39. BARTH-WEHRENALP, G.: J. Inorg. Nuc!. Chcm. 2, 266 (1956). 40. BOVEE, H. H., A. S. GORAl, and J. B. PLATE: Air Pollution from Rocket Exhaust Products, Proceed. 130th Am. Chem. Soc. Meeting, Sept. 16-21, 1956. 720 Literaturverzeichnis B

41. BYERS, D. H., and B. E. SALTZMAN: Toxicity of N02/03-Mixtures and N 20 5, Proceedings 130th Am. Chern. Soc. Meeting, Sept. 16-21, 1956. 42. BASYROV, Z. B., und A. V. PANKRATOV: Explosionsempfindlichkeit von Ozon-Sauerstoff-Losungen gegen DruckstoBe (in Russisch), Chimitschesskaja Promyschlennosst 1962, 174-5, Ref.: CA 07, 6199d (1962), English Translation AFSC-FTD-TT-62-1460, AD 295454, N64-11153. 43. BRABETS, R. 1., and J. M. McDoNOUGH: J. Chern. Phys. 27, 880-2 (1957). 44. BRABETS, R. 1., and T. E. WATERMAN: J. Chern. Phys. 28, 1212-4 (1958). 45. BERLAD, A. L.: Comb. and Flame 0,301-2 (1961), vg1. auch dort S. 389. 46. BROWN, C., A. W. BERGER, and C. K. HERSH: J. Chern. Phys. 23, 1340-3 (1955). 47. BROWN, C., A. W. BERGER, and C. K. HERSH: J. Chern. Phys. 22, 1151-2 (1954). 48. BROWN, C., and K.D. FRANSON: J. Chern. Phys. 21, 917-9 (1953). 49. BALY, E. C. C., and F. G. DONNAN: J. Chern. Soc. [Lond.] 81, 907 (1902). 50. BROWN, C., C. K. HERSH, and A. W. BERGER: J. Chern. Phys. 23, 103-8 (1955). 51. BRAGG, S. L.: ARS J. 29, 672-4 (1959). 52. BREWER, J.: Thermodynamic Data on Oxygen and Nitrogen, Wright Patterson AFB and Air Products and Chemical Inc., Allentown, Pa. (Sept. 1961), 162 p., 239 references (!), Ref.: NASA TPA N62- 17364. 53. BLEYLE, G. A., R. B. HINCKLEY, and C. L. JEWETT: An Air-transportable LOX-Generator, Jet Prop. 24,297-301 (1954) und ARS Preprint 90-53. 54. BEEBE, J. L.: Liquid Oxygen Requirement Estimation for Complex Test Programs, ARS Preprint 630-58 (1958). 55. BECCO Chemical Division, Food Machinery and Chern. Corp., Buffalo, N. Y.: Hydrogen Peroxide (1955)- 20 p., Concentrated Hydrogen Peroxide, Bulletin No. 46 (Nov. 1958), 12 p., Becco Hydrogen Per• oxide 98%, Bulletin No. 70,8 p., Analysis of Hydrogen Peroxide, Bulletin No. 59, Materials Com, patibility, Bulletin No. 104, 55 p., High Strength H 20 2 Monopropellant and BipropeUant Per• formance Data Bulletin No. 107, 50 p. 56. BELLINGER, T. F.: Ind. Engng. Chern. 38, 160-9, 310-20, 627 -36 (1946). 57. BLOOM, R., and N. J. BRUNSVOLD: Chern. Engng. Progr. 03, 541-7 (Nov. 1957). 58. BLOOM, R., N. S. DAVIS, and S. D. LEVINE: J. ARS 20,3-17 (1950) und ARS-Preprint 6-49 A. 59. BRINKLEY, S. R., R. W. SMITH, and H. E. EDWARDS: Performance Calculations of Hydrogen Peroxideasa Monopropellant, US Bur. of Mines, Reports PX 3-107/13 and PX 3-107/14 (June 1953 and June 1954), AD 17869, AD 15405. 60. BLACK, R. P. S.: Chemical Factors in the Use and Handling of Electronic Grade Hydrogen Peroxide, Am. Soc. Testing Mat., ASTM Paper 14 (Oct. 1962), 14 p., Ref.: NASA TPA N 62-17687. 61. Bureau of Aeronautics, Dept. of the Navy: Handbook for the Field Handling of Concentrated Hydrogen Peroxide, Nav Aer 06-25-501, revised Ed. (15 Jan. 1957). 62. BLOOM, R.: Jet Prop. 27, 666 (1957). 63. BOWERSOCK, D. C., P. G. CAMBELL, and R. C. REID: Adv. Cryog. Engng. 4, 443-53 (1960). 64. BLANCHARD, R. L., and A. E. SHERBURNE: AIAA-J. 1, 2590-6 (1963). 65. BRAUN, R. J., et a1.: Analysis of Liquid Hydrogen Storage Problems for Unmanned Nuclear Powered Mars Vehicles, NASA TN D-587 (Jan. 1962),65 p. 66. BAILEY, B. M., D. C. BENEDICT, et al.: Storage, Transfer and Servicing Equipment for Liquid Hydro• gen, A. D. Little Inc., Rept. W ADC TR 59-386, Contract AF 33 (616)5641, 237 refs., 772 p., unclassif., AD 231635. 67. BAILEY, A. B., R. G. CRUDDACE, and B. W. A. RICKETSON: J. BIS 18, 203-24, (1961/62). 68. BISBEE, W. R., et a1.: The Heat of Formation of Oxygen Difluoride, Am. Chern. Soc., Symposium on Advanced Propellant Chemistry, Preprint of Papers, Vol. 9, No.1, p. 245-50. ACS Series Vol. 54. 69. BOWERSOCK, D. C., and R. C. REID: Adv. Cryog. Engng. 6, 261-71 (1961). 70. Bosco, G. B., and T. A. CARTER: Adv. Cryog. Engng. 2, 64-70 (1960). 71. BEIGHLEY, C. M., and L. E. DEAN: Jet Prop. 24, 180-6 (1954) und ARS-Preprint 114-53. 72. BROWN, P. E., J. M. CRABTREE, and J. F. DUNCAN: J. Inorg. and Nuclear Chern. 1, 202-12 (1955). 73. BROWN, M. H.: Resistance of Materials to Fluorine and Hydrofluoric Acid, US AEC Oak Ridge, Tenn., MDDC-144. 74. BAKER, B. B., and J. D. MORRISON: Anal. Chern. 27,1306-7 (1955). 75. BANCHERO, J. T., G. E. BAKER, and R. H. BOLL: Heat Transfer Characteristics of Boiling Oxygen, Fluo• rine and Hydrazine; Univ. of Michigan, Ann Arbor, Engng. Res. Inst., Rept. 51-11, Final Rept. Part A, ATI 155019 (Nov. 1951), 268 p. 76. BARTZ, D. R., M. B. NOEL, and A. F. GRANT: Evaluation of Hydrazine as a Regenerative Coolant, JPL Publicat. 111 (Oct. 15, 1957) (Confidential). 77. BLACK, 1. A., A.A. FOWLE, and P. E. GLASER: Adv. Cryog. Engng. 0,181-8 (1960). 78. BURGESON, D. A.: Results of Flowmeter Calibration in Liquid Hydrogen, Abstract in: Adv. Cryog. Engng. 0, 307 (1960). 79. BRONSON, J.C., et a1.: Adv. Cryog. Engng. 7, 198-205 (1962). Literaturverzeichnis B 721

80. BALDRIDGE, J. H.: Development of Rubber-like Materials for Applications Involving Contact With Liquid Rocket Propellants, Wright Air Dev. Center WADC Tech. Rept. 57-651, Contract AF 33(616} 3951 (Dec. 1957), 39 p., AD 142205. 81. BAKER, D. 1.: Mollier Diagram for the H2/0.-System and Experimental Results of Tests on a Rocket Motor of 500 Pound Thrust, CIT-JPL Rept. 20-127 (May 1959), 109 p., OTS-PB Rept. 153791; Ref.: CA08, 12359 (1963). 82. BAKER, L., and F. W. STEFFEN: Screaming Tendency of the Gaseous Hydrogen-Liquid Oxygen Propellant Combination, NACA RM E 58-E 09 (Sept. 1958) 24 p. 83. BROCHER: Bull. tech. Suisse rom. 84: 9, 161-6 (1958). 84. BAKER, D. 1.: Experimental Investigation of Gaseous Hydrogen and Liquid Oxygen in a Motor of 100 Pound Thrust, CIT·JPL Rept. 4-48, Contract W-04-200-0RD-455 (14 Jan. 1949). 85. BAKER, D. 1.: Regenerative Cooling Tests for Rocket Motors Using Liquid Hydrogen and Liquid Oxygen, CIT·JPL Rept. 4-53, Contract W 04-200-0RD-455 (11 Aug. 1949). 86. BROKAW, R. S., and R.N. PEASE: J. Am. Chern. Soc. 70,1454-57 (1953). 87. BUSEMANN, A.: R-Gerat mit SauerstofI", Schriften d. dt. Akad. d. Luftfahrtf. 1071-43 (1943) S. 127 -43. 88. BAKER, D.J.: Jet Prop. 20, 217-26, 234 (1955). 89. BEETON, A. B. P.: Calculated Performance of Ethanol-Water Mixtures as Rocket Fuels with LOX, Gr. Brit. Aeron. Res. Council, Rept. and Memo. 2816 (1953) 8 p., Ref. in Fuel Abstr. 16: 4, 109 (1954) und Index aeron. 10, 100 (March 1954). 90. BAUER, W. H., 1\1. S. GOLDSTEIN, and S. E. \VIBERLEY: The Reaction of Diborane and Oxygen under Explosive and Pre-explosive Conditions, in: Liquid Hockets and Propellants, ed. by L. E. BOLLINGER et aI., Academic Press, New York (1960), p. 327 -49. 91. BREISACHER, P., D. DEMBROW, and \V. G. REHL: 7th Symp. on Comb., Butterworths Scientific Publi· cations, London (1959), p. 894-- 902. 92. BERL, W. G., and W. RENICH: The Combustion of Boron Hydrides, Applied Physics Lab., Johns Hopkins Univ., Silver Spring, Rept. Xo. CM-942, Contract NOrd-7a86 (July 1958) 53 p., AD 207027, auch erschienen in Symp. on Thermal Properties, Purdue Univ. 1959, ASME, McGraw Hill Book Co., New York (1959). p. 236-50. 93. BOLLINGEH, L. E., and R. EDSE: Liquid Nitric Oxide as a Rocket Oxidiz<'c, Ohio State Univ., Columbus, Ohio, Wright Air Dev. Center, Tech. Rept. 59-12, USDC-OTS, PB Rept. 161300 (1959). 22 p., Ref.: CA 55, 20434. 94. BAMFORD, D. A., and C. H. BA~IFORD: Trans. Farad. Soc. 36,1036-42 (1940). 95. BAKER, L.: Ignition Delay with Rapidly Mixed Liquid Reactants, Illinois Inst. Technol., Chicago. Tech. Rept. No.7. Contract N 7-onr-329 13 (Aug. 1954), 238 p., AD 40233. 96. BOLLINGER, L. E., .J. A. LAUGHREY, and R. EDSE: ARS-J. 32, 81-2 (1962). 97. BELLES, F. E.: 7th Symp. on Combustion, Butterworths Scientific Publieations, London (1959), p. 745-51. 98. BOLLINGER, L. E .. J. A. LAUGHREY, and R. EDSE : ARS-J. 32, 428-30 (1962). 99. BRIDGFORTH, R.1\I.: L'S Pat. 3112608 (3.11.1960/3.12.1963), Inh.: Rocket Res. Corp., Ref.: CA 60, 5269d (1964). 100. BRlDGFORTH, R. M.: US Pat. 3112609 (12.12. 1960/3. 12. 1963) Inh.: Rocket Rcs. Corp., Ref.: CA 60, 526ge (1964). 101. BARURA, A. K., et al.: J. Chern. Phys. 41, 347 -9 (1964). 102. BUCKNELL, R. L.: Adv. Cryog. Engng. 8, 360-70 (1963). 103. BAKER, L.: A Study of the Combustion Rates of Hydrocarbon Fuels with Red Fuming Nitric Acid in a Small Rocket Engine, NACA RM E .'58-D 03a (Aug. 1958) 42 p. 104. BOYER, M. H., and P. E. FRIEBERTSHAUSER: Comb. and }<'lame 1, 264-80 (1957), vgl. auch ARS Prl' print 371·!)(i. 105. BAKER, L.: Chemical and Physical Factors Affecting Combustion in Fuel-Nitric Acid Systems, NACA RM E 58-D 03 (July 1958), 20 p. 106. BODEN: An Investigation of the WFNA-Furfurylalcohol Rocket Propellant, CIT-JPL Progr. Hept. 4-67 (May 1948), 31 p. 107. BRINKLEY, S. R., R. \V. S~UTH, et al.: Thermodynamics of the Combustion Products of Ammonia with Nitric Acid, Bur. of Mines, Rept. PX 3-107/11, Contract Nonr 97-50 (;\Iay 1953), 105 p .. AD 10884, see also AD 10883. 108. BOLLINGER, L. E., and R. EDSE: Investigation of the Premixed Jet Fuel/RFNA Rocket Propellant System, Ohio State Univ., Columbus, Final Rept. on Liquid Rocket Engine Techno!., Contract AF 33(616)2067, WADC TR 57 -407 (Oct. 1957), 25 p., AD 142108. 109. BERNARD, M. L. J.: Compt. rend. de Acad. Sci. Paris 250/111, 4361-3 (1960). 110. BURTON, J.M., and H.M.Fox: US Pat. 2993335 (13 Sept. 1956), Inh.: Phillips Petrol. Co., Ref.: CA56 3714d (1962). 111. BURTON, J. M.: US Pat. 2769304 (6 Nov. 1956), Inh.: Phillips Petrol. Co., Ref.: CAOl, 3969g. 112. BARR, W.J., and E. J. WILSON: J. Chern. Phys. 19, 470-3 (April 1951). 113. BROATCH, J. D.: Fuel 29, 106-9 (1950). 114. BERNARD, M. L.: ARS-J. 32, 956 (1962).

Dudicu-Damm-Schmiu.t, ltakdentrcib,toffc 46 722 Literaturverzeichnis B

115. BERNARD, M. L.: Nouveaux initiateurs de combustion, leur utilisation en tuyere, Franz. Pat. 1231606 (8. 1. 1951/19.4. 1960). 116. BUSCHULTE, W.: Fragen der Lithergolantriebe, WGL-Jahrbuch 1961, Verlag Vieweg & Sohn, Braunschweig (1962), S. 414-7. 117. BROADWELL, J. E., and J. R. SELLARS: Solution of Laminar Flame Problems by Use of the Analog Com• puter, Engng. Res. Inst., Univ. Mich., Ann Arbor, WADC Tech. Rept. 56-290 (June 1956), 33 p., AD 110477. 118. BENDERSKY, C.: Hydrogen-Oxygen Catalytic Ignition, Rocketdyne Rept. R 63-9 (Jan. 1963), 95 p., N 64-21901. 119. BREITWIESER, R., and J. W. USELLER: Performance of Pentaborane, Pentaborane-JP 4-Fuel Mixtures and Trimethylborate Azeotrope Fuel in A Full-Scale Turbojet E'ngine, NACA RM E 56-G 19 (20 Nov. 1956), 83 p., N 63-12542. 120. BARTEL, H. R., and W. D. RANNIE: Solid Fuel Combustion as Applied to Ramjets, CIT JPL Progr. Rept. 3-12 (27 Sept. 1946). 121. BARRERE, M.: Les Recherches dans Ie Domaine de la Propulsion Chimique, ONERA TP-141 (1964). 122. BARRERE, M., et A. MOUTET: La Propulsion par Fusees Hybrides, O~ERA TP-61 (1963). 123. BELLINGER, F., et al.: Ind. Engng. Chem. 40,1320-3 (1948). 124. BELLINGER, F., et al.: Ind. Engng. Chem. 40,1324-31 (1948). 125. BURG, A. B.: J. Am. Chem. Soc. 79, 2129-32 (1957). 126. BRAMAN, R. S., et al.: Anal. Chem. 32,1258-62 (1960). 127. BECKMANN, R. B.: Catalytic Pyrolysis of Diborane, Carnegie Inst. Techn., Pittsburgh, Pa., Rept. CCC- 1024-TR-272 (9 Dec. 1957), 18 p., AD 209020. 128. BOYNTON, C. F., D. E. TERPKO, and J. R. LUDWIG: Physical Properties of Liquid Pentaborane, Callery Chemical Co., Rept. Contract No a(s) 58-454-d (Sept. 1961),33 p., AD 267076. 129. BULTER, G. W., et al.: Vapor Phase Hydrolysis of Pentaborane-9, Oregon State Univ., Corvallis, Contract Da 18108, AMRL TDR 63-129 (Dec. 1963), 14 p., AD 431220. 130. BADEN, H. C., W. H. BAUER, and S. E. WIBERLEY: J. Phys. Chem. 62, 331-4 (1958). 131. BERL, W. G., et al.: Comb. and Flame 1, 420-30 (1957). 132. BERL, W. G., et a!.: J. Chem. Phys. 25, 797 (1956). 133. BADEN, H. C., S. E. WIBERLEY, and W. H. BAUER: J. Phys. Chem. 59, 287 -8 (1955). 134. BAUER, W. H.: J. Am. Chem. Soc. 80, 294-8 (1957). 135. BAKER, N. L.: Missiles and Rockets 1957: 9, 157-8, 161-2 (Sept. 1957). 136. BAUER, W. H.: The Oxidation of Diethyldiborane, AIAA-Preprint 63-501 (1963). 137. BLUNDELL, R. W.: Brit. Pat. 878564 (27.3.1958/4.10.1961), Ref.: CZ 1963, 20242. 138. BLAY, N. J., J. WILLIAMS, and R. L. WILLIAMS: J. Chem. Soc. 1960, 424-9 (1960). 139. BLAY, N. J., J. WILLIAMS, and R. L. WILLIAMS: J. Chem. Soc. 1960,429-33 (1960). 140. BRUEHL, H.: DB Pat. 1053376 (19.3.1959), Inh.: Heyl & Co., Berlin, Ref.: CA 00, 3984b (1961). 141. BERL, W. G., and D. DEMBROW: Nature 170. 367 (30. Aug. 1952). 142. BAUERLE, G. L., R. C. AHLERT, and J. SILVERMAN: US Pat. 3127735 (5.7.1960/7.4.1964), Inh.: North Am. Aviation, Ref.: CA 61, 5444f (1964). 143. BERL, "V. G., and \V. RENICH: The Combustion of Boron Hydrides, in: Touloukian: Thermodynamie and Transport Properties of Gases, Liquids and Solids, McGraw Hill, New York (1959), p. 236-50. 144. BARRERE, M., and A. MouTET: 5th Symp. on Combustion, Reinhold Pub!. Corp., New York (1955), p.170-81. 145. BUMGARDNER, C. L.: Tetrahedron Letters 1964: 48, 3683-8 (1964). 146. BRENTARI, E. G., and R. V. SMITH: Internat. Adv. Cryog. Engng. 10 MU, 325-41 (1965). 147. BLACKWELL, J. P.: US Pat. 3113836 (12.8.1959/10.12.1963), Inh.: Phillips Petrol. Co., Ref.: CA 60, 9093f (1964). 148. BLACKWELL, J. P., and R. C. Doss: US Pat. 3125852 (12.8.1959/24.3.1964), Inh.: Phillips Petrol. Co., Ref.: CA 61, 4141 h (1964). 149. liENS: Oxidation of 1.1-Dialkylhydrazines; Chromatographic and UV-Analysis of Tetraalkyitetrazclll's, NAVORD Rept. 5879, NOTS-2016 (June 1958) 34 p. 150. BOWEN, J. R.: Steady Detonations in Ozone-Oxygen Mixtures, Univ. of Calif., Berkeley, Univ. Microfilms (Ann Arbor, Mich.) No. 63-5486, 206 p., Diss. Abstr. 24, 1106-7 (1963), Ref.: CA 60, 11839 (1964) 151. BUTLER, E. M., and M. M. FEIN: US Pat. 3130019 (27.11. 1957/21. 4.1964), Inh.: Thiokol C. C., Ref.: CA 61, 528b (1964). 152. BURTON, J. T. A., and H. ZIEBLAND: The Thermal Conductivity of Liquid and Gaseous Oxygen, Gt. Brit., Explosives Res. and Dev. Establ., Rept. No. 2/R/56, Rept. No. ASTIA 21-56 (Jan. 1956) AD 90759, 15 p. 153. BASSYROW, S. B.: Empfindlichkeit von Gemischen organischer Stoffe mit fliissigem Sauerstoff gegeniiber ImpulsstoBen (in Russisch), Kisslorod (Moskau) 12: 6, 13-23 (1959), Ref.: CZ 1964: 12, No. 0377. 154. BECCO: Shipping Drums and Drum Vents for Concentrated Hydrogen Peroxide, Buffalo Electro-Chemi• cal Co., Inc., Final Rept. AD 50040 Contract N 140s-46174B, Supplement (31 Dec. 1954), 8 p., AD 65733. Literaturverzeichnis B 723

155. BARTLETT, W. \Y.: Conditions for Self-Heating of Exothermally Decomposing Liquids, e. g. Hydrogen Peroxide, Naval Underwater Ordnance Test Stn., Newport, R. I., Tech. Memo 227 (Jan. 1959), 12 p., AD 213497. 156. BEATTIE, 1. R.: Dinitrogen Trioxido; Progress in Inorg. Chern. 5, 1-26 (1963), Interscience Publ., New York 1963 157. BUSCAGLIA, R., and S. \V ALLACK: Feasibility Study of a Multipurpose IR Propcllant Detector, Patterson Moos Research Div., Leesona Corp., Jamaica, N. Y., Rept. AST TR 61-382 (Aug. 1961), 52 p., AD 267159, Ref.: CA 61, 525f (1964). 158. BACH~IAIER, F.: Untersuchungen am Systcm DistickstofftetroxydfTetranitromethan, DVL-Bericht DLR FB 64-29 (1964), 28 S., Ref.: CA 63, 12961 b. 159. BESSEY, lVI. J., and H. G. PSYRAS: Fuming Nitric Acid Decontamination Equipment, Army Chern. Center, Md., Chem. Warfare Labs., Rept. CWLR-2055 (11 Oct. 1956),44 p., AD 112233. 160. BARRET, W. J., and L. WmTE: Stildies on Stainless Steel and Aluminum Sludges From ]\I;itric Acid Con• tainers, Southern Res. Inst., Birmingham, Ala., Final Summary Rept., Contract AF 18(600)53 (21 Aug. 1953), declassified 15 June 1954, 4 p., AD 18929. 161. BUMP, T. R., et al.: Jet Prop. 25, 170-80 (1955). 162. Berufsgenossenschaft der chemischen Industrie: Richtlinien zur V crhiitung von Gefahren durch elektro• statische Aufladungen, Richtl. Nr. 4, Verlag Chemic, Weinheim(Bergstr. 1960. 163. BRECKENRIDGE, H. L., and D. A. VAN GUNDY: Establishing Tank Design Criteria for Liquid Hydrogen Rockets, Vol. IV: Flight Simulation Tcst Program, Beech Aircr. Corp., Boulder, Colo., Final Rept. 8768, AFFTC TR 60-43, Vol. 4 (June 1963), 147 p., AD 408672. 164. BERL, W. G., and W. E. WILSON: ~ature (London) 191, 380 (1961), Ref.: CZ 1961, 16742. 165. BANAS, P. A., H. W. KRU_SE, and E. LIEBER: Solubility of Ammonia im Hydrazine. Naval Ordn. Test Station, Inyokern, China Lake, Calif., NAVORD Rept. 3337 (18 June 1954), 11 p., AD 48767. 166. BURNS, E. A., and E. A. LAWLER: Anal. Chcm. 35, 802-6 (1963). 167. BAILEY, B. M., D. C. BENEDICT, et al.: Handbook for Hydrogen Handling Equipment, 583 p., 226 referm• ecs (Febr. 1960), _-\D 235123. 168. BITTKER, D. A.: Comparison of Experimental and Kinetically Limited Theoretical Performance of the H 2(F2 System, NASA TN D-3607 (Aug. 1966), N66-34 652. 169. BECKETT, J. A., L. C. ROSE, and J. T. HAMRIK: US Pat. 3054252 (27. 11. 1957/18.9.1962), Inh.: Thompson Ramo Wooldridge Inc., Ohio. Ref.: CZ 1964: 21, 277, Ref. No. 2787. 170. BURRY, R. V., J. JORTNER, and J. K. ROS};MARY: ARS J. 31, (l09-13 (1961), ARS-Preprint 1123-60 (1960). 171. BURROWS, M. C.: Radiation Processes Related to OxygenfHydrogen-Combustion at High Pressures, NASA TM X-52023 (10th Symp. on Comb. 1964), N 64-20576. 172. BAILEY, T, E., and R. F. FEARN: Adv. Cryog. Engng. 9. 254-64 (1964). 173. BURGESON D. A., \Y. G. PESTALOZZI, and R. J. RICHARDS: Adv. Cryog. Engng. 9, 416-22 (1964). 174. BIRDSALL, C.1\I.. et al.: J. Chem. Phys. 23, 441-52 (1955). 175. BALL, J. J .. and D. E. MANN: Mdhane-Oxygen-Fluorine Flames; Spectroscopie and Calorimctrie i:->tudies, Wright Air Dev. Center, WADC Tech. Rept. 58-541 (Oct. 1958), 63 p., ASTIA AD 204802. 176. BURDEN, F. A., and J. H. BrRGOYNE: The Ignition and Flame Reaction of Ethylene Oxide, Proc. Roy. Soc. Lond. A 199,328-51 (Nov. 1949). 177. BELLER. H.: Ui:-> Pat. 30:11 348 (1. 5. 1958(24.4. 1962), lnh.: General and Film Co., Ref.: CA 57, 7i)10h. 178. BENSON, S. 'N.: J. Chem. Phys. 40,105-11 (1964). 179. BRAZINSKY, 1., and B. S. GOTTFRIED: Thel'modynamic Consistency of Solubility Data for the H 2-He Vapor-Liquid System, NASA TN D-1403 (Aug. 1962), 23 p. 180. BOYER, K. : Heat Transfer in Missiles and Space Operations, Institut Internat. du Froid, Cours sur I'Hydro- gene Liquide, Grenoble (Juin 1965). 181. BREZING, D.: AIAA J. 3, 1422-7 (1965). 182. BLACKMON, J. B.: J. of Spacecraft and Rockets 2, 391-8 (1965). 183. BARNETT, D.O., T. ,Yo WINSTEAD, and L. S. McREYNOLDS: Internat. Adv. Cryog. Engng. 10 M"V, 314-24 (1965). 184. BARBARAS, G. D., et al.: J. Am. Chem. Sot'. 73, 4585-90 (1951). 185. BARRERE, 1\[, et A. );IOUTET (in Franz6sisch), XVI Internat. Astron. Congress, Paris 1963, No. 122, Office Nat. d'Etudcs et de Recherches Aerospatiales. 186. BLACKMAN, A. W., and D. K. KUEHL: ARS-J. 31,1265-72 (1961). 187. BARTOCHA, B., and F. E. BRINKMAN: Guidelines for the Operation of a Be-Research Facility, NAVWEPS Rept. No. 7198 (Sept. 1963). 188. BURG, A. B., and H. 1. i:->CHLESINGER: J. Amer. Chem. Soc. 62, 3425-35 (1940). 189. BACRMAIER, F., und J. JI~!ENEZ: Untersuchungen am System Hydrazin(Ammoniak, DLR-FB 67-21 (1967). 190. BACRMAIER, F., und J. JIMENEZ: Untersuchungen am System Hydrazin(Hydrazinnitrat, DLR FB-66-66-76 (1966).

46* 724 Literaturverzeichnis C

191. BURNS, E. A.: Analysis of TITAN II Fuel by the Acetic Anhydride Method, a Critical Review, Space Techn. Labs., Redondo Beach, Calif. (Aug. 1963) 11 p., STL-TR-6110-8651-RU-000, AD 452644, N 65-17125. 192. BROCKAW, R. S.: J. Phys. Chern. 69, 2488-9 (July 1965) (I) und J. Phys. Chern. 69, 2808-9 (Aug. 1965} (II). 193. BUCHANAN, H. J., and F. M. BUGG: Orbital Investigation of Propellant Dynamics in a Large Rocket Booster, NASA TN D-3968 (May 1967) 21 p., N67-26546. 194. BUCHNER und V. NIECIECKI: WGLR Sitzg. d. Fachausschusses "Treibstoffe" Trauen (Dez. 1964), DLR- Mitteilungen 65-10 (1965) 71 S. 195. BEGUM, G. M., W. H. FLETCHER, and D. F. SMITH: J. Chern. Phys. 42, 2236 (1965). 196. BATTINO, R., and H. L. CLEVER: Chern. Rev. 66, 395-463 (1966), 686 Refs. 197. BURWELL, W. G., V. J. SARLI, and T. F. ZUPNIK: Chern. Engng. Progr., Symposium Series 61 125-35 (1966), IAA Ref. A 66-39882. 198. BAILEY, T. E.: Low Mixture Ratio Fluorine/Hydrogen Propulsion System Investigation, AIAA Second Joint Propulsion Specialist Conf., Colorado Springs, June 13-17, 1966. 199. BAILEY, C. R.: A Preliminary Investigation of Oxidizer-Rich Oxygen-Hydrogen Combustion Charac• teristics. NASA TN D-3729 (Dec. 1966), 30 p., N 67-11812. 200. BURROWS, M. C.: Mixing and Reaction Studies of Hydrazine and Nitrogen Tetroxide Using Photographic and Spectral Techniques, AIAA Paper 67-107, NASA TM X-52244, N 67-11331. 201. BOST, J. L., A. CERA, and J. A. CABEAL: Gelled Fuel Compositions, US Pat. 3232801 (16. 10. 1962/1. 2. 1966), Aerojet-Gen. Corp., Ref.: CA 64,11021 (1966). 202. BELTRAN, M. R., and T. C. KOSVIC: Parametric Study of Combustion Instability in an MMH-NTO Liquid Rocket Engine, AIAA Paper 66-603. 203. Anonym: Experimental Auxiliary Rocket Engine, Bell Aerosystems Co., Final Rept. NAS 7-305 (5. Jan. 1966), NASA CR-76150, N 66-30398, CR-76155, N 66-30399. 204. BACHMEIER, F.: Raketentechnische Eigenschaften des Systems Hydrazin(Methylalkohol, D. L. R. Forsch. Ber. 68-05 (1968). 205. BOUGON, R., 1. CHATELET und R. PLURIEN: Bulletin de la Societe Chimique de France, Division de Chimie Physique et de Chimie Mineral. Seance du 13. Mai 1966. 206. BRUMAN, A. J.: Some Design Considerations, Large Expulsion Bladders for Nitrogen Tetroxide and Hydrazine, JPL-TR-32-862, NASA CR-70034 (15 Jan. 1966) 38 p., N66-16 746. 207. BRANSTETTER, J. B., and P. C. SETZE: Experimental Behavior of Pentaborane/Air Combustion Products During Expansion in a Convergent Divergent Nozzle, NACA RM E57-120 (Feb. 1958), Declassified N67-31730. 208. BRANSTETTER, J. R., W. B. KAUFMAN, and A. L. SMITH: Experimental Behavior of Combustion Products of HEF-2 and Air During Expansion in Exhaust Nozzles, NASA TM X-381 (Dec. 1960), Declassified N67-31 532. 209. BOORADY, F. A., and D. A. DOUGLASS: J. of Spacecraft and Rockets 5,22-30 (1968). 210. BOURGAREL, M. H., and M. P. SEGEL: Adv. Cryog. Engng. 12, 103-11 (1967). 211. BAUER, H. F., and D. F. SHEEHAN: Inorg. Chem. 6,1736-7 (1967). 212. BLEICH, A., and J. HERTZ: Adv. Cryog. Engng. 12, 762-70 (1967).

c 1. COLBURN, C. B., and A. KENNEDY: J. Am. Chem. Soc. 80, 5004 (1958). 2. COLBURN, C. B.: International Symposium on Fluorine Chemistry, p. 30, Univ. Birmingham, Edited by the Chern. Soc. London (1959). 3. Anonym: Oxygen Fluoride Attracts Rocketeers, Chern. Engng. 64 (12. Jan. 1959). 4. CADY, G. H.: J. Am. Chem. Soc. 56, 2635-7 (1934). 5. Anonym: Chem. Industries 57, 1084 (1954). 6. CLARK, H. C.: Chern. Reviews 58,869-94 (1958). 7. CHRISTE, K. 0., and A. E. PAVLATH: High Energy Oxidizers, Stauffer Chem. Co., Richmond, Calif., Quart. Techn. Summ. Rept. 1 Febr. - 1 May 1963 (1 May 1963), 12 p., Contract Nonr 401900 Proj. NR 093035. 8. CULLIS, C. F., and C. B. BADDIEL: J. Chern. Soc. London 1961, 5449. 9. CIEPLUCH, C. C., H. ALLEN, and E. A. FLETCHER: ARS-J. 31, 514-8 (1961). 10. CLEAVER, C. S.: US Pat. 2958634 (1 Nov., 1960), Inh.: DuPont de Nemours & Co., Ref.: CA 55, 6214g (1961). 11. COLBURN, C. B., F. A. JOHNSON, A. KENNEDY, et al.: J. Am. Chem. Soc. 81, 6397-8 (1959). 12. COFFIN, K. P., and C. O'NEAL: Exp~rim9ntal Thermal Conductivities of the Nz0 4 ~ NOz-System, NACA TN 4209 (1958), 22 p. 13. COLE, J-. G.: The Nitrous Oxides as Rocket Fuel Oxidants, Including the Theoretical Performance of Propallant Systems Employing Nitrogen Tetroxide, JPL Progr. Rept. 9-23 (Oct. 1948), 17 p. (Declassified by JPL Publ. 38, 1 March 1955). Literaturverzeichnis C 725

14. CRITTENDEN and GONIGLE: Aero Digest 71, 60-4 (July 1955). 15. CORDES, H. F., and C. W. TAIT: Anal. Chern. 29, 485-7 (1957). 16. COHN, J. G. E.: Franz. Pat. 1262846 (4.7.60/24.4.61) und: DBP 1197281 (Am. Prior. 16.7.1959/ 22. 7. 1965), Engelhard Ind. Inc., Ref.: CA 63, 12963e. 17. CLARK, J. D.: A Field Analysis for White Fuming and Anhydrous Nitric Acid, Naval Air Rocket Test Station NARTS Rept. 23 (Sept. 1952). 18. CLARK, J. D.: Analytical Procedures for Rocket Propellants, Naval Air Rocket Test Station NARTS Rept. 20 (June 1952). 19. CLARK, J. D.: Analytical Procedures for Rocket Propellants (Mixed Acid), Naval Air Rocket Test Station NARTS Rept. 24 (Sept. 1952). 20. CLARK, J. D.: An Analytical Procedure for Mixed Acid, AR.8 Preprint 119-53 (1953). 21. CORDES, H. F., N. R. FETTER, and J. A. HAPPE: J. Am. Chern. Soc. 80, 4802-8 (1958). 22. CARTER and ELLIS: Brit. Pat. 792195 (19 March 1958), Inh.: Genatosan Ltd. 23. CLARK, C. C.: Hydrazine, Mathieson Chemical Corp., Baltimore 1953. 24. CARPENTER, L. G., et al.: Hydrazine Process Development, Aerojet-Gen. Nucleonics, Interim Tech. Rept. No.3 (Jan. 1962), 198 p., AD 272438. 25. CUSACK, J. H., et al.: Hydrazine Process Development, Aerojet-Gen. Nucleonics, Rept. No.2 (Nov. 1961), 172 p., ASD-TR-7-840 A, AD 266689. 26. CLARK, J. D.: Analytical Procedures for Rocket Propellants IV: Hydrazine and Mixed Acid, Naval Air Rocket Test Station NARTS Rept. No.9 (May 1951), 9 p. 27. CLASS, J. B., et al.: J. Am. Chern. Soc. 70, 2937 -9 (1953). 28. CORCORAN, W. H., H. H. REAMER, and B. H. SAGE: Volumetric and Phase Behavior of the HNOa/N02- System, Ind. Engng. Chern. 46,2541-6 (1954), dasselbe auch als: JPL Progr. Rept. 20-173 (10 Aug. 1953), Erganzende Unterlagen: Supplementary Material, American Documentation Inst., Washington D. C., Doc. 4350. 29. CARPENTER, C. D., and A. LEHRMAN: Trans. Am. Inst. Chern. Engrs. 17, 35-73, (1925). 30. COLE, V. V., D. C. HILL, and A. H. OIKEMUS: Proc. Soc. Exper. BioI. and Med. 84, 661-2 (1953). 31. COMSTOCK, C. C., L. LAWSON, E. A. GREENE, and F. W. OBERST: Inhalation Toxicity of Hydrazine Vapor, Army Chern. Center, Maryland, Chern. Corps Med. Lab., Res. Rept. MLRR 253 (1954). 32. COMSTOCK, C. C., et al.: AMA Arch. Ind. Hyg. 10, 476 (1954). 33. CLARK. J. D., and J. R. SMITH: Anal. Chern. 33, 1186 (1961). 34. CRAGOE, C. S., C. H. MEYERS, and C. S. TAYLOR: J. Am. Chern. Soc. 42, 206-29 (1920). 35. CAMPBELL, E. S., and C. NUDELMAN: Reaction Kinetics, Thermodynamics and Transport Properties in the Ozone-Oxygen-System, AFOSR TN-60-502, Dept. of Chern., New York Univ., New York (1961). 36. COOK, G. A., et al.: Ind. Engng. Chern. 48,736-41 (1956). 37. CORELLI, M. R.: Die Erniedrigung des Schmelzpunktes (System Tetranitromethan: Distickstofftetroxyd), Ber.4 IAF-KongreLl Zurich 1953, S. 161-2, vgl. auch: CORELLI, M. R.: L'Abbassamento del Punto di Congelamento del Tetranitrometano con Mezzi Chimici, e Nota Preliminare suI Sistema: Tetra• nitrometano-Perossido d'Azoto, L'Aerotecnica 33, No.6, 391-2 (1953). 38. COLE, V. V., D. L. HILL, and A. H. OIKEMUS: Arch. Ind. Hyg. and Occ. Health 10,158-61 (1954). 39. CHAO, G. T. Y.: ARS J. 29, 199-203 (1959). 40. CASTRON: Problems Encountered in the Use of LOX, SAE Prepr. 238 (Oct. 1957),4 p. 41. CLAUDE, G.: Brit. Pat. 887967 (26.9.1960/24.1. 1962) (franz. Prior. v. 6.10.1959), Ref.: CZ 1964: 4,211; No. 1988. 42. CLEAVER, A. V.: J. BIS 14, 159-64 (1955). 43. CLEAVER, A. V.: Handling Hydrogen Peroxide, De Havilland Gazette 1952,20-1 (Febr. 1952). 44. CARTER, T. A., and C. R. CRUSAN: Adv. Cryogenic Engng. 4, 218-30 (1960). 45. CADOGAN, W. P., and L. W. KINNEY: Ind. Engng. Chern. 48: 7, 7 A-lOA (July 1956). 46. COHEN, A. D., and L. S. BEERS: Astronautics and Aerospace Engng. 1: 7, 98-105 (1963). 47. CASUTT, L. H., F. E. MADDOCKS, and W. A. SAWYER: A Study of the Hazards in Storage and Handling of Liquid Hydrogen; USAF Contract AF 18 (600) 1687, A. D. Little Inc., Tech. Report (1959). 48. CASUTT, L. H., F. E. MADDOCKS, and W. A. SAWYER: Safety Aspects in the Handling and Storagc of Liquid Hydrogen, in: Proc. of the Propellant Thprmodyn. and Handling Conf.. Ohio StatE' Univ., Columbus 1959 (1960), p. 63-74. 49. CAINE, G., L. SCHAFER, and D. BURGESON: Adv. Cryog. Engng. 4, 241-5 (1960). 50. COPLEN, H. L.: J. ARS 22,309-22 (1952) und ARS-Preprint 52-52 (1952). 51. CLEAVER, A. V.: J. BIS 18,189-92 (1961-62). 52. COAR, R. J., and C. H. KING: Astronautics 5: 3, 26-7, 76-8 (1960). 53. CONELLY, J. G., and B. R. ETHERIDGE: Establishing Proven Design Criteria for Cryogenic Boost Tanks, Beech Aircraft Res. and Dev. Inc., Boulder, Colo., Quart. Progr. Rept. 9 (Jan. 1962), 67 p., Contract AF 33(616)5154, Proj. 3084, AD 270836. 54. Chemical Week 83,75 (1958). 55. CLAUSSEN, W. H.: J. Am. Chern. Soc. 56, 614-5 (1934). 726 Literaturverzeichnis C

56. COLE, L. G., M. FARBER, and G. W. ELVERUM: J. Chern. Phys. 20, 586 (1952). 57. CADY, G. H.: J. Am. Chern. Soc. 57, 246 (1935). 58. COLBURN, C. B., and F. A. JOHNSON: J. Chern. Phys. 33,1869-70 (1960). 59. CHERNICK, C. L., et al.: Science 138, 136 -8 (1962). 60. CLAASSEN, H. H., J. G. MAnN, und C. L. CHERNICK: Angew. Chemie 75, 801 (1963).

61. Anonym: Rare Gas Studies Lead to XeF6 , Chern. and Engng. News 41: 5, 36-9 (4 Febr. 1963). 62. CLAASSEN, H. H., H. SELIG, and J. G. MALM: J. Am. Chern. Soc. 84, 3593 (1962). 63. Callery Chemical Co., Propellant Performance Data, Callery Chemical Co. (1961), 48 p. 64. Chemiker-Kalender, herausg. v. H. V. V. VOGEL, Springer-Verlag, Berlin-Gottingen-Heidelberg 1956. 65. CURME, G. 0.: Glycols, Reinhold Publ. Corp., New York 1953, ACS Monograph Series Vol. 114, p. 88ff. 66. CROCCO, L.: Jet Propulsion 27,1266-7 (1957). 67. CROCCO, L., 1. GLASSMAN, and 1. E. SMITH: J. Chem. Phys. 31, 506 (1959). 68. COURTNEY, W. G., W. J. CLARK, and C. M. SLOUGH: ARS·J. 32, 1530-5 (1962). 69. CROCCO, L., 1. GLASSMAN, and 1. E. SMITH: Kinetics and Mechanism of Ethylene Oxide Decomposition at High Temperatures, Princeton Univ., Dept. Aeron. Engng., Rept. 416, AFOSR-TN-58-273 (April 1958), 13 p., AD 154174. 70. CASSUTT, L. H., F. E. MADDOCKS, and W. A. SAWYER: Adv. Cryog. Engng. 5, 55-61 (1960). 71. CLASS, C. R., et al.: Adv. Cryog. Engng. 5, 254-61 (1960). 72. CLARK, J. A., et al.: Adv. Cryog. Engng. 5, 467-80 (1960). 73. CORBETT, R. J., J. E. BELL, and J. M. LESTER: Adv. Cryog. Engng. 7, 149-54 (1962). 74. COXE, E. F., and J. W. TATOM: Adv. Cryog. Engng. 7, 234-43 (1962). 75. CASSUTT, L., D. BIRON, and B. VONNEGUT: Adv. Cryog. Engng. 7, 327-35 (1962). 76. CROCCO, L., 1. GLASSMAN, and 1. E. SMITH: A Flow Reactor for High Temperature Reaction Kinetics, J. Forrestal Res. Center, Princeton Univ., Aeron. Engng. Rept. 398, AFOSR TN 57-573, AD 132445. 77. CRAMER, K. H.: Orbital Storage of Cryogenic Fluids, Wright Air Dev. Center, WADC Techn. Note 58·282 (Oct. 1958),7 p., AD 203527. 78. CURREN, A. N., H. G. PRICE, and H. W. DOUGLASS: Analysis of Effects of Rocket-Engine Design Para• meters on Regenerative Cooling Capabilities of Several Propellants, NASA TN D-66 (Sept. 1959), 47 p., AD 225811. 79. CONWAY, 1. B., et al.: J. Am. Chern. Soc. 77, 2026 (1955). 80. CONWAY, 1. B.: J. Am. Chern. Soc. 75, 499 (1953). 81. CONWAY,1. B., and A. V. GROSSE: J. Am. Chem. Soc. 80, 2972-6 (1958). 82. CONWAY, 1. B., and A. V. GROSSE: Combustion of Cyanogen and Oxygen at 100 psia, Office Naval Res., Final Rept. (N 9·onr-87 301) (1 July 1954). 83. COHEN: Fuel 34, 123-7 (1955). 84. CASSUTT, L. H.: ARS·J. 31, 1122-8 (1961). 85. COXE, E. F., et al.: Adv. Cryog. Engng. 8, 404-10 (1963). 86. Anonym: Performance Evaluation of Liquid-Vapor Sensors in a Zero-Gravity Environment at Liquid- Hydrogen Temperature, Convair/Astronautics Rept. No. AE 62-0329 (25 May 1962). 87. CHELTON, D. B., B. W. BIRMINGHAM, and J. W. DEAN: Adv. Cryog. Engng. 8, 311-4 (1963). 88. CANRIGHT, R. B.: Ind. Engng. Chern. 49,1345-7 (1957). 89. CLARK, J. D.: US Pat. 3115005 (28.5. 1957/24. 12. 1963), Inh.: US Navy, Ref.: CA 60, 7864£. (1964). 90. CARNAVOS, T. C.: Some Tests with RFNA-Anhydrous Liquid Ammonia in 1000-pound Thrust Rocket Motors, General Electric Co., Rept. R 53A 0521, Contract DA 30-115·0RD-23, Proj. TU 1-2000 A (Oct. 1958), 10 p., AD 22172. 91. California Res. Corp.: United Kingdom Pat. Spec. 816769 (19. 3.1956/15.7.1959), Ref.: CZ 1960, 16312. 92. CARMODY, D. R., and A. ZLETZ: US Pat. 2857737 (28.10.1958), Inh.: Stand. Oil Co., Indiana, Ref.: CA53, 4703c (1959). 93. CARMODY, D. R., and A. ZLETZ: US Pat. 3066478 (30. 11. 1954/4. 12. 1962), Inh.: Stand. Oil Co., Indiana, Ref.: CA 58, 7781a (1963). 94. CARMODY, D. R., and A. ZLETZ: US Pat. 2998699 (5. 9. 1961), Inh.: Stand. Oil Co., Indiana, Ref.: CA5S, 27892. 95. CARMODY, D. R., and A. ZLETZ: US Pat. 2857738 (28.10.1958) und US Pat. 2857736 (28.10.1958), Inh.: Stand. Oil Co., Indiana, Ref.: CA 53, 4703c (1959). 96. CORELLI, R.: Fusees 2,69-75 (1958). 97. CUDDY, W. A.: The Utilization of Sensitivity Data Obtained From JANAF-Recommended Liquid Pro• pellant Test Methods, ARS-Preprint 1245-60 (1960). 98. COTTRELL, T. L., T. E. GRAHAM, and T. J. REID: Trans. Farad. Soc. 47, 584-90 (June 1951). 99. CASS, W. G.: Aircraft Engng. 22, 238-9 (1950). 100. Commercial Solvents Corp., Chern. Engng. News 30: 22, 2344 (1952). 101. CORELLI, R. M.: Tetranitromethane and Its Use as an Oxidizing Agent for Rockets, 3rd Congr. Aeron. European, Bruxelles 1958, Vol. 2, p. 582-66 (1962). 102. CARPENTER, R. A.: ARS-J. 29, 8-14 (1959). 103. Callery Chemical Co.: Diborane, Tech. Bulletin C-020 (15. 3. 1958), 18 p. Literaturverzeichnis C 727

104. CHERENKO, J. P.: Forced Convection Heat Transfer Characteristics of Liquid Pentaborane, Callery C. C., Contract Noa(s) 58-454-d (Sept. 1962). 18 p., NASA STAR N 62-17168, AD 285938. 105. Anonym: Chern. Week 1959, 21ff. (22 Aug. 1959). 106. Anonym: Chern. Engng. News 1959: 34, 19 (1959). 107. Anonym: Trialkyl Boranes, Callery C. C. Bulletin C-311 (1 March 1959). 108. Anonym: Triethylborane, Tri-n-butylborane, Callery C. C. Bulletin C-310 (15 June 1959). 109. COHEN, M. S., and C. E. PEARL: US Pat. 3109862 (1. 7. 1955/5. 11. 1963), Ref.: CA 60, 3005f (1964). 110. CARMODY, C.R., and A.ZLETZ: US Pat. :~001361 (29.1.1952/26.9.1961), Inh.: Stand. Oil Co., Indiana, Ref.: CA 57, 15403 (1962). 111. Anonym: Amine-Boranes, Callery C. C., Tech. Bulletin C-200 (1 Apr. 1958), 8 p. 112. CHILENSKI, J. J.: US Pat. 3120738 (3.3. 1962/11. 2. 1964), Inh.: NASA, Ref.: CA 60, 15676 (1964). 113. CARPENTER, R. A.: US Pat. 3136669 (17.10.1958/9.6.1964), Inh.: Spencer Chem. Co., Ref.: CA61, 934ge (1964). 114. CORDES, H. F.: J. Phys. Chern. 65, 1473 (1961). 115. CHAMBERLAIN, D. L.: Neutralization of Fluorine, Stanford Res. Inst., Menlo Park, Calif., Addendum 1 to Final Rept. (4 June 1958) 25 p., AD 160472. 116. COLBURN, C. B.: Adv. Fluorine Chemistry 3,92-116 (1963). 117. COOK, G. A.: US Pat. 3008902 (19. 11. 1956/14. 11. 1961), Inh.: Union Carbide Corp., Ref.: CZ 1963, 9460, US Pat. 2975035 (19. 11. 1956/14.3. 1961), Ref.: CZ 1963, 7900. 118. CARTER, H. G.: Radiation-Induced Molecular Reactions in Liquid Hydrogen, Atomic Energy Commission, Proc. Nucl. Prop. Conf., Montcrey, Calif., 15.-17. Aug. 1962, p. 35-42, N63-22306, N63-22301. 119. CORCORAN, J. M .. H. W. KRUSE, and S. SKOLNIK: J. Phys. Chem. 57, 435-7 (1953). 120. CROCCO, L., J. GREY, and G. B. MATTHEWS: .5th Symp. on Combustion, Reinhold Pub!. Corp., New York (1955), p. 164-70. 121. CORELLI, R. M.: Chimica e Industria (Milano) 31, 436 (1949), Ref.: CA 46,9845 (19.')2). 122. CARTER, E.: Thermodynamic Charts for the Decomposition Products of 80% Hydrogen Peroxide, Gt. Brit. Royal Aircr. Establishment, Tcch. Note RPD 88 (Oct. 1953). 7 p., AD 21443. 12:3. CARTER, E.: Thermodynamic Charts for the Decomposition Products of 80, 85 and 90% Hydrogen Per- oxide, Gt. Brit. Royal Aircr. Establishment, Tech. Notc RPD 164 (April 1958), 12 p .• AD 203455. 124. CHI, J. W. H., and A. M. VETERE: Adv. Cryog. Engng. 9, 243-53 (1964). 125. CARNEY, R. R.: Adv. Cryog. Engng. 9, 529-36 (1964). 126. CRANE, C. H., and W. G. SMITH: Welding J. 40: 1, Suppl. 33S-40S (1961), Ref.: CZ 1964: 19,226. 127. CHRISTE, K. 0., and J. P. GUERTIN: Inorganic Chemistry 4: 6. 905-8 (1965). 128. CHRISTE, K. 0., and J. P. GUERTIN: Inorganic Chemistry 4: 12, 1785-7 (1965). 129. CHRISTE, K. 0., and J. P. GUERTIN: Inorganic Chemistry 5.473-5 (1966). 130. COLBURN, C. B.: The Fluorides of Nitrogen and Their Derivatives. 3rd Internat. Symposium on Fluorine Chemistry, Miinchen 1965, Preprint. 131. CHRISTIAN, J. L., and J. F. WATSON: Adv. Cryog. Engng. 10, 63-76 (1965). 132. CHI, J. W. H.: Adv. Cryog. Engng. 10, 330-40 (1965). 133. CLARK, J. A.: Internat. Adv. Cryog. Engng. 10 MU, 259-83 (1965). 134. CAMPBELL, M. D.: Adv. Cryog. Engng. 10, 154-62 (1965). 135. CHAMBERLAIN, D. W.: Adv. Cryog. Engng. 10, 117 -25 (1965). 136. CAREN, R. P., et a!.: Adv. Cryog. Engng. 10,171-80 (1965). 137. CORRUCINI, R. J.: Properties of Liquid Hydrogen, Inst. Internat. du Froid, Cours sur I'Hydrogfme Liquide, Grenoble (France) (Juin 1965), Preprint. 138. CONELLY, J. G., and B. R. ETHERIDGE: Establishing Proven Design Criteria for Cryogenic Boost Tanks (Hydrogen), Beech Aircr. Corp., Quart. Progr. Rept. 8 (Dec. 1961), 39 p., AD 269195. 139. CHI, J. W. H.: J. of Spacecraft and Rockets 3, 150-2 (1966). 140. COMER, S. W.: and A. V. JENSEN: Anal. Chem. 36, 799-800 (1964). 141. COLLINS, J. 0., and S. P. TERPKO: US Pat. 3146139 (23. 12. 1960/25. 8. 1964), Callery Chem. Co., Ref.: CA 61, 13120d. 142. COATES, G. E., and F. GLOCKLlNG: J. Chern. Soc. 1954, 2526-9 (1954). 143. CORDES, H. F.: J. Phys. Chern. 67, 1693-8 (1963). 144. COMER, S. W.: Anal. Chem. 37: 7, 958 (1965). 145. CHANG, E. T., and N. A. GOKCEN: General Research: Thermodynamic Properties of Hydrazine, Unsymm. Dimethylhydrazine and Their Mixtures. Aerospace Corp., EI Segundo, Calif., Aerodyn. and Prop. Res. Lab. Rept. ATN-64 (9228)-2 (Jan. 1964),31 p., AD 458288, N65-18413. 146. CLARK, W. L., A. NUDO, and P. YIN: The Determination of Water in Storable Rocket Propellants, in: Humidity and Moisture-Measurement and Control in Science and Industry Vo!' 4, P. N. WINN (Editor), Reinhold Pub!. Corp. New York 1965, p. 55-61. 147. COATES, R. L.: Application of the T-Burner to Ballistic Evaluation of New Propellants, AIAA Preprint 66-599 (1966). 148. CHRISTE, K. 0., J. P. GUERTIN, and A. E. PAVLATH: Inorg. Nuc!. Chem. Lettcrs 2, 83 (1966). 149. CHANG, E. T., and N. A. GOKCEN: J. Phys. Chem. 70, 2394-9 (1966). 728 Literaturverzeichnis D

150. CHELTON, D. B., and D. B. MANN: Univ. of California Rept. UCRL 3421 (15 May 1956). 151. CROOMERS, E. F.: Comb. and Flame 10, 71-77 (1966). 152. CULLIS, C. F., A. FISH, and R. T. POLLOND: Proc. Roy. Soc. Lond. A 289, 413-23 (1966). 153. CHUAN, R. L., and P. C. WILBER: J. of Spacecraft and Rockets 4, 282-4 (1967). 154. CHILENSKI, J. J., and D. H. LEE: An Experimental Investigation of the Performance of the N 20 4/N2H 4 System in the Oxidizer-Rich and Fuel-Rich Regions, JPL TR 32-212 (12 March 1962). 155. CONNAUGHTON, J. W., B. F. WILSON, and W. W. WHARTON: An Experimental Study of Hypergolic Ignition and Restart in a Unique Hybrid Window Motor, AIAA Paper 66-69. 156. CHRISTE, K. 0., et al.: Inorg. Chern. 6, 533-7 (1967). 157. CARTER, G. T.: Liquid Propellant Safety Handbook, NASA TM X-56611, SP-4-44-S (Apr. 1965), N65- 27959. 158. CURRY, J. E., and W. G. SCHECK: Development of a New Cryogenic Gasket for LOX Service, NASA TM X-57585, p. 117-28 (1965), N66-31435. 159. COOK, G. A., and R. F. DWYER: Adv. Cryog. Engng. 11, 202-6 (1966). 160. CURREN, A. N., et al.: Experimental Heat-Transfer Study of a Regeneratively Cooled Hydrogen-Fluorine Rocket Engine at Low Chamber Pressure, NASA TN D-4178 (Sept. 1967) 68p., N67-35667. 161. CHRISTOS, T., et a!.: J. of Spacecraft and Rockets 4, 1224-9 (1967). 162. CAREY, L.: J. of Spacecraft and Rockets 5, 168-72 (1968). 163. CRAWFORD, R. F., R. G. HANNAH,and C. D. NEVINS: J. of Spacecraft and Rockets 4,1598-603 (1967). 164. CHI, J. W. H.: J. of Spacecraft and Rockets 4, 1329-32 (1967).

D

1. DADIEU, A.: Raketentechnik u. Raumfahrtforschung 5, 87 -9 (1961). 2. DALE, J. W., et al.: Research on Synthesis of New Oxidizers for Solid Propellants, Contract AF 04 (611)- 8520, Monsanto Res. Corp., Boston Labs., Everett, Mass., Quart, Techn. Summ. Reports: a) No.1 MRB 202201 (10 Dec. 1962) 11 p., b) No.3 MRB 202203 (22 Apr. 1963) 32 p. 3. DODD, R. E., and R. LITTLE: Nature 188,737 (1960). 4. DAWSON, B. E., and R. R. SCHREIB: Investigation of Advanced High Energy Space Storable Propellant System OF2/B2Hs' AlAA Preprint 63-238 (June 1963), 14 p. 5. DESS, H. M.: US Pat. 2942947, US Pat. 2942949, Ref.: CA54, 21681 (1960); US Pat. 2982618, Ref.: CA 55, 16927b (1961). 6. DERR, D. F.: US Pat. 2961467 (25. 10. 1956/22. 11. 1960), Inh.: Food Machinery and chern. Corp. 7. DRAEGER, A. G., and J. W. GETZ: Franz. Pat. 1275647 (5.12.1960/2.10.1961), Inh.: Food Machinery and Chern. Corp. 8. DIAMOND, P., and A. A. THOMAS: Determination of UDMH in Urine, Wright Patterson AFB, Aerospace Med. Div., 6570th Aerospace Med. Res. Labs., Final Doc. Rept. AMRL TDR 62-119 (Oct. 1962), 14 p., N 63-10186. 9. DEUTSCHMANN, A. J., and W. C. BULL: US Pat. 2803523, 2803524 (20. 8.1957), Inh.: Spencer Chern. Co., Ref.: CA 52, 673h. 10. DEVINS, J. C.: J. Am. Chern. Soc. 76, 2618-26 (1954). 11. DEVINS, J. C., and M. BURTON: US Pat. 2849357 (26.8.1958), Inh.: Olin Mathieson C. C. 12. DEVRIES, J. E., and E. S. CLAffi-GANZ: Ana!. Chern. 25, 973-4 (1953). 13. DOERNER, M. P.: US Pat. 2901886 (21. 3. 1956/1. 9. 1959), Dow Chemical, Midland, Mich., Ref.: CA 54, 3958e (1960). 14. DOLAH, R. W., M. G. ZABETAKIS, et a!.: Revue of Fire and Explosion Hazard of Flight Vehicle Combustibles (Vapor Pressures), US Bur. of Mines, Information Circ. 8137 (1963) 80 p., Ref.: CA 58, 7779c. 15. DE DAPPER, J. W., and M. NADLER: Nonmetallic Materials for Use ~With Liquid Rocket Propellants, North Am. Aviation, Downey, Calif., Missile Division, Report AL-692 (1951), unclassified LPH 729. 16. DUBoz, J.: Leitfiihigkeit von konz. Salpetersaure, EinfluB der Temperatur (in Franzosisch), Mem. des Poudres 34,351-5 (1952). 17. DEAN, L. E.: Heat Transfer Characteristics of RFNA, Bell Aircraft Corp., Buffalo, Rept. No. 117 -982-004 (July 1954). 18. DUFFY, C. H., W. H. CORCORAN, and B. H. SAGE: Ind. Engng. Chern. 48, 431-3 (1956) und CIT-JPL Progr. Rept. 20-235 (July 1954) 12 p. 19. DIGGLE, W. M., and J. C. GAGE: Brit. J. Industr. Med. 11, 140-4 (Apr. 1954). 20. Anonym: Brit. Pat. 895943 (9. 5. 62, Am. Prior. v. 8. 3. 60), Inh.: DuPont de Nemours & Co., Ref.: CA 57, 5590b (1962). 21. DRESDNER, R. D., F. N. TLUMAC, and J. A. YOUNG: J. Inorg. Nuc!. Chern. 14, 299-301 (1960). 22. DREW, C. M., and A. G. WHITTAKER: Mechanism of Decomposition of Concentrated Hydrogen Peroxide, US Naval Ordn. Test Station, Tech. Mem. 1602 (19 Jan. 1954),20 p., AD 30309. 23. DAVIS, N. S., and J. H. KEEFE: J. ARS 22,63-9 (1952) und ARS Preprint 29T-51. 24. DAVIS, N. S.: New Techniques for Transferring H 20 2 at High Pressures, ARS Preprint 174-54. Literaturverzeichnis D 729

25. DAVIS, N. S.: Hydrogen Peroxide as a Source of Oxygen, WatE'r. Heat and Power for Space Travel, Adv. in the Astronautical Sciences 2, Paper 31, 14 p., Xew York (1958). 26. DAVIS, N. S., and J. H. KEEFE: Ind. Engng. Chem. 48, 745-S (1956). 27. DIERDORFF, L. H.: The Supercooling of 90% Hydrogen Peroxide, Becco Tech. Rept. No. 2G, Subcontract DA·30-115-0RD-23, GE., Purchase Order AOSH 9 3282 (1 Jan. 1953). 28. DUFUR: J. Space Flight H155: 1, p. 8 (1955). 29. DIN, F. (Ed.): Thermodynamic Fun( tions of Gase~, Vol. I, Butterworths Sci. Publ., London 1956, p. 33-101. 30. DOWNING, R. C., et al.: Ind. Engng. Chern. 39, 259-62 (1947). 31. DOESCHER, R. N.: J. Chern. Phys. 20, 330 (1952). 32. Dechema: Dechema-WerkstofftabeIle, Herausgegeben von der Deutschen Gesellschaft fUr Chemisches Apparatewesen, Frankfurt, Postfach 7746. 33. DAVIS, W., et al.: The Gas Phase Reactions of Fluorine with \Vater: Reaction Times and Reaction Pro• ducts in a Dynamic Fluorine-Water-System, US Dept. Commerce, AEC, Rept. AECD 2877, Part I (27 Dec 1949). 34. DANGLE, E. E., and W. R. KERSLAKE: Experimental Evaluation of Gaseous Hydrogen Fuel in a 16-inch- Diameter Ramjet Engine, NACA RM E55-J18 (6 March 1956), 34 p. 35. DUDLEY, F. B., G. GARD, and G. H. CADY: Inorg. Chem. 2, 228-9 (1963). 36. DURIE, R. A.: Proc. Roy. Soc. A 211, 110 (1952). 37. DOUGLASS, H. W.: Experimental Performance of Fluorine-Oxygen-Mixtures with JP-4 Fuel in a Rocket Enginc, NACA RM E55-D27 (1955). 38. DOYLE, \V. L.: High Temperature System~ Using the Liquids Fluorine, Oxygen, Cyanogen and Hydrogen Cyanide, ARS Preprint 736-58 (1958), 13 p. 39. DOUGLASS, H. \V.: Experimental Performance of Liquid Fluorine and Liquid Ammonia Propellant Com- bination in 1000 Pound Thrust Rocket Engines NACA RM EM-C17 (May 1954), 32 p. 40. DRISCOLL, D. G.: Adv. Cryog. Engng. 0,95-102 (1960). 41. DRAYER, D. E., and K. D. TUIMERHAUS: Adv. Cryog. Engng. 7, 401-12 (1962). 42. DRELL, 1. L., and J<'. E. BELLES: Survey of Hydrogen Combustion Properties, NAG.-\. Tech. Report 1383 (1958),34 p. (altere Ausgabe: NACA RM E54-D24 (1957)). 43. DE JAEGERE, S., and A. VAN TIGGELEN: Flammpnfortpfianzung in Hydrazin-Mischungen (in Franzosisch), Revue de I'inst. fran~. du petrole pt annales des combustibles liquides 13, 451-6 (1958). , in 44. DYKEMA, O. W., and S. A. GREENE: An Experimental Study of RP-l, UDMH and N2H4 Single Droplet Burning in Air and in Oxygen; in: Progress in Astronauties and Hocketry, Vol. 2: Liquid Rockets and Propellants, Edited by L. E. BOLLlNm;R ct al., Academic Press, New York (1960), p. 299-324. 45. DONOVAN, T. M., C. H. SHOMATE, and W. R McBRIDE: J. Phys. ChE'm. 64, 281-2 (1960). 46. DWYER, R. J<'., G. A. COOK, and D. H. STELLRECHT: A Laboratory Study of Hydrogen Slush, Ind. Engng. Chern .. Prod. Res. am! Dev. 3, 31G-20 (1964), Ind. Engng. Chern. Research RE'sults Ms 64-216 (1964),24 p. 47. DEPPE, G. R., and R. H. Dow: Adv. Cryog. Engng. 8. 371-7 (1963). 48. Anonym: Patent Auslegeschrift DAS 1163868 v. 27. 2. 1964. 49. DE JAEGERE, S., and A. VAN TIGGELJ<;N: Comb. and Flame 3,187-200 (1959). 50. DE DAPPER, J. W.: US Pat. 28(j5727, Inh.: North Am. Aviat. (23.12.1958). 51. DIESEN, R. W.: J. Chern. Phys. 39, 2121-8 (1963), auch erschiencn als: Dow Chemical Co., Rept. (Aug. 1963),23 p., AD 414909. 52. Doss, R. C.: US Pat. 3013382 (14.8.1957/19.12.1961), Inh.: Phillips Petrol. Co., Ref.: CA57, 6200. 53. Doss, R. C.: US Pat. 3031838 (10.3. 1958/1. 5. 1962), Inh.: Phillips Petrol. Co., Ref.: CA 57, 7508. 54. DISHER, J. H.: J<'light Investigation of Pentaborane Fuel in Rocket Boosted 9,75 inch Diameter Ramjet Engine, NACA HIH E57-F27 (Sept. 1957),24 p. 55. DEREMIN, A. N., et al.: Detonation von Nitromethan in der Nahe der Grpnzen (in Rus8i~ch), Doklady Akad. Nauk SSSR 133, 1372--4 (1960), Ref.: CA 55, 12855. 56. DAVIS, N. S., and J. C. MCCORlIUCK: Design of Catalyst Packs for the Decomposition of Hydrogen Peroxide, in: Liquid Rockets and Propellants, Progress in Astronautics and Rocketry, Vol. 2, Edited by L. E. BOLLINGER et a!.. Academic Press, New York (1960), p. 589-616. 57. DITTER, J. :F., and I. SHAPIRO: J. Am. Chern. Hoc. Sl, 1022 (1959). 58. DELGADO, J. M. R., K. C. BACK, and A. A. THOlVIAS: Arch. Int. Pharmacodyn. 141,262-70 (1963), Ref.: CA 58, 14614c. 59. DOWNES, H. 1.: Brit. Pat. 945370 (5. 12. 1960/23. 12. 19(3). lnh.: Shell Oil Co., Ref.: CA 60, 15675 (1964). 60. DEREMIN, A. N., D. K. ROZANOY, and V. S. TROFUIOY: Comb. and Flame 7,153-62 (1963). 61. DENGLER, R. P.: An Experimental Investigation of Chemical Reaction Between Propellant Tank Material and Rocket Fuels or Oxidizers Wht'll Impacted by Small High Velocity Projectiles, NASA TN D-1882 (Aug. 1963), 39 p., N64-17152. 62. DEAN, L. E., and P. J. PETROZZI: Heat Transfer Conditions Occuring in a Hydrogen Cooled Combustion Chamber, ARS Pre print 1712--61 (1961). 63. DEMPSTER, W. E., and J. R. OLIVIER: Uround Facility Requirements for Subcooling Liquid Hydrogen, NASA TN D-127(j (July 1962), 21 p. 730 Literaturverzeichnis E

64. DONOHUE, J. A., T. D. NEVITT, and A. ZLETZ: OF2 Formation by Electrolysis ofWetHF, Am. Chem. Soc., Symp. on Advanced Propellant Chem. 1965, Preprint of Papers Vol. 9, No.1, p. 228-36, vgl. R. F. GOULD: Advanced Propellant Chemistry, ACS Series Vol. 54, Washington (1966). 65. DRAGO, R. S., and H. S. SISLER: J. Phys. Chern. 60,245-9 (1956). 66. DAWSON, B. E., A. F. LUM, and R. R. SCHREIB: Investigation of Advanced High Energy Storable Propellant System, Final Rept. June-Nov. 1962, Thiokol C. C., Reaction Motors Div., Denville, Final Rept. NASA Contract NASw-449-RMD-5507-F (1962), 118 p., N63-13249. 67. DEWITT, R. L., and H. W. SCHMIDT: Experimental Investigation of Liquid-Fluorine System Components, NASA TN D-1727 (June 19(3), 21 p. 6S. DEMoNEY, F. W.: Adv. Cryog. Engng. 9, 112-23 (1964). 69. DARDARE, M.: La Propulsion par l'Oxygene et I'Hydrogene Liquides. Institut International du Froid, Cours sur I'Hydrogene Liquide, Grenoble, France (Juin 19(5). 70. DEARING, D. L.: Summary of the Saturn S-IV and S-IVB Liquid Hydrogen Tank Internal Insulation, Development and Techniques for Future Improvement. Institut International du Froid, Cours sur l'Hydrogene Liquide, Grenoble (France) (Juin 19(5). 71. DEARING, D. L., and R. J. STEFFY: The Significance of Parameters Affecting the Heat Transfer to the Liquid Hydrogen in the SATURN S-IVB Stage for the Lunar Orbit Rendezvous Mission. Institut International du Froid, Cours sur l'Hydrogene Liquide, Grenoble, France (Juin 19(5). 72. DWYER, R. F., and G. A. COOK: Research and Rheologic and Thermodynamic Properties of Solid and Slush Hydrogen. Union Carbide Corp., (1 Feb. 19(5), 59 p., AD-456657, N 65-17475. 73. DuPont de Nemours and Co., Wilmington: Stability of High Strength H 20 2, Quarterly Report Period Ending Dec. 31, 1964, 29 p., AD-610853, N 65-17932. 74. DADIEU, A., und R. Lo: Beryllium und Berylliumverbindungen als Raketentreibstoffe. Raumfahrt- forschung 9, 192-6 (1965). 75. D'ALELLIO, G. F.: US Pat. 3146222 (27.9. 1961/25. 8. 19(4), Dal Mon Res. Co., Ref.: CA 61, 13120g. 76. DAUERMAN, L., G. E. SALSER, and Y. A. TAJIMA: J. Phys. Chem. 69, 3668-9 (1965). 77. DECKER, W. H.: J. of Spacecraft and Rockets 3,1296-7 (1966). 78. DE PALMA, J. V., and G. THODOS: J. of Spacecraft and Rockets 3,747-50 (1966). 79. DANEY, D. E., and D. B. MANN: Quality Determination of Liquid-Solid Hydrogen Mixtures, US Nat. Bur. of Standards, NBS 9189, NASA CR-76137 (21 March 1966), N 66-30304. 80. Anonym: Study to Determine an Improved Method for Apollo Propellant System Decontamination and Propellant Tank Drying, Dow Chemical Co., Midland, Mich., Contract NAS 9-4605, NASA CR-65371 (Apr. 1966),214 p., N 66-27047. 81. DUMONT, L. B., and F. L. MERRITT: Cavitating Venturi Valves for Deep Throttling of Cryogenic Fluids, AIAA-Paper 66-539 (1966). 82. DAVISON, W. R., and J. P. CARSTENS: Pyrodynamics 2, 275-304 (1965). 83. DOUGLASS, H. W., G. HENNINGS, and H G. PRICE: Experimental Performance of Liquid Hydrogen and Liquid Fluorine in Regeneratively Cooled Rocket Engines, NASA-TM-X-87 (Nov. 1959), 57 p., Declassified N 66-33342. 84. DARWIN, G. E., and J. H. BUDDERY: Beryllium, Butterworths Sci. Publ. Corp., London (1960) 392 p. 85. DEVOTO, R. S.: AIAA J. 4,1149 (Jun. 19(6). S6. DICKINSON, L. A., A. B. AMSTER, and B. L. CAPENER: Application ofTrioxygen-Difluoride in Liquid Pro• pellant Technology, AIAA Paper 68-93. 87. DEBooy, H. T.: Adv. Cryog. Engng. 12, 49-55 (1967). 88. DAVIDSON, D. L., and R. G. LANDRUM: Oxygen Difluoride Propellant System Design and Operational Experience at Arnold Center, AIAA Paper 67-279. 89. DEE, L. A., and A. K. WEBB: Anal. Chem. 39, 1165-7 (1967).

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1. ENGELBRECHT, A.: Monatsh. f. Chemie 83,1087-9 (1952). 2. EMELEUS, H. J.: Halogen Fluorides - Recent Advances, in: Fluorine Chemistry, Edited by J. H. SIMONS, Academic Press, New York 1954, Vol. 2, p. 39ff. 3. ENGELBRECHT, d., and H. ATZWANGER: J. Inorg. Nucl. Chem. 2, 348-57 (1956). 4. ELLIS, J. F., C. W. FORREST, and P. L. ALLEN: Anal. Chim. Acta 22, 27 -33 (1960). 5. ELLIS, J. F., and C. W. FORREST: J. Inorg. Nucl. Chern. 16, 150-3 (1960). 6. ELLIS, J. F.: The Attempted Use of a Hydrogen Flame Detector With Corrosive Gases, UK Atomic Energy Authority, Ind. Group Rept. IGR-TM/CA 042 (1956), 3 p. 7. ENGELBRECHT, A., und E. NACHBAUR: Monatsh. Chem. 90, 371-4 (1959). 8. ELLIS, J. F., and G. IVESON: The Application of GLC to the Analysis of Volatile Halogen and Interhalogen Compounds, Gas Chromat. Symp. Amsterdam (May 1958), Edited by D. H. DESTY, Butterworths Publ. Corp., p. 300-8. 9. ERMENC, E. D.: Design Data for Oxides of Nitrogen, Chem. Engng. 66: 7, 139-42 (23 Febr. 1959). Literaturverzeichnis F 731

10. ELVERUM, G. W., and J. S. MARTINEZ: Results of Performance Calculations for N 20 4-N2H, Bipropellant System, CIT-JPL Memo. 20-174 (July 1958), 56 p., AD 211722. 11. ELVERUM, G. W., and P. STAUDHAMMER: The Effect of Rapid Liquid Phase Reactions on Injector Design and Combustion in Rocket Motors, CIT-JPL Progr. Rept. 30-4 (25 Aug. 1959). 12. EGERTON: Trans. Chern. Soc. 105, 647 (1914). 13. ELLIS, S. R. M., et al.: Ind. Engng. Chern., Process Design and Dev. 3, 18-22 (1964). 14. EVANS, G. R.: Construction Materials for Containers of Liquid Propellants H 2, F 2, N2H4 and N20 4; An Annotated Bibliography, Lockheed Aircr. Corp., Spec. Bibl. SB-60-20 (Apr. 1960), 18 p., 142 referen• ces, AD 271 034. 15. EAGAN, E. P.: Ind. Engng. Chern. 37, 303-4 (1945). 16. ELVERUM, G. W., and D. M. MASON: J. Phys. Chem. 60, 104-8 (1956) und CIT-JPL Progr. Rept. 20-224 (May 1954). 17. EYRING, H., and F. DANIELS: J. Am. Chem. Soc. 52, 1476-86 (1930). 18. EMELYANOV, Yu. M., and Yu. V. FILIPPOV: Russian J. Phys. Chern. 36, 1224-7 (1962). 19. EMELYANOVA, T.I., B. V. STRAKHOV, and V. P. LEBEDEV: ARS-J. 31, 1350 (1961). 20. ELLIOT, D., and L. ROSENTHAL: Development of a Small Hydrogen Peroxide Solid Catalyst Rocket, ARS• Preprint 54-52. 21. ELROD, C. W.: Hydrogen Subcooling for Aerospace Vehicles, Am. Inst. of Electrical and Electronics Engrs., Int. Con£. and Exhib. on Aerospace Support, Washington, D. C., IEEE Transactions on Aerospace Vol. AS-l (Aug. 1963), p. 864-73. 22. ELVERUM, G. W., and R. N. DOESCHER: J. Chern. Phys. 20, 1834 (1952). 23. ERICSON, G. L., W. K. BOYD, and P. D. MILLER: Corrosion of Tiin Gaseous and Liquid Fluorine, TML Tech. Mem. (30 April 1958). 24. ERIKSON, T. A.: ARS-J 30,190-1 (1960). 25. EDSE, R., and W. L. DOYLE: Thermodynamic Calculations of the Performance of the Hydrogen and Fluo• rine System, Wright Air Development Center. W ACD Tech. Rept. 53-427 (March 1956). 46 p., AF Contract AF 33(616)2078, Task 70158. 2G. EULNER, R., J. MERTENS, and R.1,. POTTER: Comb. and Flame 5, 1-5 (1961). 27. ENGELBRECHT, A., und E. NACHBAUR: Monatsh. Chern. 90, 367-70 (1959). 28. EDSE, R.: Performance of a Premixed Gaseous Hydrogen and Oxygen Propellant Rocket Engine, ARS• Preprint 620-58 (1958). 29. EDESKUTY, F. J., and E. F. HAMMEL: Cryogenics 2, 193-203 (June 1962). 30. EBERSTEIN, I.J., and I. GLASSMAN: Consideration of Hydrazine Decomposition, Princeton Univ., Dept. Aeron. Engng. Rept. 490 (Dec. 1959), 23 p. 31. EVANS, M. W., F.1. GIVEN, and G. M. MULLER: Jet Propulsion 28,255-6 (1958). :~2. ERIKSON, T. A., and E. L. GROVE: Fundamentals of Liquid Propellant Sensitivity, Armour Res. Found., Chicago, IlL, Final Rept. ARF 3197-15 (26 Nov. 1962),68 p., N 63-10956. 3:3. EBERSTEIN, I.J., and I. GLASSMAN: Consideration of Hydrazine Decomposition, in: Liquid Rockets and Pro- p311ants, Progress in Astronautics and Rocketry Vol. 2, Academic Press, New York 1960, p. 351-66. 34. ETHERINGTON, T. L., and L. V. MCCARTY: AMA Arch. Ind. Hyg. Occ. Med. 5, 447-50 (1952). 3;"). ENGELBRECHT, A., E.NACHBAUR undE. MAYER: J. of Chromatography (Amsterdam) 15,228-35 (1964). 36. EpSTEIN, M.: Internat. Adv. Cryog. Engng. 101\IU, 303-7 (1965). :n. EpSTEIN, M., and H. K. GEORGIUS: Internat. Adv. Cryog. Engng. 10 MU, 290-301 (1965). 38. EYLES, A. G.: Adv. Cryog. Engng. 10, 224-32 (1965). 39. EDESKUTY, F. J.: Liquid Hydrogen in Nuclear Rocket Testing, Institut International du Froid, Cours sur I'Hydrogtme Liquide, Grenoble (Juin 19(5). 40. EVERY, R. L., and J. O. THIEME: J. of Spacecraft and Rockets 2,787-9 (1965). 41. ENGLISH, W. D., and D. R. SPICER: Cryog. Technol. 1, 260 (1965), Ref. CA 64,9497 (1966). 42. ELLION, M. E., et al.: J. of Spacecraft and Rockets 4,339-47 (1967). 43. EVEREST, D. A.: The Chemistry of Beryllium, Elsevier Pub1. Comp., Amsterdam, 151 p. (19G4). 44. ELVERUM, G. \V., et al.: The Influence of Chamber Pressure on Theoretical Performance of the F2/N2H4, F2/NH3 and F2/H2 Propellant Systems, ClT-JPL Memo 20-130 (28 June 1956) 28 p., AD 117915. 45. ENGEL, L. J.: Difllloroamino Adducts for Use as Rocket Propellant Oxidizers, US Pat. 3346430, Esso Res. Engng. Co. (14.8.1961/10.10.1967), CA 67,10417.

F

1. FARRAR, R. L.: Safe Handling of Chlorine Trifluoride and the Handling of Chlorine Oxides and Oxifluorides, US AEC Rept. K-1416, 1-53 (1960), Ref.: CA 55, 6795e (1961). 2. FRAZER, J. W.: US Pat. 3033771 (11. 4.1960/8.5. 19F-2), US Atomic Energy Commission. 3. Fox, H. M.: US Pat. 3068641 (18.4. 1955/18. 12. 196:l), Ref.: CA 58, 4369d (1963). 4. FURGASON, R. R., and J. M. SMITH: J. Chem. Engng. Data 7:4, 528-9 (1962) . •5. Anonym: Brit. Pat. 868147 (1. 8. 1957/17.5.1961, Am. Prior. v. 6. 8. 1957), lnh.: Food Machinery and Chemical Corp., Ref.: CZ 1963, 684. 732 Literaturverzeichnis F

6. FEHER, F., und J. CREMER: Z. anorg. allg. Chemie 293, 343-4 (1958). 7. FINE, A. L.: Chemical Safety Mem. Rept. No. 11, Naval Air Missile Test Center, Point Mugu, Calif. (1948). 8. FLATT, R, et F. BENGUERD: Helv. Chim. Acta 45,1765-85 (1962). 9. FINE, B.: J. Chern. Engng. Data 7: 1,91-4 (1962). 10. FINE, B.: J. Chem. Engng. Data 7: 4, 494-6 (1962). 11. FORSYTHE, W. R, and W. F. GIAUQUE: J. Am. Chern. Soc. 68, 48-61, (1942). 12. FRIEDEL, R A., J. L. SCHULTZ, and A. G. SHARKLEY: Anal. Chem. 31, 1128 (1959). 13. FONTANA, M. G.: Materials for Handling Fuming Nitric Acid and Properties of Fuming Nitric Acid with Rcference to Its Thermal Stability, Ohio State Univ., Columbus,WADC US Air Force Tech. Rept. 6519/3 (Jan. 1954),81 p., AD 27932; AF TR 6519/4 (March 1954), 130 p,. AD 47644. 14. FETTER: Chem. Engng. 1948 (Jan.-April). 15. FINE, B.: J. Chem. Engng. Data 7,177-8 (1962). 16. FILIPPOV, Yu. V., and Yu.lVI. EMELYANOV: Russian J. Phys. Chern. 35, 14-9 (1961), 35: 2, 196-200 (1961),35: 3, 303-6 (1961). 17. FILIPPOV, Yu. V., et aI., I: Schurnal Fisitschesskoi Chimii 31: 4, 896-903 (1957), III: - 32, 2817-23 (1958), V: - 33: 8, 1780-7 (1959), VI: - 33: 10,2358-64 (1959), VIII: vgl. SAMOILOVICH [S 53], IX: vgl. EMELYANOV [E 18]. 18. FRANCK, E. U., und W. STOBER: Z. f. Naturf. 7 a, 822-3 (1952). 19. FASSTOWSKIJ, W. G., i A. E. ROWINSKIJ: Sch. Prikladnoi Chimii 29: 9, 1309-15 (1956) und J. Appl. Chern. USSR 29,1415-20 (1956) (English translation), Ref.: CA 51, 3297i (1957). 20. FISCHER, W. G.: Glas- u. Instr.-Technik 8, 68-70 (1964). 21. FISHBURNE, E. S., and R EDSE: Detonability of Ozone and Nitric Oxide, Liquid Rockets and Propellants, ARS Progr. in Astronautics and Rocketry Series Vol. 2, p. 367 -83, Academic Press, New York (1960). 22. FURUKAWA, G. T., and R E. MCCOSKEY: The Condensation Line of Air and the Heats of Vaporization of Oxygen and Nitrogen, NACA Tech. Note 2969 (June 1953). 23. FOSTER, R H., and S. T. STOY: Study of Liquid Oxygen Contamination, Air Products and Chemicals Inc., Allentown, Pa., Progress Rept. No.6 (Jan. 1961), 18 p., AD 271373 and Final Rept., Contract AF 33(616)6730, Proj. 3148 (May 1961), 144 p., AD 272377. 24. FOSTEN, 1.: Jet Propulsion 26, 985-8 (1956). 25. FOLEY, W. T., and P. A. GIGUERE: Canad. J. Chem. 29, 891>-903 (1951). 26. FRONING, J. E., et al.: Ind. Engng. Chern. 39, 275-8 (1947). 27. FRANCK, E. U., et al.: Z. Elektrochemie 58,374 (1954); 55,634 (1951). 28. FITZGERALD, F.: Fuel 40, 275-80 (1961), Ref.: CA 55, 20435. 29. FOCHTMAN, E. G., 1. F. BITTEN, and S. KATZ: Ind. Engng. Chern., Prod. Res. Dev. 2, 212-6 (1963). 30. FOWLER, J. M., and C. F. WARNER: ARS-J 32,266-7 (1962). 31. FORTINI, A., and V. N. HUFF: Theoretical Performance of Liquid Fluorine and Liquid Hydrogen as a, Rocket Propellant for a Chamber Pressure of 600 psia, NACA RM E 56-L lOa (25 Jan. 1957), 38 p_ 32. FRIEDMAN, R, and E. BURKE: J. Chern. Phys. 21, 165 (1953) und 5th Symp. on Combustion, Reinhold Publ. Corp., New York (1955), p. 596-603. 33. FLIEDER, W. G., W. J. S)UTH, and K. R WET)IORE: Adv. Cryog. Engng. 5, 111-9 (1960). 34. FORTINI, A., C. D. HENDRIX, and V. N. HUFF: Experimental Altitude Performance of JP-4 Fuel and Liquid Oxygen Rocket with Expansion Ratio of 48, NASA Memo 5-14-59E (May 1959), 27 p. 35. FRUCHTMAN, 1.: Stability Limits of the Premixed Stoichiometric Cyanogen-Oxygen Flame, NASA TN D-1480 (Oct. 1962), 25 p. 36. FORBES, F. W., and C. R MARTEL: Adv. Cryog. Engng. 8, 411-6 (1963). 37. FERGUSON, H. B.: US Pat. 2991166 (4. 7.1961), Inh. Thiokol, Ref.: CA 55, 26449c. 38. FRIEDMAN, R, W. P. BARNES, and M. MARKELS: A Study of Explosions Induced by Contact of Hydrazine• Type Fuels with Nitrogen Tetroxide, Atlantic Res. Corp., Alexandria, Final Rept. No. ARC 62- 5038.05-F, Contract AF 33(616)6918, ASD TDR 62-685, AD 289035, OTS. 39. FEILER, C. E., and L. BAKER: A Study of Fuel-Nitric Acid Reactivity, NACA RM E 56-A 19 (April 1956), 48p. 40. FRANQON, J.: Beziehung zwischen chemischer Struktur und Reaktion mit HNOa bei Raketentreibstoffen (in Franzosisch), Notes tech. publ. sci. et tech. min. air 89,1-47 (1960). 41. FORSTEN, 1.: Mollier Charts for the Products of Combustion of Ammonia and Nitric Acid, Naval Air Rocket Test Station, NARTS Rept. 83, Proj. TED-ARTS-S 1-505-6 (April 1956),12 p., AD 101026_ 42. FISH, W. R: Storable Liquid Propellants, Nitrogen TetroxidejAerozine 50, Aerojet-Gen. Corp., Sacra• mento, Calif., LRP-198 (2nd Edition) (June 1962), 384 p., N 63-18834. 43. FRANQON, J.: Eigenschaften hypergoler Treibstoffe (in Franzosisch), Publ. Sci. et Techn. Ministere Air de France, Notes Tech. NT 66 (1957), 43 p. 44. FELBERG, R S., and J. R GOULD: US Pat. 2000788 (20.1. 1955/25.8.1959), Inh.: Thiokol Chern. Corp., Ref.: CA 54, 3958d (1960); CZ 1960, 11170. 45. FUCHS, R: Explosivstoffe 6, 89-97 (1958). 46. FUCHS, R: Die Amine als Raketentreibstoffe, ER-Bericht Nr. 135, BMW Flugmotorenbau Berlin (1. Juni 1943). Literaturverzeichnis G 733

47. FURNO, A. L., G. H. MARTINDlLL, and M. C. ZABETAKIS: J. Chern. Engng. Data 7, 375-6 (1962). 48. FIVEL, H. J., L. TOWER, and J. B. GIBBS: Pentaborane Combustion Performance in 9,75 inch Diameter Ramjet Engine in Connected-Pipe Altitude Facility, NACA RM E 54-1 16 (March 1957), 47 p. 49. FOSTER: Experimental Study of Nitromethane Rocket Motors with Varying Fineness Ratio, Characteristic Length and Chamber Pressure, CIT-JPL Rept. 4-53 (May 1947), 25 p. 50. FLETCHER, E. A.: Spontaneous Flammability of Pentaborane and Pentaborane-3-Methylpentane Blends. NACA RM E 53-1 17 (Febr. 1957), 11 p., (Declass. NASA Publ. Ann. 1, p. 12, 11/14/58). 51. FAUTH, M. 1., and C. F. McNERNEY: Anal. Chern. 32, 91-2 (Jan. 19(0). 52. FURUKAWA, G. 1., and R. P. PARK: J. Res. Nat. Bur. Stand. 55, 255-60 (1955). 53. FLETCHER, E. A., R. G. DORSCH, and H. ALLEN: ARS-J. 30, 337-44 (1960). 54. Anonym: Sprite Rocket Motors, Flight 1949, 288 (Sept. 1949). Anonym: Sprite Rocket, Flight 1950,157-61 (Febr. 1950). 55. FELDHAN, S. L.: Design and Performance of Type MD-l Liquid Oxygen Storage and Servicing Semi- Trailer, Air Products Inc., Emmaus, Pa., WADC Tech. Rept. 55-448 (Nov. 1956), 150 p., AD 116543. 56. FRAZER, J. W.: J. Inorg. Nucl. Chem.1l, 166-7 (1959). ;"")7. FURGASON, R. R., and J. M. SMITH: Am. Inst. Chern. Engrs. J. 8, 654-8 (1962), Ref.: CZ 1964: 5, 210-1. 58. FISCH, K. R., et al.: Compatibility of Lubricants with Missile Fuels and Oxidizers, Am. Soc. of Lubrication Engrs. 5, 287 -96 (1962), Ref.: NASA STAR N 63-13326 und CA 58, 6628f. 59. FOSTEN, 1.: MollieI' Charts for the Decomposition of Hydrogen Peroxide-Water Mixtures, Naval Air Rocket Test Station, Lake Denmark, NARTS-TED-S 1-50:")·() Rept. 43 (Nov. 1954), 11 p., AD 42747. AD 15405. 60. FRAINIER, R. J.: Adv. Cryog. Engng. 6, 20-31 (1961). 61. FAGER, J. A.: J. Spacecraft and Rockets 2,369-75 (1965). 62. FICK, H. J.: Evaluation of the Compatibility of Polyvinylidene Fluoride (KYNAR) with Storable Liquid Propellants (NZ0 4 a. NzH 4), Schjeldahl Co., Northfield, Minn., NASA CR-50999 (30 Jan. 19(3). 23 p., N 63-21363. (j3. FINHOLT, A. E., A. C. BOND, and H. 1. SCHLESINGER: J. Am. Chern. Soc. 69,1199-1203 (1947). 64. Fox, H. M.: US Pat. 2970898 (15.5.1958/7.2.1961), Phillips Petrol. Co. 65. FRANKEL, M. B., et al.: Am. Chern. Soc., Symposium on Advanced Propellant Chemistry, Detroit 1965, Preprint of Papers Vol. 9, No.1, p. 107-17. 66. FLETCHER, E. A.: Ind. Engng. Chern. 51, 1389-90 (1959). 67. FLANAGAN, J. R.: Fluorine Propulsion Technology, AIAA Paper 65-536 (1965),17 p. 68. FLOYD, J. G., B. G. SMITH, and H. H. SEIDEL: A Fortran Program for Heat Transfer Analysis of the J-2 Engine, Brown Engineering Co., Inc., Huntsville, Rept. R-127 (March 19(5), NASA CR-67353, N 66-30300. 69. FEIGEL, H.: Investigations of Space Storable Propellants OFz/B2H6' Thiokol Chern. Corp., Denville. Final Rept. RMD-6039-F, NAS 3-2553, NASA CR-5474 (10 June 19(6), 184 p., N 66-39930. 70. FARQUAHR, J., and B. K. LINDLEY: Hydraulic Design of the M-l Liquid Hydrogen Tlirbopllmp, Aerojet Gen. Corp., AGN"-8800-68, NASA CR-54 822 (15 July 1966) 106 p., N66-32 334. 71. FAETH, G. M., B. L. KARHAN, and G. A. YANYECIC: The Ignition and Combustion of Monopropellant Droplets, AIAA Paper 67-480.

G

1. GOULD, J. R., and R.A. SMITH: Abstraet. of Papers, 138th ACS Meeting, New York, Sept. 1960, p. 7M. 2. GOULD, J. R., and R. A. SMITH: Franz. Pat. 1267046 (9.9.1960/5.6.1961), Inh.: Stauffer Chern. Co. 3. GRISARD, J., H.A. BERNHARDT, and G. OLIVER: J. Am. Chern. Soc. 73, 5725-7 (1951). 4. GRIGGER, J. C., and H. C. MILLER: Wright Air Development Div., Tech. Rept. 61-54 (1961), Ref.: Werk• stoffe u. Korrosion 14, 201 (1963). ii. GREGORY, J. W., and D. M. STRAIGHT: Ignition of Hydrogen-Oxygen Rocket Combustor with Chlorinp Trifluoride and Triethyl Aluminum, NASA TN D-684 (Apr. 19(1),24 p. 6. GUSTAVSON, J.: The Hybrid Rocket Motor and Its Unique Capabilities, ARS Preprint 1167-60 (1960). 7. GORDON, J., and B. SUKORNICK: US Pat. 3055817 (16.5.1961/25.9.1962). Inh.: Allied Chern. Corp. 8. GROSSE, A. V., A. G. STRENG, and A. D. KIRSHENBAUM: J. Am. Chern. Soc. 83,1004-5 (1961). 9. GATTI, R., et al.: Z. phys. Chern. N F 35,343-7 (1962). 10. GATTI, R., J. E. SICRE Y H. J. SCHUMACHER: Ann. Asoe. quim. Arg. 47, 180-97 (1960), Ref.: CZ 1961, 1488 und 1962, 18391. 11. GROSSE, A. V., and A. G. STRENG: AXew Deep Violet Compound (OzClF3 )n, Dioxygen Chlorine Trifluoride, 142th Meeting Am. Chern. Soc .. Sept. 1962, p. 11 N, ACS Advances in Chemistry Series 36, 159-65 (1962). 12. GIAUQUE, W. F., and J. D. KEMP: J. Chern. Phys. 6,40-52 (1938). 13. GILL, W. E.: Am. Ind. Hyg. Assoc. J. 21, 87 (1960), Ref.: CZ 1963, 7450. 14. GRAY, E. L.: AMA Arch. Ind. Health 19. 479-86 (1959). 734 Literaturnrzeichni~ G

15. GRAY, E. L., J. K. McNAMEE, and S. R. GOLDBERG: Summary Report on the Toxieity of the Vapors from RFNA, Medical Div. Res. Rept. 52, US Army Chern. Center Maryland (April 1951), unciassiL ATI 100598. 16. GRIFFITH, J. R.: Warnfarben fUr Lecks an Treibstofftanks (in Englisch), NRL Progr. Rept., PB 181068, 14-5 (1962), Ref.: Werkstoffe u. Korrosion 14: 8, 699 (1963). 17. GRACE, W. R., and F. R. HURLEY: US Pat. 3015675 (4.4.1958/2.1. 1962). 18. GRUMER, J., A. STRASSER, T. A. KUBALA, and D. S. BURGESS: Uniiberwachte diffuse Verbrennung einiger neuer fHissiger Treibstoffe (in Englisch), Fire Res ...\bstr. Rev. 3, 159-76 (1961), Ref.: CZ 1962, 14978. 19. GRAEFE, A. F.: The Lower Aliphatic Derivatives of Hydrazine, Aerojet-Gen. Corp., Rept. 674 (9 No\,. 1953) 21 p. 20. GRAEFE, A. F.: US Pat. 2962532 (14.10.1957/29.11. 19(0), Inh.: Aerojet-Gen. Corp., Ref.: CZ 1962, 15097. 21. GRIFFITH, J. R.: Leak-Indicating Paints for Rocket Fuel Tanks and Storage Area~, NRL Rept. No. 57:15 (18 Jan. 1962),5 p., AD 271001. 22. GROSSE, A. V., T. R. FLINT, et al.: Exploratory Research on High Energy Propellant Systems, Res. Jnst. Temple Univ. Philadelphia, Pa., Final Rept., 4.1. 1960-4. 3.1961 (Jan. 19(1), 59 p., Contract DA 36-034-0RD-3152, AD 270941. 23. GRAY, P., and P. G. WRIGHT: Comb. and Flame 4, 95 (1960). 24. GOGORISCHWILI, P. V., M. V. KARKARSCHWILI i L. D. TSITSISCHWILI: Sch. neorganitschesskoi Chim. 1: 2, 232-42 (1956). 25. GORDON, J. S.: Freezing Point Determinations of the System HNOa/N20 4/H20. WADC TR 54-49;'), Wright Patterson AFB (Oct. 1954). 26. GRAY, E. L., F. M. PATTON, et al.: AMA Arch. Ind. Hyg.10, 418-22 (1954). 27. GMELIN: Handbuch del' Anorganischen Chemie, Verlag Chern ie, Weinheim/Bergstr. (1935ff.). 28. GRIBOVA, E. I., et al.: Russian J. of Phys. Chern. 34, 668-72 (1960), Ref.: ARS-J. 32,176 (1962). 29. GENTHE, D.: Raumfahrtforschung 8, 77 -81 (1964). 30. GROSSE, A. V., and A. G. STRENG: A Study of Ultra High Temperatures, Temple "C'niv. Res. lnst., Phila- delphia, Tech. Note No.4 (1 Aug. 1957), USDC OTS PB 131732. 31. GRAY, L. E., S. B. GOLDBERG, and F. M. PATTON: Arch. Ind. Hyg. and Occ. Med. 10, 409-17 (1954). 32. GRAY, L. E., S. B. GOLDBERG, and F. M. PATTON: Arch. Ind. Hyg. and Occ. Med. 10, 423-5 (1954). 33. GIAUQUE, W. F .. and H. L. JOHNSTON: J. Am. Chern. Soc. 51, 2300-20 (1929). 34. GEORGE, P. D.: Ind. Engng. Chern. 46, 1709-10 (1954). 35. GREENFIELD, S.: Aircr. Engng. 30, 210-5 (July 1958). :36. GARDNER, J. B.: J. BIS 19, 230-40 (1963). 37. GIGUERE, P. A., and 1. D. Lru: Can. J. Chern. 35, 283 (1957), Ref.: CZ 1963,4281. 38. GIGUERE, P. A., and J. D. Lru: J. Am. Chern. Soc. 77, 6477-9 (1955). 39. GlAUQUE, W. F.: J. Am. Chern. Soc. 52, 4816 (1930). 40. GREY, J.: ARS-J. 30,192-3 (1960). 41. GRAHAM, R. W., R. C. HENDRICKS, et al.: Adv. Cryog. Engng. 6, 517-24 (1961). 42. GIFFORD, W. E., and P. D. FULLER: Adv. Cryog. Engng. 6, 177 -84 (1961). 43. GREENFIELD, S.: Adv. Cryog. Engng. 3, 136-48 (1960). 44. GALL, J. F.: ARS-J. 29, 95-103 (1959). 45. GALL, J. F.: Ind. Engng. Chern. 39, 262-6 (1947). 46. GUNDZIK, R. lVI., and C. E. FEILER: Corrosion of Metals of Construction by Alternate Exposure to Liquid and Gaseous Fluorine, NACA TN 3333 (Dec. 1954), 10 p. 47. GENTRE, D.: Vber die Sauerstofffluoride und ihre Verwendungsmoglichkeiten in del' Raketentechnik, DFL Trauen DLR FB 65-29 (Februar 1965), 32 Seiten. 48. GORDON, J., and F. L. HOLLOWAY: Ind. Engng. Chern. 52: 5, 63 A-64 A (1960). 49. GALL, J. F.: Ind. Engng. Chern. 49,1331-2 (1957). 50. GAYNOR, A. J.: Determination of the Physical Properties of Liquid Ozone-Fluorine Mixtures, Armour Res. Foundation, Ill. lnst. of Technology, Final Rept. ARF 3156-13, 15.8. 1960-31. 10. 1961 on Contract NASw-76, Sect. 2 (26 Oct. 1961), N-87673. ;)1. GIGUERE, P. A.: Can. J. Res. B 28, 485-91 (1950). 52. GIGUERE, P. A., and J. L. CARMICHAEL: J-. Chern. Engng. Data 7, 526-7 (1962). 53. GROSSE, A. V., and A. D. KIRSHENBAUM: J. Am. Chern. Soc. 77, 5012-3 (1955). 54. GORDON, S., and V. N. HUFF: Theoretical Performance of Liquid Hydrogen and Liquid Fluorine as a Rocket Propellant, NACA RM E 52-L 11 (1953),28 p. 55. GRANT: Lithium as a Suggested Rocket Fuel, J. Space Flight 1950/12/3-5. 56. GORDON, L. J., and J. B. LEE: ARS-J. 32, 600-6 (1962). 57. GORDON, S., and V. N. HUFF: Theoretical Performance of Lithium and Fluorine as a Rocket Propellant, NACA RM E 51-C 01 (10 May 1951), 22 p. 58. GORDON, S., and R. L. WILKINS: Theoretical Maximum Performance of Liquid Fluorine-Liquid Oxygen• Mixtures with JP-4 Fuels as Rocket Propellants, ~ACA RM E 54-H 09 (1954). Literaturverzeichnis G 735

59. GORDON, S., and V. N. HUFF: Theoretical Performance of JP-4 Fuel with a 70% Fluorine + 30% Oxygen Mixture as a Rocket Propellant, Part I: :Frozen Composition. NACA RM E 56·A 13a (1956). 60. GORDON, S., and V. N. HUFF: Theoretical Performance of JP-4 Fuel with a 70-30-Mixture of Fluorine and Oxygen as a Rocket Propellant, Part II: Equilibrium Composition (Declassified 1958), NACA RM E 56-F 04 (Oct. 1956), 49 p. 61. GORDON, S., and M. E. KASTNER: Theoretical Rocket Performance of Liquid Methane with Severall!'luo• rine + Oxygen Mixtures Assuming Frozen Composition, NACA RM E 58-B 20 (20 May 1958), 44 p. 62. GORDON, S., and K. S. DRELLISHAK: Theoretical Rocket Performance of JP-4 Fuel with Several Fluorine• Oxygen-Mixtures Assuming Frozen Composition, NACA RM E 57-G 16a (13 Nov. 1957), 62 p. 63. GORDON, S., and V. N. HUFF: Theoretical Performance of Liquid Ammonia and Liquid Fluorine as a Rocket Propellant, NACA RM E 53-A 26 (March 1953),25 p. 64. GORDON, S., and V. N. HUFF: Theoretical Performance of Mixtures of Liquid Ammonia and Hydrazine with Liquid Fluorine as Oxidant for Rocket Engines, NACA RM E 53-F 08 (29 July 1953), 43 p. 65. GORDON, S., and V. N. HUFF: Theoretical Performance of Liquid Hydrazine and Liquid Fluorine as a Rocket Propellant, NACA RM E 53-E 12 (3 July 1953), 83 p. (Declassified 24 Sept. 1956). 66. GORDON, S.: Theoretical Rocket Performance of JP-4 Fuel with Several Fluorine-Oxygen Mixtures Assu• ming Equilibrium Composition, NACA RM E 57-K 22 (Febr. 1958),69 p. 67. GUPTA, A. K.: J. Soc. chem. Ind. Lond. 68,179-83 (1949), Ref.: CA 43, 8138e (1949), vgl. auch: CA48, 6126c (1954). 68. GERSTEIN, M., G. E. McDoNALD, and R. L. SCHALLA: 4th Symp. on Comb., Williams & Wilkins, Baltimore (1953), p. 375-83. 69. GLASSMAN, I., and J. E. SCOTT: J. ARS -- Jet Propulsion 24, 386 (1954). 70. GREENE, S. A., and L. J. GORDON: Jet Propulsion 27,798-9 (1957). 71. GILBERT, M., L. DAVIS, and D. ALTMAN: Jet Propulsion 25,26-30 (1955). 72. GRIFFIN, D. N., C. F. TURNER, and G. T. ANGELOFF: ARS-J. 29, 15-8 (1959). 73. GUNTHARD, H., und E. HEILBRONNER: Helv. Chim. Aeta 31,2128-32 (1948). 74. GRAY, V. H., and T. F. GELDER: Adv. Cryog. Engng. 5.131-8 (1960). 75. GRIER, N. T.: Calculation of Transport Properties and Heat-Transfer Parameters of Dissociating Hydrogen, NASA TN D-1406 (Oct. 1962), 64 p. 76. GOTTz;-,rAN, C. F.: Adv. Cryog. Engng. 5, 289-98 (1960). 77. GLUCK, D. F., and J. F. KLINE: Adv. Cryog. Engng. 7, 219-33 (1962). 78. GORDON, S., and B. J. McBRIDE: Theoretical Performance of Liquid Hydrogen with Liquid Oxygen as a Rocket Propellant, NASA Memo 5-21-59 E (June 1959), 139 p. 79. GERSTEIN, M., O. LEVINE, and E. L. 'Y mw: ·Fundamental Flame Velocities of Pure Hydrocarbons, I: Alka- nes, Alkenes, Alkynes, Benzene and CyclohexaIw. NACA RM E 50-G 24. 80. GROSSE, A. V.: Missiles and Rockets 1957: 1,61. 81. GROSSE, A. V.: Chem. Engng. News 1956,3422 (July 1956). 82. GORDON, S., and A. R. GLUECK: Theoretical P<'rformancc of Liquid Ammonia with Liquid Oxygen as a Rocket Propellant, NACA RM E 58-A 21 (12 May 1958), 84 p., AD 160109. 83. GRAY, P., and J. C. LEE: Trans. Fara(I. Roc. ,"}O. 719-28 (1954). 84. GRAY, P., J. C. LEE, and :VI. SPENCER: Comb. and Flame 7, 315-21 (1963). 85. GRAY, P., and J. C. LEE: Rev. de l'inst. fran<,J. du petrolc et annales des comb. Iif'(. 13, 443-50 (1958). 86. GILBERT: The Hydrazine Flame, CIT-JPL Progr. Rept. 20-:H8 (May 1957). 1:3 p. 87. GRAY, P., and J. C. LEE: 7th Symp. Oil Combustion. Butterworths Scientific Pub!.. London (1959) p.61-7. 88. GREENFIELD, S.: An Experimental Evaluation of Roc-ket Propelhwt Data, in: The Chemistry of Rocket Propellants, ed. by S. R. PENNER and .J. ])l·CAR~H;. Pergamon Press. Oxford-London (19GO), p. 169 89. GRAY, P., and M. SPENCER: 9th Symp. on Comb., Academic Press, XPW York and London (1963), p.148-57. 90. GOODWIN, R. D .. D. K MILLER. H. ftI. RODER, and 1.. ~\. WEB~;R: Cryogenics 2, 81-;l (Dec. 19(1). 91. GOOD, R. J., and G. V. FERRY: Adv. Cryog. Engng. 8, 306-10 (1963). 92. GOODWIN, R. D.: J. Res. Nat. Bur. Stand. 65 C, 231-43 (1961). 93. GLASER, P. E.: Review of Cryogenie Insulation SystcmR. in: Cryogenics, Cryoelectronics and Material Research, Div. 500 of A. D. Little Tnc., Symposium Frankfurt/M., 23 June 1964, p. 21-40. 94. GOULD, J., et al.: High Energ.v Propellant Investigations, Reaction Motors Inc., Rockaway, N . .r., Rept. No. RMI-440-F. Vol. I (1 Dec. 1962), 13 p., AD 472;'>. 95. GORDON, J. S.: Jet Propulsion 27,799 (1957). 96. GARTMANN, H.: Weltraumfahrt 1951/Nr. 6/1:34--9. 97. GUNN, S. V.: J. ARS 22, 33-8 (1952). 98. GORDON, J. S.: ARS-J. 29, 530-2 (1959). 99. GRAY, P., et al.: 6th Symp. on Comb., Reinhold Publ. Corp .• Npw York (1957), p. 225-63. 100. GILBERT, M.: Mechanism and Flame Spepd for Hydrazine Decomposition, CIT-JPL Progr. Rept. 20-278 (June 1955). 101. GILBERT, M.: Comb. and Flame 2, 137 --48 (1958). 102. GILBERT, M.: Comb. and Flame 2, 149-56 (1958). 736 Literaturverzeichnis G

103. GILBERT, M.: An Approximate Treatment of Hydrazine Decomposition in a Laminar Non-Isothermal Flow, CIT-JPL Progr. Rept. 20-336 (July 1957), 25 p., AD 151870. 104. GERSTEIN, M.: ARS-J. 29, 514-6 (1959). 105. GRIFFIN, D. N., and D. R. FELLER: US Pat. 3021667 (2.6. 1952/20. 2. 1962), Inh.: Olin Mathieson C. C., Ref.: CA 67, 10098 g. 106. GRANT, A. F.: Basic Factors Involved in the Design and Operation of Catalytic Monopropellant Hydrazine Reaction Chambers, CIT-JPL Tech. Rept. 20-77 (31 Dec. 1954) (Classified). 107. GREEN, L.: Fluid-Mechanical Factors in Hybrid Rocket Combustion, AIAA Preprint 63-516 (1963). 108. GRENUS, M.: Liquid Injection for Solid Rocket Thrust Control, Space/Aero Engng. 31: 4, 59-63 (1959). 109. Gmelin-Institut: Physikalische Eigenschaften von Tetranitromethan, Peenemiinde-Archiv 124/2, Anlage 2 zu Verso Pee. Nr. 1785 geh. 110. GARDNER, D. M., and J. C. GRIGGER: J. Chem. Engng. Data 8,73-4 (1963). 111. GRAY, P., and G. T. ROGERS: Trans. Farad. Soc. 00, 28-36 (Jan. 1954). 112. GRAY, P., and A. D. YOFF~J: J. Chem. Soc. 1960, 3180-5 (May 1950). 113. GREENE, S. A., and L. J. GORDON: Jet Propulsion 27,1261-2 (1957). 114. GOULD, R. F. (Editor): Borax to Boranes, ACS Advances in Chemistry Series Vo!' 32, Washington 1961. 115. GAKLE, P. S., and S. TANNENBAUM: J. Am. Chem. Soc. 77, 5289-90 (1955). 116. GALBRAITH, H. J., and J. F. MASI: Kinetics of the Pyrolysis, Hydrolysis and Oxidation of Boranes and Alkyl Boranes, Callery C. C., Rept. CCC-l024-TR-150 (7 Nov. 1955), 28 p., AD 130712. 117. GAMMON, B. E.: Preliminary Evaluation of the Air and Fuel Specific Impulse Characteristics of Several Potential Ram-Jet Fuels III: Diborane, Pentaborane, Boron and Boron-Octene-Slurries, NACA RM E 51-D 25 (1951). 118. GAMMON, B. E., R. S. GENCO, and M. GERSTEIN: A Preliminary Experimental and Analytical Evaluation of Diborane as a Ram-Jet Fuel, NACA RM E 50-J 04 (22 Dec. 1950),39 p. 119. GOULD, J. R., et a!.: US Pat. 3106584 (3. 6.1957/8.10.1963), Ref.: CA 60, 3004e (1964). 120. GALLAGHAN, J., and B. SIEGEL: J. Am. Chem. Soc. 81, 504 (1959). 121. GROVES, K. 0.: US Pat. 3140317 (3.3.1961/7.7.1964), Inh.: Dow Chem. Co., Ref.: CA 61, 9402d (1964). 122. GRAY, P., J. C. LEE, and M. SPENCER: Comb. and Flame 7, 315-21 (1963). 123. GROSS-GRONOMSKI, L.: Comb. and Flame 7, 217-26 (1963). 124. GROSSE, A. V., and A. G. STRENG: US Pat. 2992540 (13. 11. 1959/18.7.1961). 125. GAINES, J. M.: US Pat. 2962449 (19.11. 1956/29. 11. 1960), Inh.: Union Carbide Corp., Ref.: CZ 1962, 4297. 126. GORDON, J. S.: Effect of Composition on Heat of Formation for Fuming Nitric Acid, Wright Air Dev. Center, Wright Patterson AFB, WADC Tech. Rept. 56-21 (Feb. 1956), 11 p., AD 97196. 127. Anonym: Liquid Hydrogen Technology, General Dynamics/Astronautics, San Diego, Calif. Rept. AE-62- 0774 (Sept. 1962),313 p., N 63-10128. 128. GOODWIN, R. D., et a!.: Adv. Cryog. Engng. 9, 234-42 (1964), N 64-21843. 129. GRAVES, G. A., and J. R. STREETMAN: Neutron Contributions to LH2 Propellant Heating, Proc. of Nuc!. Propulsion Conf., Monterey, Calif., Atomic Energy Commision (15-17 Aug. 1962), p. 29-34, N 63- 22305, N 63-22301. 130. GUNNING, H. E., et a!.: Studies on Hydrazine, II!. Inst. of Techno!', Chicago, Status Rept. (15 Dec. 1953), 7 p., AD 29000. 131. GILLILAND, A. A.: J. Res. Nat. Bur. Stand. 66 A, 447 -9 (1962). 132. GILLILAND, A. A., and W. H. JOHNSON: J. Res. Nat. Bur. Stand. 65 A, 67 (1961). 133. GODFREY, N. B.: US Pat. 3055173 (11. 8. 1959/25.9. 1962), Inh.: Jefferson Chem. Co., Ref.: CA 68. 406f (1963). 134. GREENE, S. A..: US Pat. 3117415 (2.4.1959/14.1.1964), Inh.: North Am. Av. Inc., Ref.: CA 60,9093 (1964). 135. GRAY, P., and M. SPENCER: Comb. and Flame 6,337-45 (1962). 136. GRAY, P. D.: J. Space cr. and Rockets 1, 340-2 (1964). 137. GALE, H. W., and P. C. MOEDT: Design and Testing of a Pyrogen Igniter for a L02/LH"-Rocket Engine, Space Systems Div., AFSC, Inglewood, Calif., Rept. No. SSD TDR 62-201 (Dec. 1962). 138. GRELECKI, C. J., and S. TANNENBAUM: ARS-J. 32, 1189-94 (1962). 139. GOSNELL, R. B.: Adv. Cryog. Engng. 9, 139-45 (1964). 140. GRAHAM, R. W., et a!.: Analytical and Experimental Study of Pool Heating of Liquid Hydrogen over a Range of Accelerations, (Feb. 1965),54 p., NASA TN D·1883 (1965). 141. GRAIUM, R. W., R. C. HENDRICKS, and R. C. EHLERS: Internat. Adv. Cryog. Engng.10 MU, 342-52 (1965). 142. GILBEAU, J. J., D. L. MARTINDALE, and K. R. BURTON: Adv. Cryog. Engng. 10, 428-32 (1965). 143. GRAY, V. H., et a!.: Bonded and Sealed External Insulations for Liquid-Hydrogen-Fueled Rocket Tanks During Atmospheric Flight, NASA TN D-476 (Oct. 1960),51 p. 144. GRAHAM, R. W., and R. C. HENDRICKS: A Study of the Effect of Multi-g Accelerations on Nuclcate Boiling Ebullition; NASA TN D-1196 (1963). 145. GORDON, J. S.: Effect of Composition on Heat of Formation for Fuming Nitric Acid, W ADC Techn. Rept. 56-21, AD 97196 (Febr. 1956), 11 p. Literaturverzeichnis H 737

146. GRELECKI, C. J., and W. CRUIOE: The Thermal Reactions of Some Advanced Solid Oxidizers, Am. Chern. Soc., Symposium on Advanced Propellant Chemistry, Detroit (1965), Preprint of Papers Vol. 9, No.1; p. 80-9, vgl. R. F. GOULD (Ed.), Advanced Propellant Chemistry, ACS Series Vol. 54, Washington (1966). 147. GOLDBAUM, G. C., and J. B. DOUGLASS: AIAA J. 4, 570-6 (1966). 148. GOULD, J. R.: US Pat. 3150482 (16.5. 1957/29.9. 1964), Thiokol Co., Ref.: CA 62, 1506e (1965). 149. GORTSEMA, F. P., and R. H. TOENISKOETTER: Inorg. Chern. 0, 1925-7 (1966). 150. GUERTIN, J. P., K. O. CHRISTE, and A. E. PAVLATH: Inorg. Chem. 0, 1921-4 (1966). 151. GEORGE, J. W., in: Progress in Inorganic Chern., Vol. 2, Interscience Publ., New York (1960), p. 34-9. 152. GEERY, E. L., and W. R. THOMPSON: Heat-Transfer Characteristics of Cryogenic Hydrogen at High Heat Fluxes and Pressures from 800 to 1200 psia, AIAA-Paper 66-581 (1966). 153. Anonym: Atmosphcric Diffusion of Fluorine from Spills of FLOX Mixtures, General Dynamics/Convair, San Diego, Calif., Summary Rept. 5, NAS 3-3245, GDC-DDB-66-001, NASA CR-54926 (10 May 1966) 251 p., N 66-27229. 154. GARLE, P. S.: Contamination Control in Missile Systems, Material Protection 0,65-7 (1966), Ref.: CA 64, 7959 (1966). 155. GIFT, R. D., et al.: Clogging of Manifolds with Evaporatively Frozen Propellants, AIAA-Paper 66-540. 156. GREEN, J., N. B. LEVINE, and W. R. SHEEHAN: Elastomers for Nitrogen Tetroxide Application, AIAA Paper, Ref.: Int. Aerospace Abstracts 6, 2370 (1966), A66-28015. 157. GATTI, R., R. L. KRIEGER, J. E. SIORE, and H. J. SCHUMACHER: J. Inorg. Nucl. Chern. 28, 655 (1965). 158. GEORGE, H.: Properties of Selected Rocket Propellants, The Boeing Co., Seattle, Wash., Document D2- 11677 (1963), AD 444642. 159. GAYLE, J. B., et al.: Preliminary Investigation of Blast Hazards of RP-l/LOX and LH2/LOX Propellant Combinations, NASA TM X-53240 (9 April 1965) 35 p., N65-23667. lGO. GREEN, J., N. B. LEVINE, and R. C. KELLER: Chemically Resistant Materials for Use in Positive Expul• sion Devices, Chern. Engng. Progress 60, Symposium Series No. 52, p. 45-53 (1964), A65-15614. Hi1. GROESBECK, W. A.: Design of Coast-Phase Propellant Management System for Two-Burn ATLAS-CEN• TAUR AC-8, NASA TM X-1318 (Nov. 1966) 21 p.

H

1. HOFFMAN, C. J., and R. G. NEVILLE: Chern. Rev. 62,1-18 (19G2). 2. HODGE, H.: Toxicity of Oxygen Fluoride, Pharmacology Rept. 47B, Univ. of Rochester (1945). 3. HANZLICK, P., and 1. TARR: J. Pharmacol. 14. 221 (1919). 4. HORN, H. 1.: Chlorine Trifluoride, US Army Chemical Center, Md., MCL Rept. 22 (Nov. 1953). 5. HORN, H. I.: Acute Inhalation Toxicity of Chlorine Trifluoride, Hazelton Labs., Falls Church, Va., Progr. Rept. to Chemical Corps Procurement Agency (20 Nov. 1953). G. HENDEL, F.J.: Storable Hybrid Propulsion Systems, ARS Preprint 12G8-60 (July 19GO). 7. HUBER, F.: Beitrage zur Elektrofluorierung stickstoffhaltiger Verbindungen, Diss. TH Aachen 1959. 8. HILTON, A. R., et al.: J. Chern. Phys. 34, 1137 -41 (19Gl). 9. HIRATA, T., S. MORROW, and A. YOUNG: Inorganic Chemistry of the Oxygen Subfluorides, Reaction Motors Div. of Thiokol, First Quart. Progr. Rept. RMD-5009-Q 1 (15 Aug. 1962), N 62-16968. 10. HALPERN, C.: J. Res. Nat. Bur. Stand. A 60,513 (1961). 11. HUFF, V. N., and S. GORDO:"f: Theoretical Performance of Liquid Oxygen Fluoride as Oxidizer in Rocket Engines, Part I: Ammonia, NACA RM F, 51-L 11 (FebI'. 1952), 24 p., Part II: Hydrazine, NACA RM E 52-G 09 (Sept. 1952),20 p., Part III: Ammonia and Hydrazine, NACA RM E 52-H 14 (Oct. 1952), 15 p. 12. HENDERSON, U. Y., and P. L. GOODFRIEND: Investigation of the Dissociation Chemistry of NF2-Com- pounds, Texaco Exp. Inc. Rept. EXP-223: TM 1423 (May 1963), 13p., N 63-18103. 1:1. HARMONY, M. D., and R. J. Mn~Rs: J. Chern. Phys. 37, G3G-41 (1962). 14. HATT, N.: Organic Synthe~es. Collective Vol. II, p. 211. 15. HORVITZ, D.: US Pat. 2802031 (6.8.1957), Inh.: Metalcctro Corp. 16. HERICKES, J. A .. U. H. DANNO:"f, and M. G. ZABETAKIS: Determination of Safety Properties of UDMH, US Bur. of }Iines, Rept. Investigation No. 5635 (1960), Ref.: CZ 1963,12263. 17. HAGGERTY, W., M. MARKELS, and H. FRIEDMAN: Feuerloschuntersuchungen an Branden mit Hydrazin und unsymm. Dimethylhydrazin (in Englisch), Fire Res. Abstr. Rev. 3,133-50 (1961), Ref.: CZ 1962, 14979. 18. HORVITZ, D.: US Pat. 2954283 (2.12.1957/27.9. 19GO), Inh.: Nat. Distillers and Chern. Corp., Ref.: CA 00, 6868a (1961); CZ 1962, 6272. 19. HARSHMAN, R. C.: Jet Propulsion 27,398-400 (1957). 20. HORVITZ, D.: US Pat. 3013076 (22. 10. 1956/12. 12. 1961), Inh.: Nat. Distillers and Chern. Corp. 21. HAURDEN: US Pat. 2818379 (31. 12. 1957), lnh.: Olin Mathieson C. C. 22. HENNINGS, F. G., D. J. LADANYI, and J. H. ENDERS: Ignition of Ammonia and Mixed-Oxides-of-Nitrogen in 200 Pound Thrust Rocket Engines at HiO°F. NACA RM E 54-C 19 (May 1954), 18 p.

Dadieu-Damm-Schmidt. Hakctentreibstoffe 47 738 Literaturverzeichnis H

23. HAST, D. R.: Ultra-Low Pressure Liquid Propellant Space Propulsion System, Wright Air Dev. Center, WADC TN 58-218 (June 1958). 24. HAGGERTY, W. E., M. MARKELS, and R. FRIEDMAN: Extinguishment Studies of Hydrazine and UDMH Fires, Am. Chem. Soc., Div. of Fuel Chem., Preprint 1, 123-39 (1961). 25. HALBIG, J.: Chem. Engng. 68: 26, 108 (1961), Ref.: Werkstoffe und Korrosion 14: 5, 389 (1963). 26. HALLER, J. F., and T. H. DEXTER: US Pat. 2805129 (3. 9. 1957), Inh.: Olin Mathieson C. C., Ref.: CA 52, 674a. 27. HALLER, J. F.: US Pat. 2841543 (1. 7.1958), Inh.: Olin Mathieson C. C. 28. HARNISCH, H., G. HEYMER und E. SCHALLUS: Chem. Ing. Technik 35,7 -10 (1963). 29. HICKLING, A., and G. R. NEWNS: J. Chem. Soc. [Lond.] 1961, 5177-91. 30. HEINRICH, G.: DB Pat. 1101377 (16.12.195919.3.1961), Osterr. Pat. 214899 (14.12.1959/25.4. 19tH), Ref.: CZ 1962,17884; Brit. Pat. 890240 (15.12.1959/28.2.1962), Rcf.: CZ 1963, 2199; US Pat. 3063806 (15.2.1959/13. 11. 1962), Inh.: Farbenfabriken Bayer AG. 31. HIEBER und WOERNER: Z. f. Elektrochemie 40, 252 (1934). 32. HUGHES, A. M.: J. Am. Chem. Soc. 61, 2639-42 (1939). 33. HANRATTY, T. J., and J. N. PATTISON: Ind. Engng. Chem. 43, 1113 (1951). 34. HATCHER, J. B., and D. R. BARTZ: High Flux Heat Transfer to JP-3 and RFNA, ARS Preprint 119-51 (1951), auch erschienen als JPL External Publication 119 (Nov. 1951). 35. HORN, H. J., and R. J. WErn: AMA Arch. Ind. Health 12, 515 (1955); 13, 340 (1956). 36. HALL, E. N.: Ozone-Fluorine, in: Advanced Propulsion Systems, Edited by M. ALPERIN and G. P. SUTTON, Pergamon Press, London-New York 1959, p. 185-9. 37. HOELZGEN, H. J.: Weltraumfahrt 2,89-91 (1951). 38. HERSH, C. K., et al.: ARS-J. 30, 264-6 (1960). 39. HERSH, C. K.: Production and Properties of Liquid Ozone and Liquid Ozone-Oxygen Mixtures, A Review, in: Liquid Rockets and Propellants, ARS Progress Series Vol. 2, Ed. : L. E. BOLLINGER et aI., Acade• mic Press, New York (1960), p. 427-44. 40. HERSH, C. K., A. W. BERGER, and C. BROWN: Physical Properties of Liquid Ozone-Oxygen Mixturps: Dansity, Viscosity and Surface Tension, Am. Chem. Soc. Advances in Chemistry Series Vol. 21, Washington 1959, p. 22-7. 41. HILL, W. H., and J. L. SVrnBELY: AMA Arch. Ind. Hyg. and Occ. Med. 10, 69-76 (1954). 42. HORN, H. J.: AMA Arch. Ind. Hyg. Occ. Med.10, 213-22 (1954). 43. HERZFELD, K. F.: 7th Symp. (internat.) on Combust., Butterworths Sci. Publ., London (1959). p.27-33. 44. HINCKLEY, R. B., and R. E. KENDALL: A Large-Scale System for Servicing Cryogpnic Fluids. ARS-Pre- print 815-59. 45. HART, A. B.: Nature 163, 876-77 (1949); 193,1175 (1962). 46. HUCKABA, C. E., and F. G. KEYES: J. Am. Chem. Soc. 70,2578 (1948); 72, 5324 (1950). 47. HAEUSELER, E.: Explosivstoffe 1: 6/7, 64-8 (1953). 48. HENDRICKS, R. C., et al.: Experimental Heat Transfer and Pressure Drop Characteristics of Liquid Hydro• gen Flowing Through a Heated Tube, NASA TN D-765 (May 1961), 62 p. 49. HENDRICKS, R. C., et al.: Correlation of Hydrogen Heat Transfer in Boiling and Supercritical Pressure States, ARS-Preprint 1710-61. 50. HENDRICK8, R. C., et al.: ARS-J. 32, 244-52 (1962). 51. HEUSE und OTTO: Ann. Phys. 9, 486 (1931). 52. HURDEN, D.: J. BIS 18, 192-8 (1961-62) 53. HUNT, M. S., and B. G. WHITE: J. BIS 18, 199-203 (1961-62). 54. HOLTEN, D. C.: Adv. Cryog. Engng. 6, 499-508 (1961). 55. HUMPHREY, J.C.: Adv. Cryog. Engng. 6,281-92 (1961). 56. HEIDT, L. J., and V. R. LANDRI: J. Chem. Phys. 41, 149-53 (1964). 57. HANSEN, O. A.: Adv. Cryog. Engng. 2, 75-82 (1960). 58. HILSENRATH, J., et al.: Tables of Thermodynamic and Transport Properties (Air, Ar, CO 2, CO, H 2, N 2• O2, H 20), Pergamon Press, Oxford-London-New York-Paris (1960). 59. HATCHER, J. B.: High Flux Heat Transfer and Coke Deposition of JP-3 FuellVIixture, CIT-JPL 20-157 (Nov. 1951) und ARS-Preprint 46-51. 60. HASZELDINE, R. N., and A. G. SHARPE: Fluorine and Its Compounds, J. Wiley & Sons Inc., New York 1951. 61. HAASE, G.: Fliissiges Fluor als Raketentreil;>stoff und erganzende Bemerkungen iiber Fluor-Triebwcrke, Vortrag VOl' dem WGL-AusschuB fiir Treibstoffe am 28. 3. 1962 in Miinchen, Ref.: Explosivstoffe 11, 128-9 (1963). 62. Hu, J. H., D. WHITE, and H. L. JOHNSTON: J. Am. Chern. Soc. 75, 5642-5 (1953). 63. HAENDLER, H. M., et al.: J. Am. Chern. Soc. 76, 2178-9 (1954). 64. HOWARD, O. H., and C. W. WEBER: AMA Arch. Ind. Health 19,355 (1959). 65. HERTEL, W.: Uber Raketentreibstoffe, Schriften dpr dt. Akad. d. Luftfahrtforschung, Heft 1071/43 (194:1), S.47-53. Literaturverzeichnis H 739

66. HAPPEL, J., and C. J. MARSCH: Chem. Engng. Progr. 54: 6, 60-4 (1958). 67. HENDERSON, U. V.: Mechanism of the Autodecomposition of Liquid Acetylenic Monopropellants, Experi• ment Inc. TM 1152 (Jan. 19(0), 13 p. 68. HENDERSON, U. V., L. E. LINE, et al.: Mechanism of Autodecomposition of Certain Liquid Acetylenic Compounds, Experiment Inc. TP 140-EXP 259 (Dec. 1958), 14 p. 69. HINES, W. S., and H. WOLF: ARS·J. 32, 361-6 (1962). 70. HOPPE, R, et al.: Angew. Chem. 74, 903 (1962). 71. HUFF, V. N., C. S. CALVERT, and V. C. ERDMANN: Theoretical Performance of Diborane as a Rocket Fuel, NACA RM E 8-1 17a, 31 p. 72. HUFF, V. N., and S. GORDON: Theoretical Performance of JP-4 Fuel with Mixtures of Liquid Ozone and Fluorine, NACA RM E 56·K 14 (28 Jan. 1957), 22 p. 73. HARDIN, M. C., and A. 1. MASTERS (Rcaction Motors Inc., Indianapolis): The Use of Lithium as a Rocket Propellant, Combustion Inst., Wcstern States Section, Paper WSS/CT 61-9 (1961), 9 p., Ref.: CA 58, 402h (1963). 74. HESS, L. G., and V. V. TILTON: Ind. Engng. Chern. 42, 1251-8 (1950). 75. HECKERT, W. H., and E. MACK: J. Am. Chem. Soc. 51, 2706-17 (1929). 76. HOLZL, R A.: US Pat. 2993768 (25.7. 19(1), Inh.: Sundstrand Corp., Ref.: CA 50, 27893a. 77. HUNTER, B. J., et al.: Adv. Cryog. Engng. 5, 146-56 (1960). 78. HERZBERG, F.: Adv. Cryog. Engng. 5, 526-32 (1960). 79. HERBERT, L. S., and H. ZIEBLAND: Heat Transfer and Performance Studies of the Propellant Combination Gaseous Hydrogen and Gaseous Oxygen, Part I: Some Computed Thermodynamic Data for 10, 30, 60 and 100 at Combustion Pressure, Expl. Res. and Dev. Establ., Gt. Britain, Rept. 4jRj58, XR 750/2:~. JSRP 581699 (Nov. 1958), AD 209816. 80. HERSCH, M.: Combined Effect of Contraction Ratio and Chamber Pressure on the Performance of a Gaseous Hydrogen and Liquid Oxygen Combustor for a Given Propellant Weight Flow and Oxidant: Fuel Ratio, NASA TN D-129 (Feb. 1961), 13 p. 81. HEIDMANN, M. F.: Combustor Performance With Various Hydrogen-Oxygen Injection Methods in a 200 Pound-Thrust Rocket Engine, NACA RM E 58-E 51 (Sept. 1958), 45 p. 82. HEIDMANN, M. F., and C. M. AUBLE: Injection Principles from Combustion Studies in a 200-Pound• Thrust Rocket Engine Using Liquid Oxygen and Heptane, NACA RM E 55-C 22 (7 June 1955), 55 p., Declassified 19 March 1957. 83. HUFF, V. N., and A. FORTINI: Theoretical Performance of JP-4 Fuel and Liquid Oxygen as a Rocket Propellant, Part I: Frozen Composition NACA RM E 56-A 27 (17 April 1956), 35 p., Part II: Equi• librium Composition, NACA RM E 56-D 23 (7 Sept. 1956), 47 p. 84. HUTCHEON and GREEN: Calculated Data for the Combustion of Liquid Oxygen with Water Diluted Alco• hols and Paraffine in Rocket Motors, Gr. Brit. Aeron. Res. Council, Rept. and Memo 2572 (Oct. 1947), 13 p. 85. HAMMOND, J. A.: Explosive Reaction of Pentaborane-Oxygen Mixtures, Olin Mathieson Tech. Res. Rept. HEF 153, Contract AF 33(600)33920 (19 Aug. 1958), 109 p., AD 207044. 86. HUDDERS, R. S., C. J. DORF, and A. H. HOLCOMBE: Adv. Cryog. Engng. 8, 461-0 (1963). 87. HAUSER, R L., and W. F. RUMPEL: Adv. Cryog. Engng. 8, 242-50 (1963). 88. HENNINGS, G., and G. MORRELL: Low-Temperature Chemical Starting of a 200 Pound Thrust JP-4/~itric Acid Rocket Engine Using a Three-Fluid Propellant Valve, NACA RM E 55-E 04 (30 June 1955), 25 p., N 63-12540. 89. HENNINGS, G.: Preliminary Investigation of a Chemical Starting Technique for the _\cid-Gasoline Rocket Propellant System, NACA RM E 52-K 21 (Jan. 1953), 23 p. 90. HALLIDAY, K. C.: Ignition of Fuel with Nitric Acid, ARS-Preprint 80-52. 91. HALLIDAY, K. C.: US Pat. 2949006 (16.8. 19(0), Inh.: US Army, Ref.: CA 55, 4964c. 92. HAMILTON. B. R: US Pat. 2994191 (1. 8.19(1), Inh.: Phillips Petrol. Co., Ref.: CA 55, 27891a. 93. HURDEN, D.: Raketentechnik u. Raumfahrtforschung 3,9-13 (1959). 94. HENDERSON, U. V., and H. P. WOODS: Combustion of Elemental Boron, Texaco Exp. Co., Rept. TM 1274, EXP 223 (1 Aug. 19(1),9 p., AD 265311. 95. HENDEL, F .•J., and E. H. CAVECCHE: Chem. Engng. 67: 11,93-6 (1960). 96. HARDIN, ]\II. C., A. I. MASTERS, and L. E. TOOLE: ARS-J. 32,1292-4 (1962). 97. HARPER, S. A., and W. E. GORDON: Detonation Properties of Ozone, in: Ozone Chemistry and Technology, Am. Chern. Soc., Advances in Chemistry Series No. 21, Washington (1959), p. 28-37. 98. HERSH, C. K., G. lVI. PLATZ, and R J. SWEHLA: J. Phys. Chern. 63,1968-9 (1959). 99. HALL, A. R, and H. G. WOLFHARD: Trans. Farad. Soc. 52,1520-5 (Nov. 1956). 100. HIROSHI-TsUJI: Entztindung und Flammenstabilisierung cines Stroms von brennbaren Gasgemischen (N2H 4 und CHaNHNH2) dUfch cine heiBe Dtise (in Englisch), Aeron. Res. Inst. Univ. Tokyo, Japan, Rept. 26, No. 357, p. 119-36 (1960), Ref.: CZ 1963, 1924. 101. HAUEL, A. P.: Canad. Pat. 635282 (20. 10. 1959/23. 1. 19(2), Inh.: Engelhard Ind. Inc., Newark, Ref.: CZ 1963,17083. 102. HORNER, J. W.: US Pat. 2988430 (13. G. 19(1), Inh.: Ramo Wooldridge Inc., Ref.: CA 55, 21592d.

47* 740 Literaturverzeichnis H

103. HENDERSON, U. V.: Mechanisms of the Autodecomposition of Liquid Acetylenic Monopropellants, Experi• ment Inc., a) Progress Rept. Jan.-June 1958, Rept. TM·l039·EXP·259 (1 July 1958), 9 p., AD 202214, b) Quart. Progr. Rept. July-Sept. 1958, Rept. TM-l059-EXP·259 (1 Oct. 1958), 10 p., AD 210231, c) Quart. Progr. Rept. Oct.-Dec. 1958, Rept. TM-l075-EXP-259 (1 Jan. 1959), 7 p., AD 225220, d) Quart. Progr. Rept. Apr.-June 1959, Rept. TM-1102·EXP-259 (1 July 1959), 9 p., AD 220088. 104. HENDERSON, U. V., H. P. WOODS, and G. POPLIN: The Combustion of Elemental Boron with Fluorine; Texaco Experiment Inc., Final Rept. EXP 233, TEI-TP-209 (3 Feb. 1964), 23 p., AD 430909, N64·16444. 105. HAUSER, T. J., and M. V. PECK: Research in Hybrid Combustion, AlAA-Prcprint 63·510 (1963). 106. HENDERSON, U. V., H. P. WOODS, and G. POPLIN: The Combustion of Elemental Boron With Fluorine, AIAA-Preprint 63-492 (1963). 107. HILLENBRAND, L. J., and M. L. KILPATRICK: J. Chem. Phys. 21, 525-35 (1953), vgl. auch J. Chem. Phys. 19, 381 (1951). 108. HAGER, K. F.: Ind. Engng. Chem. 41, 2168-72 (1949). 109. Hummel Chem. Comp.: Tetranitromethane, Techn. Data Sheet 104, Hummel Chem. Comp., 90 West Street, New York 6. 110. HENRY, R. A., and C. W. TAIT: US Pat. 3070473 (1. 11. 1957/25. 12. 1962), Ref.: CA 58, 6639f. (1963). 111. HANNUM, J. A.: US Pat. 2537526 (9. 1. 1951), Inh.: Borg-Warner Corp., Ref.: CA 45, 3147 (1951); US Pat. 2538516 (16.1.1951), Ref.: CA45, 2653e (1951); US Pat. 2542193 (20.2.1951), Ref.: CA 45,10545 (1951); US Pat. 2559071 (3.7.1951), Ref.: CA 45,9836 (1951). 112. HICKS, J. A., and D. P. NEEDHAM: The Low Pressure Decomposition Flamc of Ethyl Nitrate, Part 1: Chemical Kinetics, Grt. Brit. Expl. Res. and Dev. Establ., ERDE Rept. 23fR/59, JSRP 591363 (8. Dec. 1959), AD 229230. 113. HERRICK, C. S., et aI., Ind. Engng. Chcm. 52, 105-12 (1960). 114. HAUGH, J. F.: Pyrolysis of Decaborane, Delware Univ., Newark, Tech. Res. Rept. OMCC-HEF 57, Sub- contract Olin Mathieson C. C. (June 1957), 70 p., AD 155442. 115. HILL, W. H., et al.: Ann. Ind. Hyg. Assoc. J. 21, 312-5 (1960), Ref.: CZ 1963, 17435. 116. HATTORI, K., et aI.: US Pat. 3038943 (12. 10. 1959/12.6. 1962), Inh.: Callery C. C. 117. HUNT, M. W., and R. M. TILLMAN: US Pat. 3057763 (10.8.1959/9.10.1962), Inh.: Continental Oil Co., CA 58, 2320 (1963). 118. HIBBARD, R. R., and G. L. DUGGER: Fundamental Flame Velocity, Heat of Combustion and Spontaneous Ignition Temperature of Dimethylaminodiborane, NACA RM E52-L23 (19 Dec. 1956), 6 p. (De• class. from Confidential 17 July 1958). 119. HALFORD, F. B., A. V. CLEAVER, and W. N. NEAT: DB Pat. 1070882 (10. 12.1959), Inh.: De Havilland Eng. Co., Ref.: CA 55, 14918i. 120. HAWTHORNE: Aviation Age 1952,36-7 (April 1952). 121. HORVITZ, D.: US Pat. 3129215 (14.5. 1958/14. 4. 1964), Inh.: fmc Corp., Ref.: CA 60, 15874f. (1964). 122. HARRJE, D. T.: A Study of Liquid-Oxygen Boil-Off, CIT-JPL Memo 20-138 (15 Dec. 1956), 13 p., AD 124622. 123. HENDERSON, W. P.: The Storage and Handling of Liquid Propellants for Rockets and Guided Missiles, Army Chem. CJnter, M

134. HAMLIN, A. G., G. IVESON, and T. R. PHILLIPS: Anal. Chem. 35, 2037-44 (1963). 135. HERSH, C. K., and A. J. GAYNOR: Physical Properties of the Liquid Ozone-Fluorine System, Am. Chem. Soc., Symposium on Advanced Propellant Chemistry 1965, Preprints of Papers Vol. 9, No.1, p.128-35. 136. HURST, G. L., and S. 1. KHAYAT: Hydrolysis of the Nitrogen Fluorides, Am. Chem. Soc., Symposium on Advanced Propellant Chemistry 1965, Preprints of Papers Vol. 9, No.1, p. 197-210. 137. HERRING, R. N., and P. L. BARRICK: Internat. Adv. Cryog. Engng. 10 MU Supplement, 151-9 (1965). 138. Hsu, A. C. T., and C. McKINLEY: Chem. Engng. Progr. 06: 2, 80-4 (Feb. 1960). 139. HERTZ, J., and J. F. HASKINS: Adv. Cryog. Engng. 10, 163-70 (1965). 140. HAMMEL, E. F.: Critical Phenomena in Fluids, Institut International du Froid, Grenoble (France), (Juin 1965), Preprint. 141. HALL, L. A.: Thermal Conductivity of Ten Cryogenic Liquids - A Bibliography (H2, O2, Fz u. a.), Nat. Bur. Stand., NBS-7684, NASA CR-50292 (15 Apr. 1963),21 p., N65-17283_ 142. HARPOOTHIAN, E.: The Production of Large Tanks for Cryogenic Fuels. Douglas Paper No. 3155, vor• getragen am 12. 11. 1964 bei der Deutschen Gesellschaft fUr Raketentechnik und Raumfahrt, Miinchen. 143. HOWELL, J. R., and M. K. STRITE: Heat Transfer in Rocket Nozzles Using High Temperature Hydrogen Propellant, AIAA Paper 65-557. 144. HOLLEY, CH. E., and J. F. LEMMONS: The Preparation of the Hydrides of Mg and Be. Los Alamos Sc. Lab., Rept. LA-1660 (1954), 72 p. 145. HEAD, E. L., C. E. HOLLEY, and S. W. RABIDEAU: J. Am. Chem. Soc. 79 (1957), 3687-9. 146. HAUSNER, H. W. (Ed.): Beryllium, Its Metallurgy and Properties, Berkeley 1965, 300 p. 147. HAWS, J. L., and D. G. HARDEN: J. Spacecraft and Rockets 2: 6, 972-4 (1965). 148. HINES, W. S., and J. D. SEADER: Study of an Endothermic Fuel for the Atlas Rocket Motor, Rocketdyne Report RM 1105/362, Contract AF 04(611)9721 (Dec. 1964),24 p., AD 454771, N65-17476. 149. HElDMAN, M. F.: Oscillatory Combustion of a Liquid-Oxygen Jet with Gaseous Hydrogen, NASA TN D-2753 (March 1965), 26 p., N65-19846. 150. HOFFMAN, C. J., and R. G. NEVILLE: Chem. Rev. 62,1-18 (1962), 183 Refs. 151. HETHERINGTON, G., and P. L. ROBINSON: J. Chem. Soc. 1955, 2230 (1955). 152. HETHERINGTON, G., and P. L. ROBINSON: "Nitryl Fluoride and Nitronium Compounds", in: Recent Aspects of the Inorganic Chemistry of Nitrogen, The Chem. Soc., London, Spec. Publ. 10, p. 23-32 (1957). 153. HOLMSTEAD, G. M.: Freezing of Cryogenic Liquids When Expanded to Pressures Below the Triple Point Pressure, General Dynamies/Astronautics GDA, A 63-0832, NASA CR-60325 (Aug. 1963), 63 p., N 66-29346. 154. HINES, W. S.: Rocketdyne Rept. R-2059 (24 Aug. 1959). 155. HANNUM, N. P., and H. E. SCOTT: NASA TM X-52251 (1966), N 67-11334. 156. HURD, D. T.: Chemistry of the Hydrides, J. Wiley & Sons, New York (1952) 231 p. 157. HOLLYWOOD, L. P., T. R. METZ, and R. N. PORTER: Storage Tests of Nitrogen Tetroxide and Hydrazine in Aluminum Containers, JPL TR 32-1039, NASA CR-81294 (Jan. 1967) 27 p., N67-16559. 158. HOUSE, P. A.: Resilient Seal Materials for Liquid Rocket Propellants, Society of Aerospace Material and Process Engineers, 6th ~at. flymposium, Seattle, \Vash. 1963, Vol. 2, A65-11167. 159. HERNANDEZ, H. P., et al.: Adv. Cryog. Engng. 12, 174-217 (1967). 160. HASTINGS, G. A., et a!.: Literature of Low G Propellant Behavior, Lockheed Miss. and Space Co., Sunny• vale, LMSC-A 835805, NASA CR-65539 (Sept. 1966), N66-38975. 161. HESS, F. D.: The Determination of Water in Nitrogen Tetroxide, Aerospace Corp., EI Segundo, Calif., TR-1001(221O-10)-6, SSD-TR-67-106 (June 1967) 22 p., AD 655071, N67-35692. 162. HERSCH, M., and E. J. RICE: Gaseous Hydrogen-Liquid Oxygen Rocket Combustion at Supercritical Chamber Pressures, NASA TN D-4172 (Sept. 1967) 31 p .. N67-35666. 163. HURD, S. E., and E. Y. HARPER: J. of Spacecraft and Rockets 5, 220 (1968).

I

1. IVESON, G.: Analysis of Corrosive Gases by Gas-Liquid-Chromatography (CIFa, HF, UF6), United Kingdom Atomic Energy Authority Rept. 82, 1-15 (1960), Ref.: CA 55, 6058a (1961). 2. International Critical Tables of Numerical Data, Physics, Chemistry and Technology, Vo!'l (1926)ff., Edited by E. W. WASHBURN, McGraw-Hill Book Co., Inc., New York. 3. ISHAGHOFF, 1., and J. M. CANTY: Adv. Cryog. Engng. 9, 46-51 (1964). 4. IRMSCHER: Acetylen als Raketentreibstoff, Forschungsreihe der Nordwestdeutschen Ges. f. Weltraumfahrt, Nr.8 (Sept. 1952). 5. ISAKSON, V. E., C. D. HOLBEN, and C. V. FOGELBERG: Adv. Cryog. Engng. 3, 232-7 (1960). 6. Ikoku, C., et al.: Autoxidation of UDMH, NOTS China Lake (Sept. 1965), NOTS-TP-3903, N 66-15018, AD 622785. 7. Illinois Institute of Technology Research Institute: "Design Datafor Pressurized Gas Systems", Vol. XV, lIT Research Institute, Chicago, Ill., Contract NASA 7-388 (March 1966), 15 Volumes. 742 Literaturverzeichnis J

J 1. JARRY, R. 1., and H. C. MILLER: J. Phys. Chern. 60, 1412-3 (1956). 2. Jet Propulsion Lg,boratory: Combined Bimonthly Summ. Rept. 56, 7 Oct.-l Dec. 1956 (15 Dec. 1956), Confidential. 3. JARRY, R. J.: J. Phys. Chern. 61, 498-9 (1957). 4: JUDGE, J. F.: Missiles and Rockets 15: 19, 31-45 (9 Nov. 1964). 5. JONAS, H., und H. J. ABENDROTH: DBPat. 1130821 (4.2.1960/7.6.1962), Inh.: Farbenfabriken Bayer, Leverkusen, Ref.: CZ 1963, 4140. 6. JELLUM, E.: Colorimetric Method for Determination of UDMH in Blood Plasma, Royal Norwegian Air Force, Inst. of Aviation Med., Blindern, Norway, FMI Rept. 61-7, Ref.: NASA TPA N62-14194. 7. JACOBSON, K. H., et al.: The Inhalation Toxicity of Methylated Hydrazine Derivatives, US Army Chern. Center, Md., Med. Div. Rept. No. 292 (June 1954). 8. JACOBSON, K. H., et al.: Arch. of Ind. Health 12,609-16 (1955). 9. JONES, M. M., L. F. AUDRIETH, and E. COLTON: J. Am. Chern. Soc. 77, 2701-2 (1955). 10. JOHNSTON, W. H., und E. SCHWARZ: Angew. Chemie 75, 932 (1963). 11. JOHNSTON, H. S., et aI., I: J. Am. Chern. Soc. 73, 2319-21 (1951), II: J. Phys. Chern. 57, 390-5(1953), III: J. Am. Chern. Soc. 77, 4208-12 (1955). 12. JOHNSON, F. A.: US Pat. 3013631 (10.5. 1960), Inh.: Roehm u. Haas Co., Ref.: CA 56, 8297 a (1962). 13. JENKINS, A. C., and F. S. DIPAOLO: J. Chern. Phys. 25, 296-301 (1956). 14. JENKINS, A. C., and C. M. BIRDSALL: J. Chern. Phys. 20, 1158-61 (1952). 15. JENKINS, A. C., F. S. DIPAOLO, and C. M. BIRDSALL: J. Chern. Phys. 23, 2049-54 (1955). 16. JENKINS, A. C., and C. M. BIRDSALL: J. Chern. Phys. 22,1779 (1954). 17. JOHNSTON, H. L., and E. R. GRILLY: J. Chern. Phys. 14, 233 (1946). 18. JACOBS, R. B.: ARS Journal 29, 245-51 (1959). 19. JONES, P., et al.: Trans. Farad. Soc. 55, 91 (1959), Ref.: CZ 1963, 6135. 20. JOHNS, H. E.: Can. J. Res. 17 A, 221 (1939). 21. JOHNSTON, H. L., W. E. KELLER, and A. S. FRIEDMAN: J. Am. Chern. Soc. 76, 1482-6 (1954). 22. JOHNSTON, H. L., et al.: J. Am. Ch~m. S;)c. 72,3933-8 (1950). 23. JEWETT, C. L., and A. A. FOWLE: Hg,ndling, Transportation and Storage of Liquid Hydrogen, ARS-Pre- print 1074-60 (1960). 24. JACOBS, R. B.: Adv. Cryog. Engng. 2,303-17 (1960). 25. JOHNSTON, H. L., et al.: Adv. Cryog. Engng, 1, 324-8 (1960). 26. JONAS, H.: Fluor und anorganische Fluorverbindungen, Ullmanns Encyclopadie der technischen Chemie, 3. Aufi., 7. Bd., S. 577ff., Mlinch~n 1956. 27. JARRY, R. L., and H. C. MILLER: J. Am. Chern. Soc. 78, 1552 (1956). 28. Jet Propulsion 27,678-9 (1957). 29. JOHNSTON, H. S., and R. WOOLFOLK: J. Chern. Phys. 41, 269-73 (1964). 30. JORTNER, J., E. G. WILSON, and S. A. RICE: J. Am. Chern. Soc. 85, 814-5 (1963). 31. JACKSON, D. R., and A. B. ASH: Brit. Pat. 789960 (3. 5. 1954/29. 1. 1958), Inh.: Wyandotte Chem. Corp., Ref.: CZ 1962, 8478. 32. JOHNSTON, H. L., and W. L. DOYLE: Development of the Liquid Hydrogen-Liquid Oxygen Propellant Combination for Rocket Motors, Ohio State Univ., Res. Foundation, Tech. Rep. No.7 (Dec. 1951). 33. Anonym: Ozone: Ominous, Omnipotent, Jet Propulsion 27,300-1 (1957). 34. JACOBS, R. B.: Adv. Cryog. Engng. 8, 529-35 (1963). 35. JENKINS, A. C.: Laboratory Techniques for H'1ndling High-Concentration Liquid Ozone, Ozone Chem. and Techn., Am. Chem. Soc., Advances in Chemistry Series No. 21 (1959), p. 13-21. 36. JENSEN, A. V., and B. B. GOSHGARIAN: Pentaborane, AFTC, Edwards AFB (1961), 40 p., AD 258885, Ref.: CA 58, 12361 (1963). 37. JOYNER, ADAMS, and GALBRAITH: Methods of Estimating Heats of Combustion, Callery C. C., Rept. CCC- 1024-TR-30 (30 June 1954). 38. Anonym: Gasoline to Kerosene to ZIP, Jet Propulsion 27,682 (1957). 39. JOHNSON, K. D.: The Evaluation and Control of Toxicity Hazards in Solid Propellant Operations, ARS Paper 2766-63 (Jan. 1963), 27 p., N64-22240. 40. JONES, R. M.: Anal. Chern. 38, 338-40 (1966). 41. JARRY, R. L., W. H. GUNTHER, and J. FISCHER: The Mechanism and Kinetics of the Reaction Between Nickel and Fluorine, Argonne National Lab., Ill., Rept. ANL-6884 (Aug. 1963), 30 p., N 63-22988. 42. JACKSON, J. D., W. K. BOYD, and P. D. MILLER: R9activity of Metals with Liquid and Gaseous Oxygen, DefenseMetals Inform'1tion Center, Battelle Memorial Inst., Columbus, Ohio, Contract AF 33(616) 7747, DMIC-Memo 163 (15 Jan. 1963), N63-13071. 43. JAMNOW, P. A., M. W. JESSKOWA i W. S. ASEW: tJber den Kohlendioxydgehalt in filissigem Sauerstoff (in Russisch), Kisslorod (Moskau) 12: 6, 43-6 (1959), Ref.: CZ 1964: 23, 206. 44. JEFFERSON, T. B.: Cryogenic Propellant Stratification Analysis and Test Data Correlation, Martin Co., Denver, Colo., Contract AF 33(616)5615, ARL 62-432 (Sept. 1962), 27 p., N63-11538. Literaturverzeichnis K 743

45. JENSEN, A. V., B. B. GOSHGARIAN, and N. E. DANE: Mass Spectral Analysis of Rocket Engine Combustion Products Containing Boron Nitridc, AFSC Inglewood (1962), 10 p., USDC OTS AD 295656, Ref.: CA 60, 10466d (1964). 46. JIMENEZ, J.: Unveroffentlichte Arbeiten, DVL-Institut f. Raketentreibstoffe, Stuttgart. 47. J OST, A., et al.: Detonation and Shock Tube Studies of Hydrazine and Nitrous Oxide, Gottingen University and Wright-Patterson AFB, ARL Rept. 63-157 (Sept. 1963), 75 p., N63-22347, AD 419097. 48. JOHNSON, F. A.: Inorg. Chern. 5,149-50 (1966). 49. JONES, W. L., C. A. ANKERMAN, and J. W. GIBB: Experimental Performance of a Hydrogen-Fluorine Rocket Engine at Several Chamber Pressures and Exhaust Nozzle Expansion Area Ratios, NASA-TM X-387 (Oct. 1960), 39 p., Declassified N 66-33348. 50. Anonym: JANAF Thermochemical Tables, Joint Army Navy Air Force Thermochemical Working Group, Ed.: The Dow Chemical Co., Thermal Laboratory, Midland, Mich., Dir.: D. R. STULL (1964£f.), CFSTI• PB 168370. 51. JOH~, E. C., and L. C. BALL: Properties of Oxygen Fluorine Mixtures, The Boeing Co., Seattle, Wash., Aerospace Group Rept. DS-12209 (12 Jan. 1964), 39 p., N 66-28671. 52. JOHNSTON, H., and P. D. OJA: High-energy Propellants from Hydrazines and Nitro Compounds, US Pat. 3213609 (13. 7. 1959/26. 10. 1965), Dow Chemical Co., Ref.: CA 64,3276 (1966). ;'i;t JACOBS, T. A., R. R. GIEDT, and N. COHEN: Measurements of Hydrogen-Fluorine Kinetics at High Tempera• tures, AIAA-Paper 66-637 (1966). 54. JOHNSTON, H. L., A. L. SMITH, and N. C. HALLET: The Heat Capacity of Liquid para-Hydrogen from the Boiling Point to the Critical Point, Ohio State Univ., Res. Foundation, Cryogenic Lab., Columbus, Ohio, Tech. Rept. TR 264-15 (1952). 55. JOHNSON, W. R.: Helium Pressurant Requirements for Liquid Hydrogen Expulsion Using Submerged Gas Injection, NASA TN D-4102 (Aug. 1967) 47 p., N67-33441.

K

1. KOELLE, H. H.: Handbook of Astronautical Engineering, McGraw Hill, New York (1961). 2. KILNER, S. B., and L. R. RAPP: Application of Storable Propellants to Space Flight, ARS Preprint 2267 -61 (Oct. 1961). 3. KIRSHENBAUM, A. D., and A. V. GROSSE: J. Am. Chern. Soc. 81,1277-9 (1959). 4. KIRSHENBAUM, A. D., A. V. GROSSE, and J. G. ASTON: J. Am. Chern. Soc. 81, 6398-402 (1959). ri. KIRSHENBAUM, A. D., and A. G. STRENG: J. Chern. Phys. 35, 1440-2 (1961). 6. KIRTCHIK, H., and G. RIECHMANN: General Electric Co., Flight Prop. Lab., Quart. Progr. Rept. No.7, DM-62-238 (15 Oct. 1962), 13 p., N 63-10549. 7. KANAREK, 1. A.: US Pat. 2968145 (10.5.1954/17.1.1961), Inh.: North Am. Aviation, Ref.: CA 55, 13852e; CZ 1962, 6272. 8. KRAMERS, H., M. P. P. BLIND, and E. SNOCK: Chern. Engng. Sci. 14, 115 (1961), Ref.: CZ 1963, 9073. 9. KAZMIROWSKI, H. G.: DDR Pat. 23001 (25.5. 1959), Ref.: CA 58, 6746a. 10. KLAGER, K., E. M. WILSON, and G. F. HELMKAMP: Ind. Engng. Chern. 52, 119-20 (1960). 11. KUNKEL: Health Hazard of Perchloryl Fluoride, Transactions of the Symp. on Health Hazards of Milit. Chemicals, Chern. Warfare Lab. Pub. 2-10 (Aug. 1958). 12. KELSO: Reaction Between Nitric Oxides and Ammonia on Supported Catalysts, Aberdeen Proving Ground, Ball. Res. Lab., Mem. Rept. 699 (July 1953), 15 p. 13. KNIGHT, O. A.: Ncw Synthetic Fuel-Monomethylhydrazine, Hydrocarbon Process Petrol. Refiner 41: 2, 179-84 (1962), Ref.: CA 58, 1292h (1963). 14. KIT, B., and D. S. EVERED: Rocket Propellant Handbook, MacMillan Comp., New York. 15. KOCH, J. H.: DAS 1117015 (13. 7. 1960/9. 11. 1961, Am. Prior. vom 14. 7. 1959), Inh.: Engelhard IndustriEs Inc., Newark, Ref.: CZ 1962, 7028. 16. KLEMENC, A., und T. SPIESS: Monatsh. Chern. 77, 216-23 (1947). 17. KRETSCHMAR, G. G.: J. ARS 24,175-9 (1954), auch erschienen als ARS Preprint 100-53 (1953). 18. KAY, W. B.: Properties of Fuming Nitric Acid, USAF TR 6519, Part VI, Wright Patterson AFB, Dayton, Ohio (March 1955) (unclassified 6 DH 3060). 19. KAY, W. B., and M. G. FONTANA: Properties of White Fuming Nitric Acid, Ohio State Univ., Res. Found., Progr. Rept. No. 26 (12. Oct. 1954). 20. KAy, W. B., and S. A. STERN: Ind. Engng. Chern. 47, 1463-9, 1470-2 (1955). 21. KAPLAN, N., and R. J. ANDRUS: Ind. Engng. Chern. 40,1946-7 (1948). 22. KOOIKER, R. H., L. H. SCHUMAN, and YWK-KWONG CHAN: AMA Arch. Envir. Health 7, 13-31 (1963). 23. K"Rop, S.: AMA Arch. Ind. Hyg. 9, 199 (1954). 24. KLINGELHOEFER, W. C.: Anal. Chern. 34,1751-3 (1962). 25. KIN}[EY, G. R., J. C. HUMPHREY, and C. HENNINGS: Rocket Engine Starting with Mixed Oxides of Nitrogen and Liquid Ammonia by Flow-Line Additives, NACA RM E53-F05 (1953), Declassified 1963. 26. KALIL, E. 0.: US Pat. 3034291 (3.3.1949/15.5.1962), Inh.: KeUog Co., Ref.: CA 57, 6199h (1962). 744 Literaturverzeichnis K

27. KENNEDY, A., and C. B. COLBURN: J. Chem. Phys. 35, 1892-3 (1961). 28. KAUFMAN, J. J.: J. Chem. Phys. 37, 759-64 (1962). 29. KAY, W. B., and M. D. SANGHVI: J. Chem. Engng. Data 4, 22-32 (1959). 30. KAMENETSKAYA, S. A.: Untersuchung der kritischen Konzentration der Ozon-Explosion (in Russisch), Sch. fiz. chimii (1958), Ref.: Explosivstoffe 9, 188 (1960). 31. KIMBALL, A. R.: Adv. Cryog. Engng. 5, 77 -84 (1960). 32. KRETSCHMAR, G. G.: J. ARS 23, 82-4 (1953). 33. KANAREK, 1. A.: Properties, Handling and Storage Characteristics of Ethyl Alcohol and Liquid Oxygen, North American Aviation Inc., Downey, Calif., Missile Div., Rept. AL-128 (1948). 34. KRUSKA, E.: Zeitschr. VDI 97,65-70,271-7,709-13,823-9 (1955). 35. KRUSKA, E.: Weltraumfahrt 8, 109-10 (1957). 36. KOPITUK, R. C.: AIAA-Journall, 73-5 (1963). 37. KEEFE, J. H.: Field Transportation of Concentrated Hydrogen Peroxide, ARS·Preprint 328-56. 38. KEEFE, J. H., and C. W. RALEIGH: Jet Propulsion 27,663-4 (1957). 39. KUBASCHEWSKI, 0., und W. WEBER: Z. Elektrochemie 04,200-4 (1950). 40. KRETSCHMAR, G. G.: Jet Propulsion 24, 379-80 (1954). 41. KAUFMAN, W. F., W. H. ARMOUR, and L. GREEN: ARS-J. 32,1600-2 (1962). 42. KANDA, E.: Studies of Fluorine at Low Temperatures, Bull. Chem. Soc. Japan 12,416,463,472,477,511 (1937). 43. KOCH, S. D., et al.: Energiereiche polycyclische Kohlenwasserstoffe als Diisentreibstoffe (in Englisch), 137th Meeting Am. Chern. Soc. 1960,30-0; Ref.: Angew. Chemie 72, 532 (1960). 44. KOLFENBACH, J. J., and R. F. FINN: US Pat. 2938330 (31. 5.1960), Inh.: Esso Research Engng. Comp., Ref.: CA 55, 3064c. 45. KIRSHENBAUM, A. D., A. G. STRENG, and A. V. GROSSE: J. Am. Chern. Soc. 85, 360-1 (1963). 46. KANARECK, C. A.: US Pat. 2930684 (29. 3.1960) Inh.: North American Aviation Inc., Ref.: CA 04,14691 b (1960). 47. KAYE, S.: Rev. Sci. Instr. 32, 965-6 (1961). 48. KROPSCHOT, R. H., et al.: Adv. Cryog. Engng. 5, 189-98 (1960). 49. KILLIAN, W. R., and J. O. SIMPSON: Adv. Cryog. Engng. 5, 505-8 (1960). 50. KEHAT, E.: Adv. Cryog. Engng. 7, 163-9 (1962). 51. KRop, S.: Jet Propulsion 24, 223-9 (1954), vgl. auch ARS-Preprint 124-54 (1954). 52. KIRSHENBAUM, A. D., and A. V. GROSSE: J. Am. Chern. Soc. 78,2020 (1956). 53. KURZ, P. F.: Ind. Engng. Chern. 48, 1863-8 (1956). 54. KURZ, P. F.: Fuel 35, 318-22 (1956). 55. KURZ, P. F.: Fue133, 250-1 (1954). 56. KAYSER, L. T.: Priifstand der Arbeitsgemeinschaft fiir Raketentechnik u. Raumfahrt an der TH Stutt• gart, Unveriiffentliche Beobachtungen. 57. KROPSCHOT, R. H., and R. W. BURGESS: Adv. Cryog. Engng. 8, 425-36 (1963). 58. KOSHAR, M. M., and J. HOERNING: Analysis of the Rapid Cooldown of a Liquid Oxygen Loading System, Proc. of the Propellant Thermodynamics and Handling Conf. 1959, Ohio State Univ., Engng. Exp. Station, Spec. Rept. 12 (1960), p. 503-19. 59. KISTIAKOWSKY, G. B.: US Pat. 2563532 (7.8.1951), Ref.: CA 45, 9250b (1951). 60. Kooy, J. M. J.: Astronautica Acta 1, 157 -65 (1955). 61. KOLLE, D. E.: Raketentechnik u. Raumfahrtforschung 2, 101-2 (1958). 62. KOLLE, D. E.: Raketentechnik u. Raumfahrtforschung 3, 86-8 (1959). 63. KELLEY and KAVANAGH: Self-Igniting Fuels·Exploratory Work with Hydrogen Peroxide, Mass. Inst. Techn., Div. Ind. Coop., Rept. No. 23 (15 Oct. 1947). 64. KAVALL, A. J.: Feasibility Investigation of a Hybrid Rocket for Crew Escape Capsule Applications, Her• cules Powder Co., Kenvil, N. J., Summary Rept. No.1, Sept. 1961 - June 1962, Contracts DA-36- 034-0RD·3538-RD, AF 33(657)-2·R & D-l11, FDL-TDR-64-31 (March 1964), 58 p., AD 600691, N64-22274. 65. KOLLE, D. E.: Raketentechnik u. Raumfahrtforschung 7, 97 -106 (1963). 66. KANT, A., and W. H. MCMAHON: Thermal Decomposition of Hydrazine, Am. Chern. Soc., Div. Inorg. Chern., Paper 75, Meeting Atlantic City, N. C. (Sept. 1959). 67. KING, C. H.: US Pat. 2914910 (1 Dec. 1959), Inh.: United Aircr. Corp., Ref.: CA 04, 2746g (1960), Brit. Pat. 813449 (29.9. 1955/13. 5. 1959), Am. Prior. v. 11. 10. 1954, Inh.: United Aircr. Corp., Ref.: CA 53, 19392g (1959); CZ 1960,6379. 68. KUHN, L. P., and L. DE ANGELIS: J. Am. Chem. Soc. 76, 328-9 (1954). 69. KUHNS, L. J., R. H. FORSYTH, and J. F. MASI: Anal. Chern. 28,1750-2 (1956). 70. KRACKOW, E. H.: AMA Arch. Ind. Hyg. Occ. Med. 8, 335-9 (1953). 71. KOSTER, R.: Angew. Chemie 69, 94-5 (1957). 72. KAUFMAN, J., et al.: Gas Chromatography of Boron Hydrides, AFOSR TN 56-534 (Nov. 1956), AD 110353 73. KUHNS, L. J., et al.: Anal. Chem. 34,1700-1 (1962). Literaturverzeichnis L 745

74. KAUFMAN, J., et al.: Anal. Chern. 29, 1032-5 (1957). 75. KOSTER, R.: Liebigs Ann. Chern. 618, 31-43 (1958). 76. KOSTER, R., und K. ZIEGLER: Angew. Chern. 70, 371-2 (1958). 77. KOSTER, R.: Angew. Chern. G9, 94 (1957). 78. KILPATRICK, M., and L. L. BAKER: A Study of Fast Reactions in Fuel-Oxidant Systems: Anhydrous Hydra• zine with 100% Nitric Acid, 5th Symp. on Combust., Reinhold Publ. Corp., New York (1955), p.196-205. 79. KWASNIK, W.: Chemie-Ingenieur-Technik 36,690-2 (1964). 80. KNIGHT, W. P.: US Pat. 3132977 (4. 10. 1948/12.5. 1964), Inh.: Aerojet Gen. Corp., Ref.: CA 61, 2897 e (1964). 81. KEELER, M. J., and E. F. KNOLL: Investigation of Hydrofluoric Acid as a Corrosion Inhibitor for Fuming Nitric Acids, Aerojet Gen. Corp., Rept. June 1954 - May 1956, WADC Tech. Rept. 56-310 (Nov. 1956), 165 p., AD 110504. 82. KOSTING, P. R., and A. K. WONG: Examination of a Failed Type 347 Steel Drum Used for the Storage and Shipping of Fuming Nitric Acid, Watertown Arsenal Lab., Mass. WAL Rept. 316/48 (1 June 1954), 21 p., AD 42423. 83. KRYNITZKY, J. A., and H_ W. CARH.ART: Stability of Hydrazine in Liquid Ammonia, NavalRes. Lab., Washington, D. C., NRL Rept. 4219 (29 Sept. 1953), 16 p., AD 19380. 84. KUWADA, D. M.: Determination of Water in Hydrazine by GasChromatography, CIT-JPLTR 32-362 (15 Nov. 1962), 8 p., N63-13444. 85. KAYSER, L. T.: Eine radiale, membrangetrennte Einspritzmethode fiir Fliissigkeitsraketentriebwerke mit variablem Schub und/oder variablem Mischungsverhaltnis, Arbeitsgemeinschaft fiir Raketentechnik und Raumfahrt, TH Stuttgart, AGRR-TB 11 (Sept. 1964). 86_ KRAMER, P. A.: Raketentechnik u. Raumfahrtf. 6, 153-5 (1962). 87. KOLLE, D. E.: Raketentechnik u. Raumfahrtf. 0,106-8 (1961). 88. KOLLE, D. E.: Raketentechnik u. Raumfahrtf. 0, 141-3 (1961). 89. KENNY, R. J., et al.: Development and Demonstration of Main Tank Injection Pressurization System, Martin-Marietta Corp., Denver, Colo., Final Rept. FTC CR 6323, RTD TDR 63-1-123 (Dec. 1963), AD 426714. 90. KAUFMAN, J. G., and M. HOLT: Adv. Cryog. Engng.10, 77-85 (1965). 91. KULEY, C. J.: Anal. Chern. 30, 1472-5 (1963). 92. KEY, C. F., and J. B. GAYLE: Effect of Liquid Nitrogen Dilution on LOX Impact Sensitivity, NASA-TM• X-53208 CFSTI (15 Feb. 1965), 31 p., N65-19275. 93. KOCHER, R. M.: Adv. Cryog. Engng. 10, 253-8 (1965). 94. KREBS, C. H.: Zur Entwicklung von H 2/Oz-Kleintriebwerken, 3. Europaischer RaumfahrtkongreB, DGRR Stuttgart 1963, Sonderdruck 1519 (63). 95. KOSSTRJUKOW, W. N.: Thermodynamische Untersuchungen bei tiefen Temperaturen XI: Spezifische Warme von LiH zwischen 3,7 und 295°K, S und H bei 298°K (in Russisch), Sch. fizik. Chim. 30, 1759-62 (1962), Ref.: CZ 1964: 19,30, Ref. No. 0384. 96. KENNEBECK, M., et al. : Toxic Hazards Evaluation of TITAN II Test Firings: Methods and Results of Labo• ratory and Field Investigations, 6570 Aerospace Medical Res. Labs., AFSC, Rept. AMRL-TDR- 63-52 (June 1963), 70 p., AD 412442. 97. KUBY, W. C.: AIAA J. 4: 1, 160-3 (1966). 98. KENNY, R. J., and P. A. FRIEDMAN: J. of Spacecr. and Rockets 2, 746-53 (1965). 99. KRASCELLA, N. L.: Tables of the Composition, Opacity and Thermodynamic Properties of Hydrogen at High Temperature. NASA SP-3005 (1963). 100. KEPHINGER, M. L.: Report of Toxic Effects of Fluorine Following Short-Term Inhalation. Miami Univ., Res. Center of Toxicology, NASA CR-76741 (31 May 1966), 82 p., N 66-32296. 101. KAPRALOVA, G. A., E. M. TROFIMOVA, and A. E. SHILOV: Upper Ignition Limit in the Reaction of Fluorine with Hydrogen (in Russian), Kinetika i Kataliz 6, 977-81 (1965), Ref. in: IAA G, 1338 (1966), A 66-20394. Engl. Translation: Kinetics and Catalysis 6,884-8 (1965). 102. KWAWER, A. J., and J. J. GRIFFIN: Status of the Atlas FLO X Propulsion System, AIAA-Paper, First Propulsion Joint Specialist Conf. (1965). 103. KIRK, R.E., and D. F. OTHMER: Encyclopedia of Chemical Technology, 2nd Edition, Interscience Pub!., John Wiley & Sons, New York (1963ff.). 104. KIRSHENBAUM, A. D., and A. G. STRENG: J. Am. Chern. Soc. 88, 2434-6 (1966). 105. KREBS, H. J.: Luftfahrttechnik-Raumfahrttechnik 12, 335-41 (1966). 106. KELLEY, J. H.: J. of Spacecraft and Rockets 4, 1217 -24 (1967).

L

1. LA BELLE: Toxicity of Oxygen Fluoride at Levels of Exposure from 10 to 0,1 ppm by Volume, Univ. Rochester, N. Y., Pharmacology Rept. 478, Contract W-7401-eng-49 (AEC M-1941), (Jan. 1945). 2. LA LANDE, W. A.: US Pat. 2982617 (2. 5. 1961) Inh.: Pennsalt CC, Ref.: CAoo, 16926i. 746 Literaturverzeichnis L

:l. LODWIG, R. M., and J. L. MARGRAVE: Comb. and Flame 3,147-56 (1959). 4. LIBERTO, R R: An Investigation of Field Test Methods for Determining the Water Content of Titan II Propellants, Bell Aerosystems Co., Supp!. Tech. Rept. 8182-933005, Contract AF 04 (694)72 (May 19(2),44 p., AD 275537, Ref.: TAB N62-3-4, p. 28 (1962). 5. LIBERTO, R. R.: Storable Propellant Data for the Titan II Program, Bell Aerosystems Co., Progr. Rept. 8122-933002, Contract AF 04(694)72 (Nov. 19(1),22 p., AD 266457. (I. LOWRY, T. M., and J. T. LEMON: J. Chern. Soc. 1935, 693. 7. LEECH, H. R: Quart. Reviews 3,22-35 (1949). tl. LYNN, S., D. M. MASON, and B. H. SAGE: Ind. Engng. Chern. 46,1953-5 (1954). 9. LYNN, S.: Ionization in Solutions of N02 in HN03 from Optical Absorbance Measurements, CIT-JPL Progr. Rept. 20-175 (Sept. 1953), 11 p. 10. LENEHAN: Determination of Excessive Sludge Formation in Mixed Acid Storage Drums, Naval Air Rocket Test Station NARTS Rept. No. 29 (Febr. 1953), 8 p. 11. LYNN, S.: Optical Absorbance of the Ternary System HN03fN02/H20, CIT-JPL Progr. Rept. 20-187 (Jan. 1953) 22 p. 12. LANGE, N. A.: Handbook of Chemistry, 6th Ed. 1946, McGraw-Hill Book Comp., New York p.1472. 13. LEDUC, A.: Chern. Rev. 6, 1-16 (1929). 14. LUCIEN, H. W.: J. Chern. Engng. Data 7, 541-2 (1962). 15. LUCIEN, H. W.: Preliminary Study of the Effects of Ionizing Radiations on Propellants: The x-Irradia• tion of Ammonia and Hydrazine, NASA TN D-1193 (Febr. 1962),9 p. 16. LALANNE, F.: Bestimmung von Wasser und Anilin in Hydrazin, Chim. analyt. [4] 41, 45-8 (1959), Ref.: CZ 1963, 9831. 17. LEVOE, C. E., and D. M. MASON: Inhibiting Effect of HF in Fuming Nitric Acid on Corrosion of Austenitic Cr-Ni-Steels, CIT-JPL Progr. Rept. 20-253 (14 Jan. 1955). 18. LARSON, O. E.: US Pat. 3031839 (4.9. 1958/1. 5. 1962), Ref.: CA 57, 750ge. 19. LOUIS, P., R. JACKSON, and N. DI CIANNI: The Microwave Spectrum, Structure and Dipole Moment of F 20, Mallinkrodt Chern. Lab., Harvard Univ., Cambridge, Mass., Rept. (1961), 4 p., AD 272270. 20. LEWIS, G. L., and C. P. SMITH: J. Am. Chern. Soc. 61, 3063-6 (1939). 21. LIEPMANN, H. W.: Helv. Phys. Acta 11, 381 (1938). 22. LEBEDEW, M. J E.: Uberhitzung und Siedeverzug bei fiiissigem Sauerstoff (in Russisch), Kisslorod (Rus• sisch: Sauerstoff) Moskau 12: 2,15-21 (1959), Ref.: CZ 1964: 15,203, Ref. No. 1863. 23. Little, A. D., Inc. Cambridge: Rapid, High Pressure Transfer of Liquid Oxygen Within a System Immer• sed in Liquid Nitrogen, Special Rept. 105, Rept. C-59879 (1 Aug. 1959),72 p., AD 267498. 24. Little, A. D., Inc. Cambridge: Long Term Storage of Liquid Oxygen, Special Rept. 85, Rept. C-59879, Contract AF 04(647)130 (18 July 1958), 24 p., AD 267782. 25. Laporte Chemicals Ltd.: Hydrogen Peroxide, Data Manual (Aug. 1960), 80 p. 26. LEWIS, T. J., and T. M. WALTERS: J. App!. Chern. 10, 396, 403 (1960), Ref.: CZ 1963, 6135-6. 27. Little, A. D., Inc.: Liquid Propellant Losses During Space Flight, A. D. Little Rept. 63270-00-03 (Nov. 1961), 137 p., AD 270974. 28. Laporte Chemicals Ltd., Chern. and Ind. 1959: 3, 76-9 (1959). 29. Little, A. D., Inc.: Analysis of Thermal Protection Systems for Propellant Storage During Space Mis• sions, A. D. Little Inc., Tech. Rept. 63270-04-03 (Dec. 1961), 55 p., AD 270973. 30. Little, A. D., Inc.: Liquid Hydrogen Safety Manual, US Air Force Ballistic Missile Div., Contract AF 18(600)1687, Rept. C-61092 (19 Oct. 1959). 31. Little, A. D., Inc.: Study of Potential Hazards and Safety Precautions Required in Handling Large Quantities of Liquid Hydrogen, Contract AF 33(616)5223 (27 Aug. 1958). 32. LE VALLEY, W. H., and W. K. SUTTON: Adv. Cryog. Engng. G, 293-301 (1961). 33. LADD, J. W.: Adv. Cryog. Engng. 6, 388-95 (1961). 34. LIEBERMANN, P.: Adv. Cryog. Engng. 2, 225-42 (1960). 35. LEECH, H. R.: Research 5, 108-15 (1952). 36. LEWIS, R., and G. v. ELBE: Combustion, Flames and Explosion of Gases, Academic Press Inc., London- New York 1961. 37. LANDAU, R.: Corrosion 8, 283-8 (1952). 38. LINGNAU, E.: Werkstoffe und Korrosion 7, 634-71 (1956). 39. LORENZO, C. F., and T. W. GODWIN: Ignition of Several Metals in Fluorine, ARS Preprint 740-58. 40. LANDAU, R, and R ROSEN: Ind. Engng. Chern. 39, 281-6 (1947). 41. LANDAU, R.: in: Engineering Developments in the Gaseous Diffusion Process, BENEDICT et a!., ed., p. 111-21 (New York 1949). 42. LANDAU, R, and R ROSEN: Ind. Engng. Chern. 40, 1389 (1948). 43. LANDAU, R, and R ROSEN: US AEC Manhattan Project, Declass. Rept. No. 154, Oak Ridge, Tenn. (1946). 44. LEWIS, T. J.: J. App!. Chern. 11, 405-13 (1961). 45. Lo, R E.: Untersuchungen am System Lithium/Ammoniak, DLR Forschungsbericht 65-05 (Feb. 1965), 53 S., vgl. auch Z. anorg. aUg. Chern. 344, 230-40 (1966). Literaturverzeicilnis L 747

46. LAVROV, F. A., i N. A. POKATILO: Die Ito lie der Nitrosite bei der spontanen Verbrennung von Dicyclopen• tadien mit Salpetersaure (in Russisch), Akademija Nauk SSSR, lnstitut Nefti, Trudy 12,354-62 (1958). 47. LARSEN, O. E., and E. D. GUTH: US Pat. 3058301 (24.12.1958/16.10. 1962), Inh.: Phillips Petrol. Co .. Ref.: CA 60, 1532g (1964). 48. LEONARD, A. S.: J. ARS 17, 20-31 (1947). 49. LOSSING, F. P., K. J. INGOLD, and A. W. TICKNER: Discuss. Farad. Soc. 14, 34-44 (1953). 50. LAQUER, H. L.: Adv. Cryog. Engng. 5, 85 -94 (1960). 51. LAQUER, H. L.: Pressurized Transfer of Cryogenic Liquids, A. D. Little Inc., Cambridge, Mass., Special Rept. No. 78, Rept. No. C-59879-9, AFBMD Document 8-8735 (1 June 1958) AD 219437. 52. LAWLER, J. H. L.: The Specific Impulse of Hydrogen Burned in Nitrogen-Oxygen Mixtures, Wright Patterson AFB, Directorate of Adv. Systems, Techn. Rept. WADD TN 60-254 (Nov. 1960), 315 p., AD 265361. Ref.: CA 57, 14041i (1962). 53. LOVELL, J. C., N. E. SAMANlCH, and BARNETT: Experimental Performance of Area Ratio 200, 25 and 8 Nozzles on JP-4 Fuel and LOX Rocket Engine, NASA Tech. Memo X-382 (Aug. 1960), 16 p. 54. LOVELL, J. C., and N. E. SAMANICH: Experimental Performance of Nozzles Having Area Ratios up to 300 on JP-4-Fucl-LOX-Rocket Engine, NASA TN D-847 (June 1961), 17 p. 55. LIEBERT, C. H., and R. C. EHLERS: Determination of Local Experimental Heat Transfer Coefficients on Combustion Side of an Ammonia-Oxygen Rocket, NASA TN D-l048 (Sept. 1961), 20 p. 56. LYON, D. N., P. G. KOSKY, and B. N. HAR)IAN: Adv. Cryog. Engng. 9, 77-87 (1964). 57. LARSEN, P. S., and J. A. CLARK: Adv. Cl'yog. Engng. 8, 507-20 (1963). 58. LINDQUIST, C. R., and L. R. NIENDORF: Adv. Cryog. Engng. 8, 398-403 (1963). 59. LADANYI, D. L.: Ignition Delay Determinations of Furfuryl Alcohol and Mixed Butyl Mercaptans with Various White Fuming Nitric Acids Using Open-Cup and Small-Scalc Rocket-Engine Apparatus, NACA RM E 53-E 29 (Feb. 1955), 17 p. 60. LADANYI, D. L., and R. O. MILLER: Comparison of Ignition Delays of Several Propellant Combinations Obtained with Modified Open-Cup and Small-Scale Rocket Engine Apparatus, NACA RM E 53-D 03 (June 1953), 20 p. 61. LUTZ, 0., J. LAMBRECHT und W. l\HiLLER: Reaktionsenthalpie-Entropie-Tafel fUr ein unterstochiometri• sches Gemisch Hydrazin-Salpetersaure bis 4000 oK, Deutsche Forschungsanstalt f. Luftfahrt, Braun• schwcig, lnst. fiir Strahltriebwerke, Forschungsbericht FBS to/54 (April 1954), vgl. auch FBS 2/54 (Marz 1954). 62. LEPIE, A.: Ein Beitrag zur Messung des Ziindverzuges hypergolcr Raketentreibstoffe, Dissertation TH Miinchcn 1961. ii3. LADANYI, D. L.: Orthotoluidine and Triethylamine in Rocket Engine Applications, NACA RM E 52-K 19 (June 1953). H4. LADANYI, D. L.: Some Fundamental Aspects of Nitric Acid Oxidants for Rocket Applications, NACA RM E 52-J 01 (1953). 1\5. LUTZ, 0.: Vergleichsbetrachtungcn und Treibstofffragen bei Raketenantrieben, Schriften der dt. Akad. d. Luftfahrtforschung Nr. 1071, S. 13-36 (1943). H6. LUTZ, 0.: Some Special Problems of Power Plants. in: History of German Guided Missiles Development, Agardograph 20. Verlag App~lhans & Co., Braunschw3ig (1957), p. 238-252. 67. LADANYI, D. J., et al.: Starting of Rocket Engine at Conditions of Simulated Altitude Using Crude Mono• ethylaniline and Other Fuels with Mixed Acid, NACA RM E 50-D 20 (19 July, 1950). 68. LYSYJ. 1., and P. R. NEWTON: Anal. Chpm. 35, 90-2 (1963). 69. LEWIS, J. D., and A. C. MERRINGTON: 7th Symp. on Combust., Butterworths Scientific Publications. Lon• don (1959), p. 953-7. 70. LEE, D. H., and D. D. EVANS: The D~velopment of a Heated-Hybrid Generated Gas Pressurization System for Propellant Tanks, CIT-NASA-JPL Tech. Rcpt. 32-375 (15 Feb. 1963), 56 p., N 63-14483. 71. LEE, D. H.: Performance Calculations of Monopropellant Hydrazine and Monopropellant Hydrazinc and Hydrazine Nitrate Mixtures, CIT-JPL Tech. Rept. 32-348 (3 Dec. 1962), 92 p., USDC OTS price $ 8,60. 72. LEE, D. H.: Development of the Midcourse Trajectory-Correction Propulsion System for the Ranger Spacecraft, CIT-JPL Tech. Rept. 32-335 (15 March 1963), 25 p., N 63-19783. 73. LARSON, R. L., et al.: A Monopropellant Space Vphicle Propulsion System, ARS Preprint 2217 -61 (1961). 74. LAWRENCE, E. A., andF. L. vONBREOHT: US Pat. 2815270 (11. 7. 1/9453. 12. 1957},Inh.:Aerojet-Gen.Corp. 75. LEVY, J. B.: Naval Ordn. Lab. NAVORD Rep. 2897 (Aug. 1953), 20 p., und: J. Am. Chern. Soc. 76, 3790 (1954). 76. LAWRENCE, R. W., and W. P_ KNIGHT: ARS-J. 29, 29-32 (1959) und ARS-Preprint 527-57 (1957)_ 77. LEWIS, G. D.: Performance of Propyl Nitrate as a Rocket Monopropellant, United Aircr. Corp., East Harford, Conn .. Rept. R 16614-1 (Unclass. LPH 3047). 78. LEVY, J. B.: Ind. Engng. Chern. 48, 762-5 (1956). 79. LAWRENCE, E. K., and E. C. NOONAN: Liquid l\ionopropcllants: Interpretation of Strand Burning Rates, I: Ethyl Nitrate. Naval Ordn. Lab., NAVORD Rept. 4239 (8 June 1956), 32p., AD 105996. 80. LEVY. J. B., and F. J. ADRIAN: J. Am. Chern. Soc. 77, 2015-16 (1955). 748 Literaturverzeichnis L

81. LEZBERG: Spontaneous Ignition of Pentaborane Sprays in a Hot Air Stream, NACA RM E 55-F 29a (Nov. 1956), 26 p., (Declass. by NACA Res. Abstr. 128, 6/4/1958). 82. LAMNECK, J. H., and S. KAYE: Thermal Reaction of Diborane with Trimethylborane, NACA RM E 58- E 12 (Sept. 1958), 26 p. 83. LAWTON, E. A., and E. A. WEILMUENSTER: US Pat. 3013083 (6.1.1956/12.12.1961), Ref.: CZ1963, 20242. 84. LAMBERTI: Review of the Toxicological Properties of Pentaborane, Diborane, Decaborane and Boric Acid, NACA RM E 56-H 13a (Dec. 1956), 24 p. 85. LONG, LEVINSKY, HILL, and SVIRBELY: AMA Arch. of Ind. Health 1957, No.5 (Nov. 1957). 86. LANG, K, und F. SCHUBERT: DB Pat. 1071703 (24.12. 1959), Inh.: Farbenfabriken Bayer, Ref.: CA 50, 10892 (1961). 87. LADANYI, D. J., and R. O. MILLER: Jet Propulsion 26,157-63 (1956) und ARS-Preprint 255-55. 88. LALLI, G.: Ann. Geofis. (Roma) 16, 385-406 (1963), Ref.: CA 61, 4886h (1964). 89. Anonym: Methods of Gaging Liquid Oxygen, A. D. Little Inc., Cambridge, Mass., Special Rept. No. 66, C-59879 (1 April 1958), 84 p., AD 162535. 90. LOGAN, J. L., and A. ROALD!: US Pat. 3006733 (30. 1. 1958/31. 10. 1961), Ref.: CZ 1963, 10273. 91. LAMNEK, J. H.: J. Chem. Engng. Data 5, 233-5 (1960). 92. LONG, S. A., W. H. BERGDORF, and E. J. KINSLEY: The Development of Corrosion Inhibitor for Fuming Nitric Acids, Proceedings of the Propellant Thermodynamics and Handling Com., Ohio State Univ., Spec. Rept. 12 (1960). Ed. by L. E. BOLLINGER and A. W. LEMMON, p. 539-51. 93. LEWIS, G. J.: Trans. Inst. Chern. Engr. 39: 3, No. 155, A 56-A 58 (1961), Ref.: CA 1962, 6910. 94. LUCIEN, H. W.: J. Chern. Engng. Data 6, 584-6 (1961), Ref.: CZ 1963, 7283. 95. LOVE: The Hydrogen Peroxide Reaction·Control System for the X-l B Research Airplane, NASA TN D-185 (Dec. 1959), 28 p. 96. LEUPOLD, M.: Raketentechnik u. Raumfahrtf. 6, 112-7 (1962). 97. Lo, R.: Praktische Erfahrungen beim Arbeiten mit elementarem Fluor, DVL-Bericht 413, DLR-FB 65-12 (Marz 1965), 24 S. 98. LOGAN, S. E., and C. A. WALKER: Adv. Cryog. Engng. 10, 441-50 (1965). 99. LACAZE, A. : Transferl de Chaleur it I'Hydrogene Liquide, Inst. Internat. du Froid, Cours sur I'Hydrogene Liquide, Grenoble Juin 1965. 100. LIEBENBERG, D. H., and F. J. EDESKUTY; Adv. Cryog. Engng. 10, 284-91 (1965). 101. LEVY, J. B., et al.: The Deflagration of Hydrazine Perchlorate, Am. Chem. Soc., Symposium on Advanced Propellant Chemistry, Detroit (1965), Preprint of Papers Vol. 9, No.1, p. 56-79. 102. Lo, R. E.: Erfahrungen bei der lithergolen Verbrennung von Lithiumhydrid mit Fluor, Bericht3. Sitzung Treibstoff-Fachausschu13 WGL. DLR M.itt. 65-10 (1965). 103. Lo, R. E.: Einige Eigenschaften von Lithiumhydrid im Hinblick auf seine Verwendung als Raketenbrenn• stoff, 1. Teil: Dichte von LiH-Pre13kiirpern, DLR-FB 65-49 (1965) 22 S. 104. Lo, R. E.: Eigenschaften von Lithiumhydrid im Hinblick auf seine Verwendung als Raketenbrennstoff, Teil II: Warmeleitfahigkeit, DLR FB 68-23 (1968). 105. Lo, R. E.: Beryllium und Berylliumverbindungen als Raketentreibstoffe. DVL Institut fUr Raketentreib- stoffe, Interner Bericht (April 1965), 171 S. 106. LEWIS, B.: US Pat. 3177652 (27.2.1961/13.4.1965), Ethyl Corp., CA 63, 5442a (1965). 107. LEVY, J. B., and B. K COPELAND: J. Phys. Chem. 67, 2156 (1963); 69, 408 (1965). 108. LUPER!, M., and J. J. LOVINGHAM: Investigations of Space Storable Propellants, Thiokol Chern. Corp .• Reaction Motors RMD 6028-F (Jan. 1964), NASA CR 58800, N 64-30525. 109. LEA, R. H., J. G. DREW, and F. K WOLF: J. of Spacecraft and Rockets 3,728-34 (1966). 110. LAWTON, E. A., and D. F. SHEEHAN: US Pat. 3254944 (20. 12. 1961/7. 6. 1966), CA 65,5295 (1966). 111. LEVY, J. B., and B. K WESLEY: J. Phys. Chern. 69, 3700-4 (1965). 112. LUCIEN, H., and M. L. PINNS: The x-Irradiation of Hydrazine and 1,1-Dimethylhydrazine, NASA TM X-54848 (18 Sept. 1964), 13 p., N 66-33176. 113. LEE, W. B.: Ind. Engng. Chem., Prod. Res. Dev. 6, 59-64 (1967). 114. LAWVER, B. R.: AIAA-J. 4, 659 (1966). 115. LAWVER, B. R., and J. J. KAPPL: Effects of Additives on Altitude Hypergolic Ignition, AlA A Paper 66-608_ 116. LAWLER, A. E.: Adv. Cryog. Engng. 12, 780-4 (1967). 117. LAPIN, A.: Adv. Cryog. Engng.12, 198-206 (1967). 118. Anonym: A Study of Hydrogen Slush and/or Hydrogen Gel Utilization, Lockheed Miss. and Space Co. Sunnyvale, Calif., Vol. I: LMSC-K11-67-1, NASA CR-87655 (11 March 1967) 72 p., N67-34 912; Vol. II: NASA CR-85822 (11 March 1967) 236 p., N67-31330. 119. Anonym: Hydrogen Handbook, A Compilation of Properties, Handling and Testing Procedures, Compati• bility with Materials and Behavior at Low Temperatures, A. D. Little Inc., Rept. (April 1960) 246 p., AD 242 285. 120. LEE, W. B.: Feasibility Study of Oxygen/Hydrogen Powdered Metal Ignition, Marquardt Corp., Van Nuys, Calif., Final Rept. NAS 8-11 250, NASA CR-68 773 (1 Sept. 1965) 82 p., N67-31 967. 121. LAWVER, B. R., and B. P. BREEN: The Effect of Additives on Droplet Hydrazine Burning (in N 20 4 ). AIAA Paper 67-482. Literaturverzeichnis M 749

M

1. MORROW, S. I., D. D. PERRY, and M. S. COHEN: J. Am. Chern. Soc. 81, 6338-9 (1959). 2. MORROW, S. I., et al.: J. Am. Chern. Soc. 82, 5301-4 (1960). 3. MARSH, F. D.: US Pat. 3032400 (14. 1. 1960(1. 5. 1962), Inh.: DuPont de Nemours and Co. 4. MARGRAVE, J. L., and R. P. WENDT: J. Chern. Phys. 31, 857 (1959). 5. MASON, D. M., and S. S. T. FAN: J. Chern. Engng. Data 7,183 (1962). 6. MrTZ, M. A., F. L. ALDRICH, and V. M. VASTA: Study of the Intermediary Metabolic Pathways of UDMH, Wright Patterson AFB, 6570th Aerospace Med. Res. Labs., Final Rept., AMRL-TDR 62-110 (Sept. 1962), 27 p., N 63-10469, AD 290509. 7. McBRIDE: Analytical Procedures for 1.1-Dimethyl Hydrazine, US-NOTS 1475, NAVORD Rept. 5263 (May 1956). 8. MALONE, H. E., and R. A. BIGGERS: An Acetylation Method for Determining Mixtures of Either Hydra• zine/l,l-Dimethyl Hydrazine or Monomethyl Hydrazinejl,l-Dimethyl Hydrazine, Space Systems Div., Inglewood AFSC Rept. SSD-TDR 62-203 (Dec. 1962), 15 p., Ref.: TAB 63-2-3, p. 11 (1963). 9. ~1ALONE, H. E.: Anal. Chern. 33, 575 (1961). 10. MALONE, H. E., and R. E. BARRON: Determination of Mixtures of Diethylene Triamine with Hydrazine and Substituted Hydrazines, Edwards AFB, Calif., Rept., US OTS AD 255804 (1961), 14 p., Ref.: CA 58, 6637 c (1963). 11. MOBERG, M., W. KNIGHT, and H. KINDSVATER: Anal. Chern. 28, 412-3 (1956). 12. MASON, D. M.: Simplified Method for Testing the Acceptability of Fuming Nitric Acid for Storage and Use as an Oxidizer for Rocket Fuels, CIT-JPL Progr. Rept. 20-229 (29 Jan. 1954). 13. MASON, D. M., L. L. TAYLOR, and S. P. VANGO: Anal. Chern. 27, 1135-42 (1955), auch erschienen als CIT-JPL Progr. Rept. 20-205 (Jan_ 1954). 14. MURACA, R. F.: The Analysis of Red Fuming Nitric Acid, CIT-JPL Pro gr. Rept. 20-343 (Dec. 1957), 26 p. 15. MALONE, H. E.: Determination of Hydrogen Fluoride in Fuming Nitric Acid, Wright Air Dev. Center, WADC Power Plant Lab., Rept. WADC-TN-WCLP-55-155 (1 April 1955), 11 p. 16. MASON, D. M.: Jet Propulsion 26,741-4 (1956), auch erschienen als ARS Preprint 237-55 (1955). 17. MORTENSON, L. N.: Problems Encountered During Installation and Operation of a Storable Propellant Facility for Testing of TITAN II Components and Systems, Wyle Labs., EI Segundo, Calif., T~ 10235 (7 March 1961). 18. MILLER, W. S.: Brit. Pat. 795545 (28 May 1958, Am. Prior. US Pat. 2733195), Inh.: Olin Mathieson Chern. Co., Ref.: CA 50, 9700b (1956). 19. MANNION, J. P_: US Pat. 2849356 (26 Aug. 1958), Inh.: Olin Mathieson C. C., Ref.: CA 52, 19624h. 20. McDONALD: Photolysis of Ammonia at 1849 A, Illinois Inst. of Technology, Dept. Chern. (Feb. 1953). 20p. 21. ~'IACMILLAN, J. A.: Possible Implications of the Damage by Radiation in the Storage of Propellants in Outer Space and Tentative Methods for its Measurements, US AEC Argonne ~at. Lab., Rept. 6585 (July 1962), 17 p., Ref.: CA 57, 15401 b (1962). 22. MOORE, R. L.: Research on the Hazard Classification of New Liquid Propellants (N20 4, N2H 4, BSHg, ClFa). North Am. Aviation-Rocketdyne Rept. R-2452-3 (31 Oct. 1960). 23. MURACA, R. F.: Solubility of Aluminium Nitrate in RFNA, CIT-JPL Progr. Rept. 20-338 (Jan. 1958), 10 p. 24. ~IASON, D. M., and L. L. TAYLOR: Inhibiting Effect of HF in HNOa on Liquid and Gas Phase Corrosion of Several Metals, CIT-JPL Progr. Hept. 20-225 (Jan. 1955), 23 p. 2,,). MASON, D. :U.: }Iechanism of Inhibiting Effect of HF in Fuming Nitric Acid on Liquid Phase Corrosion of AI- and ~teel-Alloys, CIT-JPL Progr. Rapt. 30-309 (Ike. 1956), 13 p. 26. :VIASON, D. ]);L 1. PETKER, and S. P. YANGO: J. Phys. Chern. 59, 511-{i (1955), Supplementary Material: American Docum9ntation Inst., \Vashington, D. C., D,)cumcnt 4465. 27. MASON, D. M.: Viscosity and Density of the Nitric Acid-Nitrogen Dioxide-Water System, CIT-JPL Progr. Rept. 20-214 (Jan. 1954),3:3 p. 28. McKEOWN, A. B., and F. E. BELLES: Vapor Pressures of Concentrated ~itric Acid tlolutions in the Com• position Range 83-97% H~03' 0-6% N02, 0-15% H 20 and in the Temperature Range 20-80°C. NACA RM E 53-G 08 (1953). 29. McKEOWN, A. B., and F. E. BELLES: Vapor Pressure and Calculated Heats of Vaporization of Concen• trated Nitric Acid Solutions in the Compositions Range 71-89% HNOa, 7 -20% N02, 1-10% H 20 and in the Temperature Range 10-60°C, NACA RM E 53-L 14 (1954). 30. McKEOWN, A. B., and F. E. BELLES: Ind. Engng. Chern. 47, 2540-3 (1955). 31. MCCURDY, J. L.: Ind. Engng. Chern. 34, 1002-4 (1942). 32. McADAMS, A. J., and S. KROP: J. AMA 158,1022-4 (1955). 33. McKENNIS, H., and A. S. YARD: Anal. Chern. 26,1960 (1954). 34. McKENNIS, H.o J. H. WEATHERBY, and L. B. WITKIN: J. Pharmacal. and Exper. Therap. 114,385 (1955) 35. MASCOLO: Heat Transfer to Ammonia Flowing Turbulently in an Unsymmetrically Heated Rectangular Tube, ~orth. Am. Aviation, Rockctdyne Div .. Rept. E-1155 (Nov. 1958),46 p. 750 Literaturverzeichnis M

36. MILLER, R. 0.: Safety and Handling of Ozone-Oxygen Mixtures, Proc. Propellant Thermodynamics and Handling Conf., Ohio State Univ. 1960, p. 493-502. 37. MILLER, R 0.: J. Phys. Chem. 63,1054-7 (1959). 38. MULLINS, J. C., 'V. T. ZIEGLER, and B. S. KIRK: The Thermodynamic Properties of Oxygen from 30 to 100oK, Georgia Inst. Techn., Engng. Exp. Station, Atlanta, Rept. on Contract NBS CST-7339 and 7238 (1 March 1962), 108 p., Ref.: NASA TPA N 62-15397. 39. MACHU, W., und S. A. ZAKI: OsterI'. Chem. Ztg. 61,157 (1960), Ref.: CZ 1962,17330. 40. ]\UTHlEU: Zersetzung von HzOz mit Ca(Mn04)2 (in Franzosisch), Pub!. Sci. Min. Air. France, Kote Techn. 27 (1948), 13 p. 41. MCCORMICK, J. C., A. LIJEWSKI, and G. CARMINE: Storage of 90% and 98% (by Weight) Hydrogen Pcr• oxide in Sealed Containers for Extended Periods, BECCO Chem. Div., fmc. Propulsion Department Rept. No. 3504-7 (Nov. 1961),71 p., Rep. SSD-TR-61-29; AD 268379. 42. MCCORMICK, J. C.: Space/Aeronautics 39:3,101-9 (March 1963). 43. MECKERT: Hz0 2, Problems and Operating Procedures, ARS-Preprint 78-52. 44. MARTINEZ, F., and J. A. WOJTOWICZ: Super-Oxidizers, Holloman AFB, New ~Iexico, Rept. (1961), 79 p., AD 256787; Ref.: CA 58,5441£. 45. McKINLEY, C., and E. S. J. WANG: Adv. Cryog. Engng. 4,11-25 (1960). 46. MEDARD, L.: Mem. poudres 31,273-85 (1949), Ref.: CA 46,11687. 47. MCCAMY, C. S.: Ind. Engng. Chem. 49: 9, 81A-82A (Sept. 1957). 48. MOTTRAM, A. W. T.: Liquid Hydrogen as a Fuel, 12. lAF Congress, Washington. D. C., Academic Press 1963, p. 1-9. 49. MORTENSEN, L. N.: Adv. Cryog. Engng. 6, 379-87 (1961). 50. MATSCH, L. C., and O. P. ROBERTS: Adv. Cryog. Engng. 6, 555-61 (1961). 51. MENARD, J., and L. WElL: Adv. Cryog. Engng. 6, 587-9 (1961). 52. MACINKO, J., P. B. CHELTON, and J. DEAN: Adv. Cryog. Engng. 3,1-10 (1960). 53. McINTOSH, G. E., et a!.: Adv. Cryog. Engng. 1, 62-76 (1960). 54. MURRAY, R L., et al.: Ind. Engng. Chem. 39, 249-54 (1947). 55. MILLER, W. T., and L. A. BIGELOW: J. Am. Chem. Soc. 58,1585-9 (1936). 56. MYERS, W. R, and W. B. DELONG: Chem. Engng. Progr. 44, 359-62 (1948). 57. MILLAWAY, E. E., and L. C. COVINGTON: Resistance of Titanium to Gaseous and Liquid Fluorine, TMCA Publication (1959). 58. McBRIDE, R H.: Metering of Fluorine and Hydrogen Fluoride, AECD Rept. 3690 (1945). 59. MAYER, L., and J. GUELICH: AMA Arch. Env. Health 7, 445-7 (1963). 60. MASON, D. M., O. W. WILCOX, and B. H. SAGE: J. Phys. Chem. 56,1008-10 (1952). 61. MCCARTHY, J. R, and H. WOLF: ARS-J. 30, 423-5 (1960). 62. MAYA, W.: Inorg. Chem. 3, 1063 (1964). 63. MILLIGAN. D. E., and D. R SEARS: J. Am. Chem. Soc. S5, 823 (1963). 64. MALM, J. G., J. SHEFT, and C. L. CHERNICK: J. Am. Chcm. Soc. 85,110 (1963). 65. MANN. D. E.: Some Aspects of Fluorine Flame Spectroscopy, Proc. of the Propellant Thermodyn. and Handling Conf., Ohio State Univ., Special Rept. No. 12 (1960). p. 127 -38. 66. MANN, D. E., and G. T. ARMSTRONG: Fluorine and Ammonia Combustion, '''right _lir Dev. Center, Tech. Rept. 53-365 (Sept. 1956),53 p., ASTIA AD 97331. 67. MUELLER, K H., and W. P. WALTERS: J. Am. Chem. Soc. 76, 330-2 (1954) and 73, 1458-61 (1951). 68. MEEHAN and ELDRIDGE: Jet Propulsion 25,54 (1955). 69. MANDELL, B., and L. E. WHITE: Adv. Cryog. Engng. 5,120-7 (1960). 70. MOORE, R W., A. A. FOWLE, and B. M. BAILEY: Adv. Cryog. Engng. 5, 450-9 (19GO). 71. MINKIN, H. L., and H. F. HOBART: Liquid Hydrogen :Flowmeter Calibration Facility, NASA TN D-577 (Oct. 1961), 40 p., AD 265479. 72. MINKIN, H. L., H. F. HOBART, and 1. WARSHAWSKY: Adv. Cryog. Engng. 7, 189-97 (1962). 73. MALONEY, C. J., and A. S. KIDWELL: Effect of Potential Rocket Fuels and Oxidizers on Elastomers and Development of Elastomeric Compounds Suitablc for Retention of These Materials, Wright Air~Dev. Center WADC TR 56-351, Contract AF 33(616)2962 (Nov. 1956), 115 p., AD 110511. 74. MORRELL, G.: Intcrnal Film Cooling of 1000 Pound Thrust Liquid Ammonia-Liquid Oxygen Rocket En• gine Combustion Chamber, NACA RM E 51-E 04 (July 1951), 42 p. 75. MURRAY, R C., and A. R HALL: Trans. Farad. Soc. 47, 743-51 (July 1951). 76. MILLER, R 0., and D. D. BROWN: Effect of Ozone Addition on Combustion Efficiency of Hydrogen- Liquid Oxygen Propellant in Small Rockcts, KASA Memo 5-26-59E (Junc 1959), 18 p. 77. MCGREW, J. L.: Adv. Cryog. Engng. S, 387-92 (1963). 78. MERRILL, H. K, and D. W. MURPHY: Adv. Cryog. Engng. 8, 393-7 (1963). 79. MULLINS, J. C., W. T. ZIEGLER, and B. S. KIRK: Adv. Cryog. Engng. 8, 12G-:34 (1963). 80. MULLINS, J. C., W. T. ZIEGLER, and B. S. KIRK: Adv. Cryog. Engng. 8, 116-25 (1963). 81. MCCROSKEY, J. G.: Gelled Propellant Safety Investigation (N20 4 and UDMH). AFSC, Edwards AFB, RTD-TDR 63-1069 (July 1963), 14 p., N 63-22727, AD 418275, Ref.: CA 60. 15671 (1964). Literaturverzeichnis M 751

82. MATOS, S. R., and E. J. JOHNSON: pprformanee of Irradiated and Chemically Treated JP-5 Fud with IRFNA, Ammunition Dev. Div., Picatinny Arsenal, Dover, N. J., Tech. Rept. DL-TR 1-61 (Aug. 1961), 21 p., AD 268931, Ref.: CA 58, 5441 d. 83. MERTENS, J., and R. L. POTTER: Comb. and Flame 2, 181--2 (1958). 84. MERTENS, J., and R. L. POTTER: Comb. and Flame 3, 525-7 (1959). 85. MORRELL, G., and D. J. LADANYI: Chemical Igniters for Starting Jet Fuel/Nitric Acid Rockets, NACA RM E 57 -G 26 (Oct. 1957), 17 p. 86. MASON, C. M., G. GELERNTER, and J. COOPER: Long Range Research Leading to the Development of Superior Propellants: Mechanism of Burning (KerosenefNitric Acid), Bur. of Mines, Progr. Rept. 60, Proj. TB 3-0110 (1. 1. 1956/31. 3. 1956), 3 p., AD 94702. 87. MILLER, R. 0.: Ignition Delays of Alkyl Thiophosphites with WFNA and RFNA, NACA RM E 52-K 2;') (Febr. 1953), 24 p. 88. MAKOVKY, A., and A. SALMON: J. App!. Chem. 8, 670-2 (1958). 89. MALINA, F. J., and J. W. PARSONS: US Pat. 2771739, Inh. : Aerojet-Gen. Corp. (27. 11. 1956), Ref.: CA 51, 3969h (1957). 90. MURACA, R. F.: Determination of Hydl'azine and Water in Furfuryl Alcohol - Aniline Fuel Mixtur('~, CIT-JPL Progr. Rept. 20-284 (Feb. 1956). 91. MASON, D. M.: Simplified Chemical Method for Testing the Acceptability of Furfuryl Alcohol - Aniline Rocket Fuel Mixtures, CIT-JPL Progr. Rept. 20-259 (Jan. 1955),4 p. 92. MASON, D. M.: Factors Affecting Formation of Resins and Their Deposition on Heat Exchanger Wall" by Furfuryl Alcohol - Aniline Mixtures. CIT-JPL Progr. Rept. 20-210 (Dec. 1953). 93. MILLER, R. 0.: Ignition Delays and Fluid Properties of Several Fuels and Nitric Acid Oxidizers in Tem• perature Range from 70° to -105°F, NACA TN-3884. 94. MILLER, R. 0.: Effects of Nitrogen Tetroxide and Water Concentration on Freezing Point and Ignition Delay of Fuming Nitric Acid, NACA RM E53-G31. 95. MILLER, R. 0.: Ignition Ddays of Some Nonaromatic Fuels with Low-Freezing RFNA in Temperature Range from -40° to -105°F, NACA RM E52-K20 (19 Jan. 1953),17 p. 96. MILLER, R. 0.: Low Temperature Ignition Delay Characteristics of Several Rocket Fuels with l\Jixed Acid in Modified Open Cup Type Apparah18, NACA RM E50-H16 (17 Oct. 1950),23 p. 97. MOUTET, A .. et M. BARRERE: La recherche aeronautique 75, 23-35 (1960). 98. MORRELL, G.: Summary of NACA-Research on Ignition Lag of Self· Igniting Fuel-Nitric Acid PropellantH, NACA RM E57-G19 (Oct. 1957),48 p. 99. MILLER, R. 0.: Ignition Delay Characteristics in :UodifiPrl Open Cup Apparatus of Several :Fuels with Nitric Acid Oxidants within T('mperature Range 70 to -105°F, NACA RM E51-J11 (1951). 100. MOSHIER, R. W., and L. SPIALTER: Amines, I: N, N, N', N'-Tetramethyl-l,2.propanediamine, WADe. ARL, Wright Patterson AFB, WADC Tech. Xote 56-2m (1 June 1956), 7 p., AD 97228. 101. MOUTET, A., et H. MOUTET: Franz. Pat. 1290333 (3.3.1961/13.4.1962), Ref.: CA 58, t296" (1963). 102. MOUTET, A., et H. MOUTET: Franz. Zusatzpatent 78084 zu FP 1246776, Ref.: CA 57, 16954 (1962). 103. MOUTET, A., et H. MOUTET: Franz. Zusatzpatent 79974 zu FP 1246776 (16.6.1961/15.2.1963), Rd.: CA 60, 1531a (1964). 104. MOUTET, A., et H. MOUTET: Franz. ZlIsatzpatent 76768 zu FP 1246776, Ref.: CA 58, 406e (1963). 105. MOFFAT, W. H.: Reliability Analy~i~ of Hybrid Propulsion System, Space General Corp., EIMonte, Calif., Rept. 21.'54 (Nov. 1961),21 p .. Rd.: NASA TPA N62-15897. 106. METZLER, C. V., and 'V. H. MOBERLY: Basic Inve~tigation of Hybrid Combustion Processes, Rocketdyn{' Quart. Progr. Reports R-2267-1 (:H :'IIarch 19(0), 17 p., anri R-2267-2 (30 June 1960). 107. MOORE, G. E., F. M. COOPER, and D. H. DRISCOLL: A Hybrid Rocket Propellant System 90% Hydrogen Peroxide/Solid Fuel, Part I: General Consideration~, General Electric Co., Schenectad.\', X. Y., l{('Jlt. No. R 52 A 0516 (Nov. 1952), 26 p., AD 5249. 108. MOORE, O. E., D. H. DRISCOLL, and K. BERMA:-i: siehl' [M 107]. Rept. R 5:3 .-\ 0509 (July 1954), 74 p., AD 53096. 109. MOORE, G. E., and K. BERMAN: Jet Propulsion 26, 965-8 (1956). 110. MITTLER, S., M. KING, and B. BURKHARDT: Toxicity of Ozone, Ozone Chem. and Technology, Am. Clwm. Soc. Advances in Chem. Series. No. 21, Washington (1959), p. 344-51. 111. MANLEY, T. C.: Research on Liquid Ozone and Development of Full Scale Equipment for Its Manufacture, Ozone Processes Div., Welsbach Corp., Philadelphia, Pa., Final RqJt. 16 May 1951·-31 Dec. 19;')2. Contract NOa(s) 51-609-c (20 Mareh 1953),34 p., AD 7658. 112. MILLAN, G., and S. SANZ: HydrazinC' Dpcomposition Flames, Institute Naeional de Tecnica Aeronautica, Spain, Office of Sci. Res., Rept. on Contract AF 61(514)734-C, OSR TN 56-466 (June 1956), AD 97084. 113. MICHEL, K. W .. und H. G. WAGNER: Z. phys. Chem. NF 35,392-5 (1962). 114. MARX, P. C.: Propulsion Research Program: Catalytic Decomposition of Hydrazine, Aerospace Corp .. Los Angeles, Semiannual Tech. Rept. 1 Jan.-30 .June 1962, TDR f)9 (2210-13) TR-2, DCAS TDR 62-162 (31 Aug. 1962), i5 p., AD 285083. 752 Literaturverzeichnis M

115. MARTINEZ, J. S., L. J. VAN NICE, and A. F. GRANT: NIMPHE, a New Rapid, Restartable Monopropellant Hydrazine Engine, AIAA-Preprint 63-242 (June 1963), 7 p. 116. MARTINEZ, J. S., L.J. VAN NICE, and A. F. GRANT: Astronautics and Aerospace Engng. 1: 9, p. 82 (Oct. 1963). 117. MEAD, G. A.: ARS-J. 29 192-8 (1959). 118. MASON, C. M., and J. RIBOVICH: Sensitivity Characteristics of Liquid Explosive Systems, US Bur. of Mines, Progr. Rept. No.8, Oct.-Dec. 1963 (Jan. 1964), 9 p., AD 431641, N64-16624. 119. MARXMANN, G. A., and M. GILBERT: Turbulent Boundary Layer Combustion in the Hybrid Rocket, United Techno!. Corp., Sunnyvale, Calif., WSS/Combustion Institute Paper 62-24 (Aug. 1962),39 p., see also 9th Symp. on Comb., Academic Press, N. Y. (1963), p. 371-83, N63-14904. 120. MOUTET, A., et M. BARRERE: Contribution a l'etude de la combustion dans les fusees a lithergol ou hybrides, International Series in Aeronautics and Astronautics Div. IX, Symposia, Vol. 7, Advances in Aero• nautical Sciences No.3, Pergamon Press (1961), p. 465-95. 121. McALEVY, R. F., and SUH YONG LEE: A Porous Plug Burner Technique for the Study of Composite Solid Propellant Defiagration on a Fundamental Level and Its Application to Hybrid Rocket Propulsion, AIAA-Preprint 63-496 (1963). 122. MOUTET, H., et M. PUGIBET: Augmentation de l'Impulsion Specifique des Lithergols par Addition d'Hydro- gene, ONERA TP 178(1964) et La Recherche Aerospatiale 101, 21-31 (1964), 123. MUELLER, K. H.: J. Am. Chern. Soc. 77, 3459-62 (1955). 124. MAKOVKY, A., and L. LENJI: Chern. Rev. 58,627-44 (1958). 125. MCCULLOUGH, I. P., et al.: J. Am. Chern. Soc. 76, 4791-6 (1954). 126. MEDARD, L.: Mem. Poudr. 1951, 125-35 (1951). 127. MUELLER, K. H.: Jet Propulsion 25,468-70 (1955). 128. McDONALD, C.: The Rate of Decomposition of Liquid Pentaborane from 85 ° to 202°C, NACA RM E55-H01 (21 Oct. 1955). 129. MORREY, J. R., and G. R. HILL: Kinetics and Mechanism of Diborane Pyrolysis, Utah Univ., Salt Lake City, TR 1, AFOSR, TN 58-220 (8 Jan. 1958). 137 p., AD 154121. 130. MAJOR, C. J.: Chern. Engng. Progr. 54: 3, 49-54 (March 1958). 131. MIKHAILOV, B. M.: Russian Chern. Rev. 31, 207 -224 (1962). 132. McDONALD, C.: The Thermal Stability of Pentaborane in the Range 329 to 419°F, NACA RM E54-G16 (Dec. 1956), 4 p. 133. MCCARTY, L. V., G. C. SMITH and R. S. McDONALD: Anal. Chern. 26,1027-31 (1954). 134. McDONALD, G. E.: Thermal Decomposition of Ethylpentaborane in Gas Phase, NACA RM E56-D26 (13 July 1956), 20 p., (Declass. 26 Febr. 1958). 135. MACKEY, D. R., H. J. BIRCH, and A. E. WEBER: Determination of Pentaborane Impurity in Hi-Cal-3, Callery Chemical Co., Rept. CCC-1024-TR-259 (8 Aug. 1957), 6 p., AD 207392. 136. MARSEL, J., and L. KRAMER: 7th Symp. on Combustion, Butterworths Sci:ntific Publications, London (1959), p. 906-12. 137. METZ, F. I., F. E. WELSH, and W. B. ROSE: EPR Spectrum of Liquid OF2, Am. Chern. Soc., Symposium on Advanced Propellant Chemistry 1965, Vol. 9, No.1, p. 237-44. 138. MCCULLOUGH, F., and H. P. JENKINS: 5th Symp. on Combust., Reinhold Publ. Corp., New York (1955), p.181-90. 139. Metal Hydrides Inc., Beverley, Mass.: Sodium Borohydride and Potassium Borohydride Manual (1958), Lithium Borohydride Tech. Bulletin 402-D (June 1958), Sodium Borohydride, Tech. Bulletin 502-H (Feb. 1958), Sodium Hydride Dispersed in Oil (1959), 20 p. 140. McBRIDE, W. R., and E. M. BENS: J. Am. Chern. Soc. 81, 5546 (1959). 141. McBRIDE, W. R., and H. W. KRUSE: US Pat. 3135800 (8. 4. 1957/2.6. 1964), Inh.: US Dept. of the Navy, CA 61, 4215e (1964). 142. MUSGRAVE, W. K. R.: Adv. in Fluorine Chern. 1,1-28 (1960). 143. MOULTON, J. F.: Small Scale Tests on Liquid Oxygen (LOX)-Alcohol Fuels, Naval Ordn. Lab., White Oak, Md., NOL Rept. 10301 (15 June 1949), 8 p., AD 120395. 144. MAIDEUX, F.: Bull. Soc. Chim. France 1962, 950-5 (1962). 145. MERAZ, D.: Feasibility Development of Variable Demand Liquid Propellant Gas Generator, Naval Ordn. Test Station, China Lake, Calif., NOTS TP 3234, NAVWEPS 8352 (Sept. 1963), 86 p., AD 427964. 146. MALONE, H. E.: The Evaluation and Calibration of the Nitric Acid Analyzer, Wright Air Dev. Center, Wright PattersonAFB, WADC Tech. Rept. 58-62 (May 1958), 33 p.,AD 207339, auch unter AD 52645. 147. MOYLE, M. P., and A. J. FEDOR: The Mechanism of Explosion Initiations in the Standard Impact Sensi• tivity Tester, Lehigh Univ., Inst. of Res., Bethlehem, Pa., Final Rept. RPL-TDR 64-61 (March 1964), 45 p., N 64-21408. 148. MARKELS, M., et al.: A Program to Advance the Technology of Fire Extinguishment (H2), Atlantic Res. Corp., Alexandria, Va., I: Interim Rept. Apr. 1961-March 1962, ASD TDR 62-526 (Sept. 1962), 65 p., AD 288077, N63-10149; II: Annual Rept. April 1962-March 1963, ASD TDR 62-526-P2 (March 1963), 69 p., AD 411396. Literaturverzeichnis M 753

149. MILEK, J. T.: A Bibliography on Hydrazine, North American Aviation, Inc., Downey, Calif., Rept. AL- 2332 (13 July 1956), 83 p., AD 143938. 150. MARTIN, M.: DAS 1113331 (30.7.59/31. 8.1961), Franz. Prior. 30. 7.1958, Ref.: CZ 1962, 10330. 151. MURACA, R. F., and L. J. TAYLOR: Phase Diagrams of Ternary Systems Containing Unsymmetrical Di• methylhydrazine, Water and JP-4 or Toluene, CIT-JPL Progr. Rept. 20-316 (29 March 1957), 8 p., AD 134864. 152. MURACA, R. F., S. P. VANGO, et al.: Field Method for Determination of Unsymmetrical Dimethylhydrazine and Water in NIKE Fuels, CIT-JPL Progr. Rept. 20-315 (29 March 1957), 11 p., AD 134652. 153. MALONE, H. E.: Determination of Hydrazine-1.1-Dimethylhydrazine Mixture, AFFTC Edwards AFB, Calif., AFFTC-TN-59-38 (Jan. 1960), AD 231372. 154. MESSINA, J.: Greases Nonreactive with Missile Fuels and Oxidizers, Frankford Arsenal, Philadelphia, Pa., Nat. Symp. of the Soc. of Aerospace Material and Process Engrs., Hollywood, Nov. 1962, FA-A63-10 (Sept. 1963). 10 p., N64-12705, AD 422788. 155. MALONE, H. E., and J. C. MELVILLE: Determination of Water in Rocket Fuels, Wright Patterson AFB, WADC Tech. Rept. 59-28 (23 Jan. 1959), 14 p., AD 208858. 156. MURACA, R. F., and F. CHANG: Evaluation of Monopropargylhydrazine and Unsymmetrical Dipropargyl• hydrazine as Rocket Fuels, CIT-Jet Propulsion Laboratory, Progr. Rept. 20-351 (22 Aug. 1958), 13 p., AD 205358. 157. MALLORY, H. D., and R. A. PLAUSON: Nature 195,1293-4 (1962). 158. MOlliENTHY, A. M.: Adv. Cryog. Engng. 9, 273-83 (1964). 159. MASSONNE. J., und R. HOLST: Angew. Chern. 78, 336 (1966). 160. MALM. J. G., et al.: Chern. Rev. 65,199-236 (1965). 161. MILLER, P. C.: Adv. Cryog. Engng. 10, 37 -45 (1965). 162. MURPHY, D. W.: Adv. Cryog. Engng. 10, 353-9 (1965). 163. MANSON, L.: Adv. Cryog. Engng.10, 297-304 (1965). 164. MARTIN, K. B., et al.: Adv. Cryog. Engng. 9, 146-52 (1964). 165. MUGNIER, D., and L. WElL: Adv. Cryog. Engng. 9, 98-103 (1964). 166. MILLER, W. S., J. D. SEADER, and D. M. TREBES: Forced Convection Heat Transfer to Liquid Hydrogen at Supercritical Pressures, Institut Internat. du Froid, Grenoble, France (Juin 1965). 167. MILLER, R. N., et al.: Properties of Foams, Adhesives and Plastic Films at Cryogenic Temperatures (LH2), Ind. Engng. Chern., Product Res. and Dev. 1, 257 -61 (1962). 168. MIDDLETON, R. L., J. M. STUCKEY, et al.: Adv. Cryog. Engng. 10, 216-23 (1965). 169. McKANNAN, E. C., and R. L. GAUSE: J. of Spacecraft and Rockets 2, 558-64 (1965); AIAA Paper 64-631. 170. MARSHALL, M. D., and L. L. LEWIS: DJcomposition of Nitronium Perchlorate, Am. Chern. Soc., Sympo• sium on Advanced Propellant Chemistry, Detroit (1965), Preprint of Papers, Vol. 9, No.1, p. 90-9. 171. MASTERS, A. 1.: Applicability of FLOX-Light Hydrocarbon Propellant Combinations as Liquid Rocket Propellants, AIAA-Paper 65-581 (June 1965), 16 p., J. of Spacecraft and Rockets 3,905-11 (1966). 172. MORRELL, J. C.: US Pat. 3153902 (4. 4.1961/27.10. 1964), Inh. nicht genannt, Ref.: CA 62, 5134c (1965). 173. MOUTET, A., et H. MOUTET: Patentanspruch DAS 1130343 (2.9.1960/24.5.1962), Franz. Prior. (2.9. 1959) FP 804079 und (12. 12. 1959) FP 812889, Inh.: ONERA. 174. MCCARTHY, J. R.: Chern. Engng. Progr., Symposium Series No. 41, Vol. 59, 201-7 (1963). 175. MASTERS, A. 1., and J. E. COLBERT: Rocket Testing of Four FLO X-Light Hydrocarbon Propellant Com• binations, AIAA-Paper 66-624, J. of Spacecraft and Rockets 3, 905-11 (1966). 176. MOSIER, S. A., R. E. DOTSON, and O. K. MOEHRBACH: Hypcrgolic Ignition of Light Hydrocarbon Fuels with Fluorine-Oxygen (FLO X) Mixtures, Combustion Institute, Western States Sect., Paper WSCI 65-23 (1965), 11 p., Ref.: CA 64, 4851 (1966). 177. McDERMOTT, C. E., R. R. BRESHEARS, and J. MCCAFFERTY: AIAA-Paper 66-949. 178. MARCUS, J. P., W. A. DAY, and J. G. JELINEK: Design and Development of an Elastomer Seal for Long• Term Hazardous Propellant Storage (N20 4), NASA-MSFC Conf. on Design of Leak.Tight Fluid Connectors 1965, p. 129-44, N 66-31420, N 66-31436. 179. METZER, T. H., and T. YAMAUCHI: Development of a Flexible Material Resistant to Nitrogen Tetroxide and Hydrazine, Illinois Inst. Tech., Chicago, Ill., IlTRI-U 6046-6, NASA CR-81645, (22 Dec. 1966) 105 p., N67-18000. 180. McKEE, H. C., and W. A. McMAHON: Analysis of Nitrogen Tetroxide Samples, Southwest Res. Inst., San Antonio, Tex., Contract NAS 9-5422, NASA CR-65372 (15 Apr. 1966) 31 p., N66-27049. 181. MARANO, D., and W. G. SCHECK: Development of Improved LOX Compatible Laminated Gasket Com• posite, NASA CR-79703 (Aug. 1966) 147 p., N67-10 900. 182. MARTIN, C. H.: The Freezing Points of Hydrazine-Ammonium Perchlorate Mixtures, Stanford Res. Inst., Menlo Park, Calif., SRI-ASD-6063, NASA CR-84856 (1 Apr. 1967), N67-31369. 183. MATHESON, J. C., et al.: Investigation of Light Hydrocarbon Fuels with FLOX as Liquid Rocket Pro• pellants, Pratt & Whitney, Final Rept. PWA-FR-2227, NASA CR-72147 (15 Sept. 1967) 149 p., ~67-35 368.

Dadieu-Damm-Schmidt, Raketentreibstoffe 48 754 Literaturverzeichnis N

1. NEUMARK, H. R.: Trans. Electrochem. Soc. Preprint 91-3. 2. National Bureau of Standards: Selected Values of Thermodynamic Properties, Ser. I, Nat. Bur. Stand. Washington D. C. (30 June 1947 to 31 March, 1950). 3. NAGARAJAN, G.: Bull. Soc. Chim. Belges 71, 337-46 (1962). 4. NEUGEBAUER, C., and J. L. MARGRAVE: J. Am. Chern. Soc. 79, 1338-40 (1957). 5. NASIAK, L. D., T. M. MYSKIEWICZ, and M. SOBENIAK: Thixotropic Propellants and Unit Operations, Bell Aerosystems Co., Rept. BLR 62-24 (C) Rev. A (Apr. 1963), 15 p. 6. NICHOLAISEN, B. H.: US Pat. 2773813, 2773814, 2773815 (11 Dec. 1956), Inh.: Olin Mathieson Chern. Corp., Ref.: CA 01, 4665f. 7. NICHOLAISEN, B. H.: Canad. Pat. 554659, 554658 (10.6.1954/18.3.1958), Ref.: CZ 1963, 4489. 8. North American Aviation, Missile Division, Downey, Calif.: Properties of Hydrazine, MRR·56·440 (1956). 9. NOEL, M. B.: Experimental Investigation of the Forccd·Convection and Nucleate·Boiling Heat Transfer Characteristics of Liquid Ammonia, CIT-JPL Tech. Rept. 32-125 (19 July 1961), 14 p. 10. National Bur. of Standards: Tables of Thermodynamic Properties of Ammonia, Nat. Bur. Stand. Circular No. 142 (19 Apr. 1923). 11. NEAT, W.: Interavia 12,929-30 (1957), vgl. auch: Wcltraumfahrt 8,74-6 (1957). 12. Anonym: Franz. Pat. 1149080 (5. 5. 1956/19. 12. 1957), Brit. Prior. v. 27. 7. 1955, Inh.: Napier & Son Ltd. 13. NEUMARK, H. R.: Trans. Electrochem. Soc. 1946/367-85. 14. NASH, L. K.: Anal. Chemistry 21, 980-2 (1949). 15. NEUMARK. H. R., and HOLLOWAY: Missiles and Rockets 57/9/97-9. 16. Inco (International Nickel Co., Inc.): Handling Fluorine and Fluorine Compounds with Inco Alloys, Inco Inc., New York, Tech. Bull. 17. N OEL, ~I. B.: Experimental Investigation of Heat Transfer Characteristics of Hydrazine and a Mixture of 90% Hydrazine and 10% Ethylenediamine, JPL Tech. Rept. 32-109 (27 June 1961), 18 p. 18. North American Aviation, Aerophysics Department: Rocket Research on Fluorine and Oxygen Mixtures, Bimonthly Progress Rept. No.2, Rep. Nr. AL-1824-2, Contract USAF 33(616)2134, E.O-R 539-46-E (1 Feb. 1954). 19. NEIN, M. E., and R. R. HEAD: Adv. Cryog. Engng. 7,244-50 (1962). 20. NOVOTNY, R. J.: Ammonia-Liquid Oxygen Studies, Reaction Motors Inc., Rept. RMI-440-F, Contract NOa(s) 51-710 (1 Dec. 1952),37 p., AD 4726. 21. NECHAEV, Yu. I.: Cryogenics 2, 175-6 (March 1962). 22. NICHOLSON, A. J. C.: J. Chcm. Soc. [Lond.] 1949, 1553-5 (1949). 23. NAHMANI, G., and Y. MANHEIMER: J. Chern. Phys. 24, 1074-7 (1956). 24. NEEDHAM, D. P., and J. POWLING: Proc. Roy. Soc. [Lond.] A 232,337-50 (1955). 25. NERAD, A. J., and D. T. HURD: US Pat. 2984830 (14. 7.1959), Inh.: General Electric Co., Ref.: CA 1909, 18447i. 26. NEWKIRK, A. E.: J. Am. Chern. Soc. 70, 1978 (1948). .' 27. NOLL, P. B.: The Handling of Boron Propellants for Liquid Rocket Engines, Proc. of the Propellant Thermodynamics and Handling Conf., Ohio State Univ., Engng. Exp. Station, Spec. Rept. 12 (1960) p. 89-98. 28. NOSOVA, V. V., et al.: Comb. and Flame 8, 163-4 (1964). 29. Anonym: Design and Development of the XSM-64 A Booster Liquid Oxygen Tank Vent Valve, North American Aviation, Downey, Calif., Rcpt. AL-2671 (5 Sept. 1957) AD 158018. 30. NEAL, A. E., and R. H. WARREN: Design, Development and Tcsting of a Liquid Hydrogen Tank Vcnt and Relief Valve, Rept. No. S60R1616 (Dcc. 1960), 143 p., Parker Aircr. Co., Los Angeles, Calif. (unclas• sif. rept.), Ref.: ASTIA TAB N61-3 (1961) AD 259086, Div. 27, p. 116. 31. NIENDORF, L. R., and O. J. NOICHL: Research of Production Techniques for Obtaining of over 50% Solid in Slush Hydrogen, Linde Co., Tonawanda (Feb. 1965), 110 p., AD 457753, N65-18170. 32. NASA: Sealed-Foam, Constrictive-Wrapped, External Insulation System for Liquid-Hydrogen Tanks of Boost Vehicles, NASA TN D-2685 (March 1965), 161 p. 33. NELSEN, F. M., and S. GROENNINGS: Anal. Chern. 30, 660-5 (1963). 34. NAGAI, C. K., et al.: Chamber Tcchnology for the Space Storable OF2-MMH Propellant Combination, AIAA Paper 66-623 (1966). 35. NORED, D. L., and H. W. DOUGLASS: Performance of JP-4 Fuel with Fluorine-Oxygen Mixtures in 1000- pound Thrust Rocket Engines, NACA RM E 58-C 18 (11 June 1958),35 p., Declassified 1966, N 66- 33309. 36. NASA: Handling Hazardous Materials, NASA SP-5032 (Sept. 1965), 93 p. 37. NYE, H. H., and D. W. MOORMAN: J. of Spacecraft and Rockets 0, 139-45 (1968). 38. NEIN, M. E., and J. F. THOMPSON: Experimental and Analytical Studies of Cryogenic Tank Pressurant Requirements, NASA TN D-3177 (Feb. 1966) 111 p., N66-16938. Literaturverzeichnis OIP 755 o 1. ORDlN, P, M,: Experimental Performance of Chlorine Trifluoride and Hydrazine Propellant Combination in 100 pound Thrust Rocket Engine, NACA RM E9-F01 (Aug. 1949), 22 p. 2. OLSON, E. C.: Anal. Chern. 32, 1545-7 (1960). 3. ORYSH, M. S., L. L. GRUSS, and A. GALLACCIO: Pitmann-Dunn Labs., Tech. Rept. R 1524 (1960), Ref.: Corrosion A 1: 4,168 (1962) und: Werkstoffe u. Korrosion 14,319 (1963). 4. OLAH, G. A., and S. J. KUHN: US Pat. 3103782 (7.11.1960/17.9.1963), Inh.: Dow Chern. Co., Ref.: CA 60, 2718g (1964). 5. Olin Mathieson C. C.: Monomethyl Hydrazine, Product Booklet AD·1198·361. 6. OVERSTREET, R., and W. F. GIAUQUE: J. Am. Chern. Soc. 59, 254-9 (1937). 7. OBERST, F. W., C. C. COMSTOCK, and E. B. HACKLEY: AMA Arch. Ind. Hyg. Occ. Med. 10, 319-27 (1954). 8. OLIVIER, J. R., and W. E. DElI1PSTER: Orbital Storage of Liquid Hydrogen, NASA TN D-559 (Aug. 1961), 69 p. 9. O'DONNELL, P. M., and A. E. SPAKOWSKI: Reaction of Copper and Fluorine from 800 to 1200°F, NASA TN D·768 (April 1961), 15 p. 10. ORDIN, P. M., E. A. ROTHENBERG, and W. H. ROWE: Investigation of LiquidFluorine andHydrazine• Ammonia·Mixture in 100 Pound Thrust Rocket Engine, NACA RM E 52-H 22 (Oct. 1952), 35 p., Declass. FebI'. 1961. 11. OLSON, W. T.: ARS-J. 32, 672 (1962) and ARS-Preprint 2266-61. 12. OTTO, E. W., and R. A. FLAGE: Control of Combustion Chamber Pressure and Oxidant-Fuel Ratio for a Regeneratively Cooled Hydrogen and Fluorine Rocket Engine, NASA TN D-82 (Nov. 1959), 61 p. 13. OTTO, E. W., and R. A. FLAGE: Studies of Combustion Chamber and Feed System Stability During Thrott• ling of a Regeneratively Cooled Liquid Hydrogen and Liquid Fluorine Rocket Engine, Am. Soc. Automotive Engrs. Preprint 246B (Od. 1960). 14. ORDlN, P. M., H. W. DOUGLASS, and W. H. ROWE: Investigation of the Liquid Fluorine-Liquid Diborane Propellant Combination in a 100 Pound Thrust Rocket Engine, NACA RM E51-I04 (1951). 15. ORDlN, P. M., S. WEISS, and H. CHRISTENSON: Adv. Cryog. Engng. 5, 481-6 (1960). 16. OLSON, W. T., and P. C. SETZE: 7th Symp. on Combustion, Butterworths Scient if. Publications, London (1959), p. 883-93. 17. OSBORN, G., and B. JONES: Development of Use of Hydrazine Fuel in the XLR 16-AJ-2 Rocket Engine, Aerojet Engng. COIp., Azusa, Calif., Progr. Rept. 2018-11 (25 Sept. 1950), AD 204536. 18. O'HANLON, T. W.: Zero-g Report on Liquid Hydrogen Nucleate Boiling, General Dynamics/Astronautics, Rept. 55D859-1 (2 FebI'. 1962). 19. OLSEN, W. A.: Adv. Cryog. Engng. 8, 342-59 (1963). 20. OSBORG, H., D. HORVITZ, and A. H. POPE: US Pat. 2955032 (4. 10. 1960). Rd.: CA 55, 3063b. 21. ORDAHL, D. D.: Astronautics 4: 10,48-9,84 (1959). 22. Olin Mathieson C. C.: Pentaborane, Olin Mathieson C. C., New Haven, Conn., Tech. Bull. LF-202 (June 1960). 23. ONIAK, T. P., and F. J. GERHART: Inorg. Ch(m. 1: 4, 742-4 (1962). 24. OLAR, G. A.: US Pat. 3141295 (12.4. 1961/21. 7. 1964), Ref.: CA 61, 9349f. (1964). 25. OGIMACHI, N., J. M. CORCORAN, and H. W. KRUSE: Thermal Analysis of Systems of Hydra:dne with Propyl Alcohol, Isopropyl Alcohol and Allyl Alcohol, Naval Ordn. Test Station, Inyokern, China Lake, Calif., NA VORD Rept. 3351 (25 June 1954), 11 p., AD 51887. 26. OSBORG, H., D. HORVITZ, and A. H. POPE: DSPat. 3133845 (19.8.1960/19.5.1964), Ref.: CA61, 5444c (1964). 27. ODINZOW, W. A.: Detonationsgeschwindigkeit im Gemisch C(N02)4/Dieselkraftstoff (in Russisch), Sch. priklad. chim. DSSR 34, 1092-6 (1961), REf.: CZ 1964: 21, 277. Ref. 2776. 28. OLSEN, R. E., D. W. FISH, and E. E. HAMEL: Synthetic Applications of Nitronium Tetrafluoroborate, Am. Chern. Soc., Symposium on Advanced Propellant Chemistry, Detroit (1965), Preprint of Papers, Vol. 9, No.1, p. 43-55. 29. ORDARL, D. D., and W. A. RAINS: J. of Spacecr. and Rockets 2, 923-6 (1965). 30. OBERSTONE, J.: The Application of Packaged High Energy Propellant Reaction Control Systems, AIAA Paper 66-947 (1966), 13 p. 31. OSlI10N, R. D.: Am. Inst. Chern. Engrs., Chern. Engng. Progr., Symposium Series 61, 92-102 (1966), Ref.: CA 64, 19302 (1966). 32. ORR, J. W., and W. E. CRANE: A Large-Scale LF2 Flow Facility Testing Program, AlAA Paper 68-249 (1968).

P 1. PIERCE, L., and E. L. PACE: J. Chern. Phys. 23, 551-5 (1955). 2. Pennsalt: Permsalt Starting to Talk About Its Perchloryl Fluoride, Chern. Week 191)8, p.71 (23 Aug. 1958). 3. Pennsalt Chemical, Philadelphia: Perchloryl Fluoride, Product Booklet DC 1819 (1957).

48* 756 Literaturverzeichnis P

4. PRIAPI, J. J.: Hypergolic Systems for the Ignition of Large Solid Propellant Rocket Motors, ARS-Preprint 1463-60 (Dec. 1960). 5. PEREGUD, E. A., i B. S. BOIKINA: Mikromethode zur Bestimmung von Fluormonoxyd (in Russisch), Sch. analititschesskoi chimii 14: 1, 141-2 (1959). 6. PANKRATOV, A. V.: Chemistry of Some Inorganic Nitrogen FluorideR, Russian Chem. Reviews 32, 157-65 (1963), Ubersetzg. von: Usspechi Chimii 32,336-53 (1963). 7. PETERS, M., and J. HOHMAN: Ind. Engng. Chem. 47, 2536-9 (1955). 8. PINKERTON, M. K., and A. A. THOMAS: Ultra Micro Procedure for UDMH in Blood, Wright Patterson AFB, Aerospace Med. Div., 6570 th Aerospace Med. Res. Labs., Final Tech. Doc. Rept. AMRL 62-120 (Oct. 1962), 8 p., N 63-10187. 9. PERLEE, H_ E., et al.: J. Chem. Engng. Data 7, 377 -9 (1962). 10. PORTER, R. W.: Chem. Engng. 00: 4,102 (1948). 11. PENNEl\iAN, R. A., and L. F. AUDRIETH: Anal. Chem. 20, 1058-61 (1948). 12. PETERS ElM, F.D., and J. \V. CLEGG: Behavior of Commercial Hydrazine in Contact with Various Materials, Battelle Mem. Inst .. Projcct RAND (1950), Unclassified LPH 80. 13. PRESCOTT, B., G. KAUFFMANN, and W. D. JAMES: AMA Arch. Ind. Health 13, 34-6 (1956). 14. PIERCE, L .. and E. L. PACE: J. Chem. Phys. 22,1271 (1954). 15. PLANK, C. J., and H. HUNT: J. Am. Chem. Soc. 61, 3590-1 (1939). 16. PURANIK, P. G., and E. Y. RAO: Potential Constants and Calculated Thermodynamic Properties of N02F and N02Cl, Indian J. Phys. 30,177-82 (1961). 17. PLATZ, G. M., and C. K. HERSH: Ind. Engng. Chem. 48, 742-4 (1956). 18. PETTERS, W. J.: Raketentechnik u. Raumfahrtf. 1, 78-9 (1957). 19. PITSKHELAURI, E. W., and V. V. YASTREBOV: Physical Chemistry of Concentrated Ozone V: The Dielectric Constant of Liquid Ozone and Its Solution in Oxygen, Russian J. Phys. Chem., Abstracts Issue 33, 18 (1959), Originalstelle: Sch. Fiz. Chimii 33: 4, 790-2 (1959). 20. PROSAD, S.: Brit. J. Appl. Phys. 3, 58-9 (1952). 21. PUNTE, C. L., L. Z. SAUNDERS, and E. H. KRACKOW: Jet Propulsion 26, 500-1 (1956). 22. PECKHAM, H. M., and R. L. HAUSER: Adv. Cryog. Engng. 4, 26-46 (1960). 23. POWELL, W. B.: Jet Propulsion 27,776-83 (1957) und JPL Progr. Rept. 20-285 (April 1956). 24. PARKER, W. G., and G. RUSTON: The Merits of Using High Energy Propellants, in: The Chemistry of Pro• pellants, Ed.: S. S. PENNER and J. DUCARME, Pergamon Press 1960, p. 556-78. 25. PASTUHOV, A., and C. L. JEWETT: Liquid Hydrogen Liquefaction and Its Field Use, ARS-Preprint 207 -55 (1955). 26. PINKSTON, J. T.: Ind. Engng. Chem. 39, 255-8 (1947). 27. PRIEM, R. J., and M. F. HEID~iANN: Propellant Vaporization as a Design Criterion for Rocket Engine Com• bustion Chambers, NASA TR R-67 (1960), 55 p. 28. PRICE, H. G., and H. W. DOUGLASS: Materials of Compatibility with Fluorine, NACA RM E56-K21 (19 Nov. 1956), 5 p. 29. PRICE, H. G., and H. W. DOUGLASS: Nonmetallic Compatibility with Fluorine, NACA RM E57-G18 (2 Oct. 1957), 7 p. 30. PRIEST, H. F., and A. V. GROSSE: Ind. Engng. Chem. 39, 279-80 (1947). 31. PROUT, W. E., and R. C. ANDERSON: Fuel 33, 125-33 (April 1954). 32. PINNS, M. L., et al.: NACA Research on Slurry Fuels, NACA Report 1388 (1958), 24 p. 33. PANKRATOV, A. V., i E. JA. KANANOVA: Russian J. inorg. Chem. 7, 897-8 (1962). 34. PRIEST, H. F., and A. V. GROSSE: Ind. Engng. Chem. 39, 431-3 (1947). 35. PANNETIER, G., et P. MIGNOTTE: Bull. Soc. Chim. France 1961, 1380-3 (1961). 36. PANNETIER, G., et P. MrGNOTTE: Bnll. Soc. Chim. France 1961,982-5 (1961). 37. PANNETIER, G., et P. MIGNOTTE: Bull. Soc. Chim. France 1961,985-8 (1961). 38. PERKINS, W. E., and R. J. FRAINIER: Adv. Cryog. Engng. 0,69-74 (1960). 39. POPE, D. H., W. R. Kn,LIAN, and R. J. CORBETT: Adv. Cryog. Engng. 0, 441-9 (1960). 40. PLATT, G. K., and C. C. WOOD: Adv. Cryog. Engng. 7, 296-302 (1962). 41. PETTEY, T. M.: Jet Propulsion 26, 474-9 (1956). 42. PRICE, F. P.: J. Am. Chem. Soc. 72,5361-5 (1950). 43. POLING, E. L., and H. P. SIMONS: Ind. Engng. Chem. 50,1695-8 (1958). 44. PARKER, W. G., and H. G. WOLFHARD: Fuel 35, 323-32 (1956). 45. PARKER, W. G., and H. G. WOLFHARD: Some Characteristics of Flames Supported by NO and N02, 4th Symp. on Combust., Williams and Wilkins Comp., Baltimore (1953), p. 420-8. 46. PANKRATOV, A. V., and L. A. BROBYSHEVA: Russ. J. Phys. Chem. No. 0, 475-8 (1961). 47. POOLE, D. R., and W. M. GRAVEN: J. Am. Chem. Soc. 83, 283-6 (1961). 48. POTTER, R. L.: Comb. and Flame 2, 129-36 (1958). 49. PINO, M. A.: Liquid Rocket Fuels, Calif. Res. Corp., Final Rept. Oct. 1951 - June 1953, Contract NOa(s} 52-034-c (20 Jan. 1954), 106 p., AD 17796. 50. PEDERSEN, C. J.: US Pat. 3038299, 3038300, Inh.: DuPont de Nemours & Co. (15. 12. 1953/12.6. 1962), Ref.: CA 07,10094£. Literaturverzeichnis P 757

51. Pennsalt Chemical, Philadelphia: Amines, Tech. Information Bulletin S-129B (1961). 52. PECK, M. V., et al.: Research in Hybrid Combustion, Rocketdyne Quart. Repts. BELL, R E., M. V. PECK, and W. H. MOBERLY: Quart. Rept. R-2267-3 (6 April 19(1). PECK,]VI. V., and R M. LODWIG: Quart. Rept. R-2267-4 (30 June 1961). PECK, ]VI. V., and R M. LODWIG: Quart. Rept. R-2267-5 (30 Sept. 1961),23 p., AD 264788, Ref.: ASTIA TAB 62-1-1, p. 51. PECK,]VI. V.: Summary Rept. 1 Dec. 1960 - 30 Nov. 1951, R-3446 (30 Jan. 19(2), ;")7 p., AD 271674. PECK, M. V., and T. HOUSER: Quart. Rept. R-2267-7 (30 June 1962). PECK, ]VI. V., and T. HOUSER: Quart. Rept. R-2267-8 (16 Jan. 1963),28 p. HOUSER, T.: Final Rept. 1 Dec. 1961 - 31 Jan. 1963, R-5179 (15 May 19(3), 45 p. 53. PANNETIER, G., et R DE HARTOULARI: Compt. rend. 244, 3155-7 (1957). 54. PARKER, W. G.: Comb. and Flame 2, 69-81 (1958). 55. PRATT, R, M. S. B. MUNSON, and R C. ANDERSON: Exploratory Studies of the Acetylene-Ethylene Oxide Combustion Systems, Texas Univ., Austin, Tech. Note 33, OSR TN 56-502, Contract AF 18(600)430 (Oct. 1956),7 p., AD 110317. 56. PINNS, M. L.: Effect of Surface-Active Additives on Physical Properties of Slurries of Vapor-Proccss Magne• sium, NACA RM E55-H26 (3 Nov. 1955), Declassified 20 June 1957, 22 p. 57. PRIEM, R. J., and B. J. CLARK: Comparison of Injectors with a 200 Pound-Thrust Ammonia-Oxygen Engine, NACA RM E57-H01 (4 Sept. 1958), 10 p., N63-12544. 58. PASS, 1., and A. O. TISCHLER: Effect of Fuels on Screaming in 200 Pound-Thrust Liquid-Oxygen-Fuel Rocket Engine, NACA RM E56-CI0 (22 June 1956), 25 p., Declassif. 3 Sept. 1958. 59. Peenemiinde Archiv Nr. 124/4: Zusatzstoff zur Schmelzpunkterniedrigung von Tetranitromethan. 60. POLLARD, F. H., H. S. B. MARSHALL, and A. E. PEDLER: Trans. Farad. Soc. 52, 59-68 (1956). 61. POWLING, J., W. A. W. i:-iMITH, and J. THYNNE: Comb. and Flame 4,201-11 (1960). 62. POWLING, J., and W. A. W. SMITH: Comb. and Flame 1,308-20 (1957). 63. PARRY: The Chemistry of Boron Hydrides and Related Hydrides, Wright Air Dev. Center, WADC Tech_ Rept. 59-207 (May 1959), 178 p. 64. PROSEN, E. J., W. H. JOHNSON, and F. Y. PERGIEL: J. Res. Nat. Bur. Stand. 61. 247-50 (1958). 65. PONDY, P. R., and H. C. BEACHELL: J. Chern. Phys. 25, 238-41 (Aug. 1956). 66. PARIDON, L. J., and G. E. MACWOOD: J. Phys. Chern. 63,1997-9 (Dee. 1959). 67. PRICE, F. P.: J. Am. Chern. Soc. 73, 2141-44 (1951). 68. POUSTIAN ••J. E., and J. R GOULD: US Pat. 2977387 (28.9.1955/28.3.1961), Ref.: CZ 1962.16194. 69. POWERS, J. V., Internat. Adv. Cryog. Engng. 10 MU, 458-63 (1965). 70. POLAK, R J., and C. OBERLAND: IEC Prod. Res. and Development 3,234-9 (1964). 71. PARIBOK, W. P., i N. W. GROCHOLSKAJA: Toxizitat von NO und N02 (in Russisch), Pharmakol. II. Toxiko• logie USSR 25, 741-() (1962), l{,ef.: CZ 1963, 20500. 72. PIZZOLATO, P. J., and C. C. FATINO: Evaluation of the Mechanism of Corrosion in Capillaries, Martin Co., Orlando, Fla., Rept. ME-531 (4 March 1964), N64-21815, AD 433622. 73. PILZ, W.: Unveroffentlichte Versuche, Forsclmngsinstitut fiir Physik del' Strahlantriebe, Stuttgart-Flug- ~. . 74. PERLEE, H. E., 1. LIEB:I'IAN, and ]VI. G_ ZABETAKIS: Review of Fire and Explosion Hazards of Flight Vehicle Combustibles, Suppl. 2, Bur. of Mines, Pittsburgh, Annual Rept. ASD TR 61-278 (Apr. 1963), 58 p .. N63-21403, AD 417126. 75. PETERS, R L.: Lubrication of Rocket Engine Pumps Utilizing High Energy Propellants, Sci. Lubrication (London) 14: 4, 26-9 (19H2). 76. PLESCIA, O. J., and R M. MANTELL: US Pat. 2926144 (12. 2. 1949/23.2. 1960), Inh.: M. W. Kellog Co., Ref.: CZ 1962, 4048. 77. POWELL, W. B., J. P. IRVING, and M. E. GUENTHER: Chlorine Trifluoride-Hydrazine Liquid Propellant Evaluation and Rocket Motor Development, CIT-JPL Tech. Rept. 32-305 (15 May 1963), 57 p., N63-21722. 78. POTTER, R L., and H. W. BYINGTON: Unsymmetrical Dimethyl Hydrazine as a Starting Fluid for Nitric Acid - Jet Fuel Rocket Engincs, ARS-Preprint 3:~0-56 (1956). 79. PINO, M. A., and P. C. CONDIT: US Pat. 2940250 (27.1. 1954/14.6.1960), Inh.: Calif. Res_ Corp., San Francisco, Ref.: CZ 1962, 3692. 80. PERKINS, P. J., M. A. COLALUCA, and L. S. SMITH: Adv. Cryog. Engng. 9,38-45 (1964). 81. POTTER, J. A., and F. Z. BRILL: Adv. Cryog. Engng. 9, 284-91 (1964). 82. PERKINS, C. K., and J. A. PETROWSKI: Adv. Cryog. Engng. 10, 278-82 (1965). 83. PERROUD, P., J. REBIERE et L. 'VEIL: Convection Forcee de l'Azote et de I'Hydrogime Liquides, Inst. Internat. du Froid, Grenoble (Juin 1965) Preprint, CEN Grenoble Note CENG/ASP 65-07. 84. PAIVANAS, J. A., O. P. ROBERTS, and D. I.-J. WANG: Adv. Cryog. Engng.10, 197-107 (1965). 85. PERKINS, P. J.: Exp. Study Under Ground-Hold Conditions of Several Insulation Systems for Liquid Hydrogen Fuel Tanks of Launch Vehicles, NASA TN D-2679 (March 1965). 86. POWERS, J. C., D. W. VOSE, and E. A. SULLIVAN: Attempted i:-iynthesis of BeH2, WADD-TR60-543, Con• tract AF 33(616)5847 (Oct. 1960), 29 p., AD 249398. 758 Literaturverzeichnis R

87. PERRY, D. D., et al.: Am. Chem. Soc., Symposium on Advanced Propellant Chemistry, Preprint of Papers Vol. 9, No.1 Detroit (1965)), p. 118-27. 88. PENZIAS, G. J.: An Atlas of Infrared Spectra of Flames, Part 4: Additional Nitrogeneous Liquid Fuels and Oxidizers, Warner and Swasey Co., Flushing, N. Y., (Oct. 1964),62 p.,AD 452631, N65-17443. 89. PANNELL, C. E., and P. D. OJA: Bipropellants from Hydrazinoalkanes and Hydrazines, US Pat. 3219500, Dow Chemical Co. (7.6. 1962/23. 11. 1965), Ref.: CA 64, 3276 (1966). 90. PUTT, J. W., and T. K. RICE: US Pat. 3 212255 (7.10.1963/19.10.1965). 91. PANOSIAN, J. 0.: Development of a Fluorine/Hydrogen Injector, AIAA Paper 66-625 (1966). 92. PRICE, H. G., R. J. LUBICK, and A. M. SHINN: Investigation of Injectors for a Low-Chamber-Pressure Hydrogen-Fluorine Rocket Engine, NASA-TM-X-485 (July 1962) 30 p., Declassified N 66-33333. 93. Anonym: RL 10 A-3·3 Rocket Engine, Pratt & Whitney Aircr., Design Rept. PWA-FR-1769, NASA CR-80920 (28 Febr. 1966), N 67-14800. 94. PARTEL, G.: Riv. Ing. 16, 969-76 (1965) (in Italienisch). 95. PILIPOVICH, D., et al.: Inorg. Chem. 6, 1918-9 (1967). 96. POOLE, D. R., and D. G. NYBERG: J. Sci. Instr. 39, 576 (1962). 97. PES ANTE, R. E., and M. NISmBAYAsm: Evaluation of the Blast Parameters and Fireball Characteristics of LOX/LH2 Propellant, Aerojet Gen. Corp., AG-0954-01-FP, NASA CR-65651 (7 Apr. 1967) 138 p., N67-32112. 98. PERKINS, H.: Effects of Various Additives on Physical Properties and Performance of MMH, NASA TM X-53356 (3 Nov. 1965) 18 p., N66-16155. 99. PORTER, R. N., et al.: Advanced Liquid Propulsion Systems, JPL Space Programs Summ. 37 -33, Vol. IV, p. 162-71 (June 1965), N65-32442. 100. PERLEE, H. E., et al.: J. of Spacecraft and Rockets 5,233-4 (1968).

R

1. RUFF, 0., J. FISCHER und F. LUFT: Z. anorg. Chem. 172, 417 -25 (1928). 2. RUFF, 0.: DR Pat. 518202 (1930), Ref.: CA 25, 2376 (1931). 3. RUFF, 0.: Z. anorg. Chern. 197, 273 (1931). 4. ROGERS, H. H.: Ind. Engng. Chem.51, 309-10 (1959). 5. RUFF, 0., und W. MENZEL: Z. anorg. Chern. 190, 257 (1930). 6. RUFF, 0., und W. MENZEL: Z. anorg. Chem. 198, 39 (1931). 7. ROHRBACK, G. H., and G. H. CADY: J. Am. Chem. Soc. 69, 677 (1947). 8. RUFF, 0., W. MENZEL und W. NEUMANN: Z. anorg. allg. Chem. 208, 293 (1932). 9. Rocketdyne, a Div. of North. Am. Av. Inc.: Theoretical Performance of Rocket Propellants (a chart), Rocketdyne Publication 573-A-2. 9a. Rocketdyne: Theoretical Performance of Rocket Propellants (a chart), Rocketdyne Pub!. 505-X (Revised 1 Jan. 1959). 10. RIEHL, W. A., H. PERKINS, and others: ARS-J. 32, 384-7 (1962). 11. ROGERS, H. H., J. H. JOHNSON, and S. EVANS: Research in Fluorine Chemistry, Rocketdyne Reports, a) Progr. Rept. R-334-19 (10 Oct. 1962), Ref.: NASA TPA N62-17096, b) Progr. Rept. R-334-20 (8 Jan. 1963),34 p., Ref.: NASA STAR N63-11831, c) Summary Rept. R 5077 (30 Apr. 1963). 12. ROLLBUHLER, R. J., and W. A. TOMAZIC: Comparison of Hydrazine-Nitrogen Tetroxide and Hydrazine• Chlorine Trifluoride in Small-Scale Rocket Chambers, NASA TN D-131 (1959), 16 p. 13. RICHTER, G. N., H. H. REAMER, and B. H. SAGE: Ind. Engng. Chern. 45, 2117 (1953). 14. REAMER, H. H.: Ind. Engng. Chem. 46, 1471-3 (1954) Supplementary Material: American Documenta" ti,m lnst., Wash., Doc. 4199. 15. Ross, D. H.: J. ARS 20, 24-31 (1950) und ARS Preprint 9-49 (1949). 16. RANDOLPH, C. L., and R. E. MEYER: US Pat. 3050560 (15. 2. 1954/21. 8.1962), Inh.: Aerojet-Gen. Corp., CA 57, 16954 (1962), fermr: Brit. Pat. 835416 (21. 6.1956/18.5.1960), CZ 1963, 15984-5. 17. ROSE: Jet Propulsion 26, Supplement Part II, 305-315 (Oct. 1956). 18. ROTHBERG, S., and COPE: Toxicity Studies on Hydrazine, Monomethyl Hydrazine, Dimethyl Hydrazine and Nitrosodimethylamine, Chemical Warfare L'tbs., Army Chem. Center, Md., Rep. CWLR-2027 (April 1955). 19. ROSSER, W. A.: Gas Ph'tse Oxidation of NHa by N02, CIT-JPL Progr. Rept. 20-273 (Oct. 1955), 13 p. 20. ROSSER, W. A., and H. WISE: J. Chem. Phys. 25, 1078-9 (1956). 21. ROSSER, W. A., and H. WISE: J. Chem. Phys. 26, 571-6 (1957). 22. ROSSER, W. A.: Kinetics of the Hydrogen + Nitrogen Dioxide Reaction, CIT-JPL Progr. Rept. 20-282 (D3c. 1955), 14 p. 23. ROBERTSON, G. D., D. M. MASON, and W. H. CORCORAN: J. Phys. Chem. 59, 683-90 (1955), Supplemen• tary Material: Am. Doc. Inst., Washington, D. C., Document 4550. 24. ROBERTSON, G. D., D. M. MASON, and W. H. CORCORAN: Ind. Engng. Chem. 47,1470-2 (1955) undCIT• JPL Progr. Rept. 20-176 (Aug. 1953), 8 p. LiLeraturverzeichnis R 759

25. RYKER, D. W., and O. J. SWENSON: US Pat. 2740692 (3. 4.1956) Inh.: Olin Mathieson C. C., Ref.: CA 50, 9699i; vg!. auch DBP 1072599 (7.1. 1960). 26. ROBELL, J.: DAS-DBP. 1084250 (Ang. 30. 6. 1960). 27. RYKER, O. W., and J. E. TROJAN: Petroleum Refiner 33: 12, 166 (1954). 28. Rocketdyne: Hydrazine Handling Manual, Rocketdyne, Canoga Park, Contract AF 33(616)6939, Project 3148, Task 30196, Rept. R-3134 (Sept. 1961),57 p., AD 266145. 29. Rocketdyne: Mechanical System Design-Criteria Manual for Hydrazine, Rocketdyne, Canoga Park, Rept. R-3130 (Sept. 1961),79 p., AD 266144.

30. Rocketdyne: Research on the Hazard Classification of New Liquid Rocket Propellants, Vo!' I (N20 4 , CIF3, N2H 4 , BSHg), Rocketdyne Rept. R-3217 (Oct. 1961),258 p., AD 272025, Vo!' II: Rept. R-3217 (Oct. 1961), 170 p., AD 272026. 31. REAMER, H. H., W. H. CORCORAN, and B. H. SAGE: Ind. Engng. Chem. 45, 2699-704 (1953) und CIT• JPL Progr. Rept. 20-184 (8 Oct. 1952). 32. ROBERTSON, G. D., D. M. MASON, and B. H. SAGE: Ind. Engng. Chem. 44, 2928-30 (1952). 33. REAMER, H. H.: Volumetric and Phase Behavior in Part of the HN03/N02fH20-System, CIT-JPL Progr. Rept. 20-328 (July 1957), 34 p. 34. REAMER, H. H.: Volumetric and Phase Behavior in the HN03fN02/H20-System, CIT-JPL Progr. Rept. 20-270 (July 1955), 20 p. 35. REAMER, H. H., W. H. CORCORAN, and B. H. SAGE: Ind. Engng. Chem., Chem. and Engng. DataSeries 1, 24-9 (1956). 36. REAMER, H. H., and D. M. MASON: Ind. Engng. Chem. 45,1094-7 (1953). 37. REESE, B. A., and R. W. GRAHAM: Jet Propulsion 24,228-36 (1954). 38. REESE, B. A., and R. W. GRAHAM: Experimental Investigation of Heat Transfer and Fluid-Friction Characteristics of WFNA, NACA TN 3181 (May 1954). 39. RITTENHOUSE, W., and D. M. MASON: Chemical Factors Affecting Corrosion of Carbon Steel AISI-l020 by Liquid Phase Fuming Nitric Acid, CIT-JPL Memo 20-147 (Oct. 1957), 31 p. 40. RITTENHOUSE, J. B., et a!.: Corrosion and Ignition of Ti-Alloys in Fuming Nitric Acid, Wright Patterson AFB, Wright Air Dev. Center, Tech. Rept. TR 56-414 (Febr. 1957), 57 p., AD 118028. 41. ROSSANO, A. T.: J. Industr. Hyg. 27, 207 -8 (Sept. 1945). 42. ROTHBERG, S., and M. H. WEEKS: Acute Toxicity of a Mixed Hydrazine Fuel (MHF-l), Army Chem. Res. and Dev. Labs., Army Chem. Center, Md., Rept. No. C RDLR 3104 (Nov. 1961), 11 p., AD 272069. 43. REINHARDT, T. F., R. L. POTTER, and F. M. MOORE: Heat Transfer Properties of Anhydrous Ammonia, OASD Res. and Dev., Liquid Propellants Symposium March 27-28, (1957), p. 85ff. 44. RICKETSON, B. W. A.: Density of Liquid Oxygen Between 90° and 105°K as a Function of Pressure and Temperature, Rocket Propulsion Establishment, Gt. Brit., RPE Tech. Memo 249 (Febr. 1962), 6 p., AD 272892. 45. ROTH, K M., and E. S. SHANLEY: Ind. Engng. Chem. 45, 2343-9 (1953). 46. RIEHL, W. A., J. R. NUNNELY, and D. D. WATSON: Methods of Analysis for Hydrogen Peroxide, Red• stone Arsenal Rept., Ordn. Missile Labs., Rept. 1 R 1 (1 May 1954), 69 p., AD 33004. 47. RUNCKEL, J. F., C. M. WILLIS, and L. B. SALTERS: Investigation of Catalyst Beds for 98% Concentration H20 2, NASA TN D-1808 (June 1963), 80 p. 48. RucclA, F. E., and C. M. MOHR: Adv. Cryog. Engng. 4, 307-18 (1960). 49. ROBIN, C. D.: Experience with Handling Liquid Hydrogen in Engine Testing, Proc. of the Propellant Thermodyn. and Handling Conf., Ohio State Univ., Spec. Rept. No. 12 (June 1960), p. 75-87. 50. REYNALES, C. H.: Adv. Cryog. Engng. 6,117-29 (1961). 51. ROBISON, W. C.: Jet Propulsion 24,112 (1954). 52. RUFF, 0.: Die Chemie des Fluors, Springer-Verlag, Berlin, 1920. 53. RUDGE, A. J.: Chern. and Ind. 1956, 504-11. 54. REUEL, N. C., and J. FRIEDMAN: Liquid Rocket Design Manual Rept. AI-259, Missile Division, North American Aviation Inc. (1947), unclass. 55. ROLLBUHLER, R. J.: The Disposal of Fluorine, Proc. of the Propellant Thermodynamics and Handling Conf., Ohio State Univ., Special Rept. No. 12 (1960), p. 259-66. 56. ROLLBUHLER, R. J., G. R. KINNEY, and L. C. LEOPOLD: Field Experiments on Treatment of Fluorine Spills with Water or Soda Ash, NASA TN D-63 (Sept. 1959), 14 p., 2 tab!., 12 refs. 57. ROGERS, J. D., K. ZEIGLER, and P. MCWILLIAMS: J. Chem. Engng. Data 7,179-82 (1962). 58. ROBERTSON, W. W., N. B. HUMPHREY, and R. D. ANDERSON: J. Chern. Phys. 21. 2093-4 (1953). 59. RINEHART, W. T., and C. S. COE: Physical Properties of JP-4 and JP-5 Fuels, North Americ. Aviation, NAA Memo APA 54-62 (9 July 1954). 60. RINEHART, W. T.: Thermodynamic and Physical Properties of JP-5 Estimated for Wide Temperature and Pressure Range with Particular Emphasis on Critical and Supercritical Regions, North Americ. Aviation, NAA Memo PDM-55-88 (10 June 1955). 61. ROSENBAUM and LEVITT: Thermodynamical Properties of Hydrogen from Room Temperature to 100000 OK, NASA TN D-1107 (Jan. 1962). 41 p. 62. ROGERS, H. H., S. EVANS, and J. H. JOHNSON: J. Electrochem. Soc. 111, 701-4, 704-7 (1964). 760 Literaturverzeichnis R

63. RUNDLE, R. E.: J. Am. Chem. Soc. 85, 112-3 (1963). 64. RAGOZIN, N. A.: Jet Propulsion Fuels, Translated by W. E. JONES, Edited by B. P. MULLINS, Pergamon Press, Oxford-London-New York 1961. 65. ROTHENBERG, E. A., and P. M. ORDlN: Preliminary Investigation of Performance and Starting Charac• teristics of Liquid Fluorine and Liquid Oxygen Mixtures with Jet Fuel, NACA RM E53·J20 (1954). 66. ROTHENBERG, E. A., and H. W. DOUGLASS: Investigation of Liquid Fluorine and Liquid Ammonia Pro• pellant Combination in a 100 Pound Thrust Rocket Engine, NACA RM E53·E08 (3 July 1953), 31 p., Declassified 16 May 1958. 67. ROESKY, H. W., O. GLEMSER und D. BORMANN: Angew. Chem. 76, 713-4 (1964). 68. ROBISON, W. C.: Jet Propulsion 24,111-2 (1954). 69. RICHARDS, R. J., W. G. STEWARD, and R. B. JACOBS: Adv. Cryog. Engng. 5, 103-10 (1960). 70. RIEDE, P. M., and D. 1. J. WANG: Adv. Cryog. Engng. 5, 209-15 (1960). 71. ROBOTTI, A.: Study on a Micro·Rocket Engine with Gaseous Propellants (H2 + O2) (in Italienisch), Riv. Combust. Italia 16: 1,3-10 (1962). 72. ROLLBUHLER, R. J., and D. M. STRAIGHT: Ignition of Hydrogen-Oxygen Rocket Engine by Addition of Fluorine to the Oxidant, NASA TN D-1309 (July 1962), 21 p. 73. ROWE, W. H., P. M. ORDIN, and J. M. DIEHL: Experimental Investigation of Liquid Diborane-Liquid Oxygen Propellant Combination in 100-Pound Thrust Rocket Engine, NACA RM E9·C11 (May 1949), 25 p. 74. ROTH, W.: J. Chem. Phys. 28, 668-70 (1958). 75. RICE, W. E., and C. A. GREGORY: Ignition Studies of Droplet Vapor Systems, Experiment Inc., Rich• mond, Va., Rept. EXP 101, 133-1, Tech. Publ. 91, Contract DA 36·034·0RD·763 (Oct. 1954),34 p., AD 107288. 76. ROSSMANN, T. G.: Program of Exploratory Research on Rocket Engine Combustion, Bell Aircr. Corp., Buf• falo, Rept. 02·982·026, AFOSR TR 58-17, Contract AF 18(600)1156 (15 Oct. 1957), 75 p., AD 148132. 77. Ross, D. H., and T. J. MCGONIGLE: Canad. Pat. 559936 (19.5.1962/8.7.1958) and US Pat. 2759418, Ref. : CZ 1957, 5456. 78. REDDING, P. E.: Astronautics 3: 4, 30-31, 72 (1958). 79. Riihm & Haas Corp.: Methylamines, a) Chemistry and Uses, SP·172 (Apr. 1960),20 p., b) Physical Pro• perties and Analytical Methods, SP·174 (March 1960), 43 p., c) Storage and Handling, SP-l73, (March 1960), 22 p. 80. RAPP, L. R., and M. P. STRIER: Chemical Aspects of Hypergolic Ignition for Liquid Propellant Rocket EnginEs. ARS·Preprint 331·56. 81. RAPP, L. R., rnd M. P. STRIER: Jet Propulsion 27,401-4 (1957). 82. RASTOGI, R. P., H. L. GIRDHAR, and N. L. MUNJAL: ARS·J. 32, 952 (1962). 83. ROWE, W. H., P. M. ORDlN, and J. M. DIEHL: Investigation of the Diborane-Hydrogen Peroxide Pro• pellant Combination, NACA RM E7-K07 (1948). 84. RING, E.: Hybrid Rocket Motor and Supporting Development, Gen. Electric, Final Rept. May 1951-June 1953, R 53A 0520 (Dec. 1953),36 p., AD 38444. 85. ROSSER, A.: Decomposition Burning of Monopropellant Drops. Hydrazine, Nitromethane and Ethyl Nitrate, CIT-JPL Progr. Rept. 20·305 (Jan. 1957), 12 p., USDC OTS PB Rept. 135689. 86. ROSE, L. C.: US Pat. 3081595 (15. 6. 1960/19.3. 1963), Inh.: Thompson Ramo Wooldridge, Ref.: CA 58, 11163d. 87. ROTH, J. F.: Z. ges. SchieB· u. Sprcngstoffwesen 36,53 (1941). 88. RADELL, J., J. W. CONOLLY and A. J. RAYMOND: J. Am. Chem. Soc. 83, 3958-60 (1961). 89. ROUSH, G., B. M. KENT, and H. A. VOLZ: Research on Toxic Hazards of Pentaborane, Wright Patterson AFB, 6570th Aerospace Med. Res. Labs. and Callery C. C., Final Rept. AMRL-TDR 62-109 (Sept. 1962), 40 p., N 63-10468. 90. Rocketdyne: Research in the Chemical, Physical and Metallurgical Sciences, Rocketdyne, Rept. R 5128 (April 1963), 59 poo RD TDR 63-1045, Ref.: ASTIA TAB 1963-3-5, p. 28. 91. RYSCHKEWITSCH, G. F.: US Pat. 2971031 (7.2.1961), Inh.: Olin Mathieson, Ref.: CA 55, 12855h, US Pat. 3030417 (6.9.1955/17.4.1962), Inh.: Olin Mathieson. 92. ROTHBERG, S., J. L. COLBOURN, and R. SALVATORE: Jet Propulsion 28,762-4 (1958). 93. ROSENDAAL: Arch. Ind. Hyg. Occ. Med. 4, 257-60 (1951). 94. REYNOLDS, W. D., \V. S. SOLOMON, and W. S. ANDERSON: Infrared Analysis of Hydrocarbon Contaminants in Liquid Oxygen, Gaseous Helium and Nitrogen, US Air Force Flight Test Center, Edwards AFB, Calif., Rept. AFFTC TN-58-25 (Nov. 1958),22 p., AD 203781. 95. REYNOLDS, T. W.: Aircraft-Fuel-Tank Design for Liquid Hydrogen, NACA RM E55-F22 (9 Aug. 1955), 28 p., N63-12535. 96. REDMOND: Decomposition of Hydrazine in Liquid Ammonia, Naval Research Laboratory NRL Rept. 4536 (June 1955), 20 p. 97. RYKER, D. W.: US Pat. 2768888 (30.10.1956), Inh.: Olin Mathieson Chemic. Corp., Ref.: CA 51, 1589f (1957). 98. RALEIGH, C. W., and P. F. DERR: Corrosion 16,507 t-511 t (Oct. 1960), Ref.: CZ 132, 4871 (1961). Literaturverzeichnis S 761

99. ROWLEY, R. W.: An Experimental Investigation of Uncooled Thrust Chamber Materials for Use in Storable Liquid Propellant Engines, CIT·JPL Tech. Rept. 32-561 (15 Febr. 1964),30 p., N64-17820. 100. Rocketdyne: Research on Hazard Classification of New Liquid Rocket Propellants, Vol. II, Rocketdyne, Canoga Park, Final Rept. R-3217, Vol. 2 (Oct. 1961), 170 p., AD 272026. 101. RUDGE, A. J.: The Manufacture and Use of Fluorine and its Compounds, Oxford University Press, Lon- don-New York-Toronto 1962, 87 p. 102. REED, R. P., and R. P. MIKESELL: Adv. Cryog. Engng. 10, 46-9 (1965). 103. ROBBINS, R. F., and P. R. LUDTKE: J. of Spacecraft and Rockets 1, 253-9 (1964). 104. RAUSCH, A., S. C. FAN, and L. E. SCOTT: Adv. Cryog. Engng. 10, 422-7 (1965). 105. RANDALL, R., and A. SULLIVAN: Adv. Cryog. Engng. 10, 451-7 (1965). 106. RIEHL, W. A., C. F. KEY, and J. B. GAYLE: Reactivity of Titanium with Oxygen, NASA TR R-180 (1963). 107. ROGERS, J. D.: Adv. Cryog. Engng. 9, 311-5 (1964). 108. ROBBINS, J. H., and A. C. ROGERS: J. of Spacecraft and Rockets 3, 40-5 (1966), auch erschienen als AIAA Paper 64-426. 109. Rocketdyne: Development of High-Energy Solid Propellant Formulations, Vol. 2: Beryllium Propellant Handling Manual, Contr. AF 046118179 RPL TDR 6410 (Jan. 1964), 66 p., AD·433006. 110. RICE, M. J.: Investigations on Some Magnesium Hydrides, Techn. Rept. Off. Nav. Res. Contract ONR· 494(04) (1 Aug. 1956). 111. RICE, M. J.: Non-Solvated Aluminum Hydride, Techn. Rept., Off. of Naval Res. Contract ONR-494(04) (1 Aug. 1956) AD 106967. 112. ROSOLOVSKY, V. J.: Thermal Decomposition of Nitrosyl Perchlorate, Doklady Akad. Nauk SSSR 146: 1, 115-7 (1962), Transl. FTD-AFSC-TT-63-116, Ref.: CZ 1963, 14965. 113. REARDON, F. H.: Combustion Stability Characteristics of Liquid Oxygen/Liquid Hydrogen at High Chamber Pressures, AL-\'A Paper 65-612 (1965), 13 p. 114. RIVARD, J. G.: New Techniques for Throttleable Bipropellant Rocket Engines, AIAA Paper 65-560 (1965) 13 p. 115. RITTER, J. A.: Chilling the M-l Fuel Turbopump to Liquid Hydrogen Temperature, Aerojet.Gen. Corp. Sacramento, AGC Rept. 8800-65, NASA-CR-54828 (3 June 19(6), 80 p., N 66-25585. 116. Rocket Research Corp.: Monopropellant Hydrazine Design Data, Rocket Research Corporation, Seattle, Wash. (1966), 115 p. 117. ROBERTS, R W., et al.: Criteria for Use of Catalytic Reactors in Large L02/LH2 Engine Ignition Systems, AIAA Paper 66-626 (1966). 118. ROWLEY, R. W., and W. H. TYLER: Effect of Injector Design on Thrust Chamber Erosion, JPL TR-30-750 (1 March 19(6), 25 p., NASA CR 75153, N 66-26283. 119. RASTOGI, R. P., H. L. GIRDHAR, and N. L. MUNJAL: Ind. J. Chem. 2, 301-7 (1964). 120. RASTOGI, R. P., K. KISHORE, and N. L. MUNJAL: AIAA-J. 3, 554 (1965). 121. RASTOGI, R. P., and K. KISHORE: AIAA-J. J, 1083-5 (1966). 122. RICCA, P. M.: Arch. Environmental Health 12, 399-407 (1966). 123. RUSSELL, L. M., H. W. SCHMIDT, and R. F. CLARKE: Reaction Characteristics of Spills of Fluorine and Fluorine-Oxygen Mixtures Upon Various Materials, NASA TN D-3118 (March 19(6) 23 p. 124. RUCCIA, F. E., et al.: Adv. Cryog. Engng. 12, 218ff. (1967). 125. ROTHE, K.: Rocket Engine Turbopumps for Space Travel, Deutsche Gesellschaft f. Flugwissenschaften, 5. Lehrgang f. Raumfahrttechnik, Stuttgart 1966, Vortrag 105. 126. Ross, D. i:l., M. E. HILL, and T. MILL: The Very Low-Pressure Pyrolysis of Difluoramine Compounds, AIAA Paper 68-147 (1968). 127. ROLLBUHLER, R. J., and W. A. TOMAZIC: Investigation of Small-Scale Hydrazine-Fluorine Injectors, NASA Memo 1-23-59E (Jan. 1959) 17 p., Declassified 1966, N66-33 332. 128. REYNOLDS, J. M., and M. HURWITZ: Electrohydrodynamic Propellant Management Systems for Cryogenic Upper Stages, AIAA Paper 66-922. s 1. SCHMIDT, E. W.: Fluor als Raketentreibstoff (Literaturzusammenstellung), DGRR Tiibingen (1962). 2. STEUNENBERG, R. K., R. C. VOGEL, and J. FISCHER: J. Am. Chem. Soc. 79, 1320 (1957). 3. SCHEER, M. D.: J. Chem. Phys. 20, 924 (1952). 4. SMITH, D. F.: J. Chem. Phys. 21, 609-14 (1953). 5. SCHAFER, K., und E. WICKE: Zschr. Elcktrochem. 52, 205-9 (1948). 6. SHlSHKOV, Yu. D., and A. A. OPALOVSKII: Russian Chem. Reviews 29: 6, 357-64 (1960). 7. SAWYER, A. E., M. HALL, and D. A. SKINNER: Determination of F and Cl in ClFa, US Atomic Energy Commission, Ind. Group Headq. CI-R-78 (1959), 6 p., Ref.: CA 54, 18169b (1960). 8. STERN, G., and R. P. BELL: Miller's Fluorinated Lubricant-ClFa-Reactions, US Atomic Energy Commission GAT-290 (1960), 23 p., Ref.: CA 54, 21730a (1960). 9. SUAREZ-ALFONSO, E., A. E. CHAMBERS, and D. J. HATZ: Mechanical System Design-Criteria Manual for Chlorine Trifluoride, Rocketdyne Rept. R-3132 (Sept. 1961), 79 p. 762 Literaturverzeichnis S

10. SUAREZ-ALFONSO, E., A. E. CHAMBERS, and D. J. HATZ: Chlorine Trifluoride Handling Manual, Rocket• dyne Rept. R 3136 (Sept. 1961),49 p. 11. SCHMEISSER, M.: Angew. Chern. 72, 324 (1960). 12. SCHlIIEISSER, M., und F. HUBER: DBP 1052369 (16.12.1957/12.3.1959), Ref.: CA 55, 1245i, Brit. Pat. 840026 (6. 7.1960), Ref.: CA 55, 184a (1961). 13. SCHOENFELDER, C. W.: J. Chromatography [Amsterdam] 7, 281 (1962). 14. SARNER, S.: Astronautics 6,7,100 (1961). 15. SIMKIN, J., and R. L. JARRY: J. Phys. Chern. 61, 503-4 (1957). 16. STRENG, A. G., A. D. KIRSHENBAUM, and A. V. GROSSE: Addition and Substitution Products of Oxygen Fluorides, Res. Inst. Temple Univ. Philadelphia, Annual Progr. Rept. 3 (15 Jan. 1963) 64 p. 17. SCHMIDT, E. W.: Raketentechnik u. Raumfahrtf. 4, 98-9 (1960). 18. SKIRROW, G., and H. G. WOLFHARD: Proc. Roy. Soc. [London] A 232,72 (1955). 19. SAX, J.: Handbook of Dangerous Materials, Reinhold Publ. Corp., New York 1958, 2nd Ed. 20. SELLECK, F. T., H. H. REAMER, and B. H. SAGE: Ind. Engng. Chem. 45,814-9 (1953); Supplementary Material: Am. Doc. Inst. Washington, Document 3844. 21. SUAREZ-ALFONSO, E., A. E. CHAMBERS, and D. J. HATZ: Nitrogen Tetroxide Handling Manual, Rocket• dyne Rept. R-3135 (Sept. 1961), 58 p., Contract AF 33(616)6939, AD 226120. 22. SUAREZ-ALFONSO, E., A. E. CHAMBERS, and D. J. HATZ: Mechanical System Design-Criteria Manual for Nitrogen Tetroxide, Rocketdyne Rept. R-3131 (Sept. 1961),83 p., AD 266130. 23. SIEGMUND, J. M.: Research on Materials and Methods for Decontamination of Toxic Missile Propellant Spillage, Allied Chem. Corp., Morristown, Contract AF 33(616)7672, Final Tech. Rept., Wright Patterson AFB (June 1962),179 p., Ref.: NASA TPA N62-14523. 24. SMITH, W. D., and O. C. BENDER: Comparison of Storable and Cryogenic Propellants, AIAA Preprint 63-177 (June 1963) 29 p. 25. STUMPE, A. R.: J. Aviation Med. 29, 650-9 (1958). 26. STREIM, H. G., E. A. BOYCE, and J. R. SMITH: Anal. Chem. 33,85-8 (1961). 27. SPAKOWSKI, A. E.: The Thermal Stability of UDMH, NASA Memo. 12-13-58E (Dec. 1958). 28. STEIN, L.: J. Phys. Chem. 66, 288 (1962). 29. STETTBACHER, A.: Explosivstoffe 4: 2. 27 (1956). 30. SHARPE, A. G.: Quart. Rev. 4, 115-130 (1950). 31. SIMONS, J. H.: Fluorine Chemistry, Academic Press, New York 1950 (2 Bande). 32. SCHULZE, G.: DBP 923547 (17.2.1955) Inh.: BASF, Ref.: CA 52, 673f. 33. STUART, A. P.: US Pat. 2813067 (12. 11. 1957) Inh.: Sun Oil Co. 34. SWENSON and RYKER: US Pat. 2774725 (18. 12 .1956), Inh.: Olin Mathieson C. C. 35. SCHWARZ, E.: tJber die strahlenchemische Bildung von Hydrazin und Anilin, Diss. Univ. Mainz 1962. 36. SOROKIN, Yu. A., and S. YA. PSHEZHETSKIY: The Formation of Hydrazine by the Action of Gamma Radiation on Solid and Liquid Ammonia, AFSC Transl. No. FTD-TT-62-838 from Doklady Akad. Nauk SSSR 138: 4, 880-3 (1961). 37. SNYDER, H. J., et al.: Hydrazine Process Development, Aerojet-General Nucleonics, Sacramento, Contract AF 33(600)42996 Proj. 7840, Interim Tech. Engng. Repts. No.7 AN 847 (Jan. 1963), 193 p., Ref.: ASTIA TAB 63-2-5 p. 32; No.8 (April 1963), 126 p., Ref.: ASTIA TAB 63-3-5, p. 29. . 38. SCOTT, D. W., et al.: J. Am. Chem. Soc. 71, 2293-7 (1949). 39. SZWARC, M.: Proc. Roy. Soc. [London] A 198,267 (1949). 40. SCOTT, F. F., J. BURNS, and B. LEWIS: Explosionsgrenzen von Hydrazin-Luft-Gemischen (in Englisch), US Bur. of Mines, Rept. Invest. 14460 (May 1949). 41. STRUNK: Missiles and Rockets 116-20 (Sept. 1957). 42. SARNER, S.: Astronautics, Data Sheets - Propellants, Astronautics 4: 11 (1959) to 6: 7 (1961). 43. STERN, S. A., and W. B. KAY: J. Am. Chem. Soc. 76, 5353-4 (1954). 44. SAGE, B. H.: Some Properties of Nitric Acid, Nitrogen Dioxide, Nitric Oxide, Water and Their Mixtures, CIT-JPL Progr. Rept. 20-107 (15. Oct. 1957), 145 p. 45. SIB BITT, W. L., et al.: Physical Properties of Concentrated Nitric Acid, NACA TN 2970 (June 1953). 46. SANDS, G. A.: Ind. Engng. Chern. 40, 1937-45 (1944). 47. SCHOENFELDER, C. W.: J. Sci. Instr. 39: 2, 88 (1962). 48. SCHMEISSER, M., und P. SARTORI: Angew. Chern. 71, 523 (1959). 49. STEPHENSON, C. C., and H. O. McMAHo: J. Am. Chem. Soc. 61, 437-40 (1939). 50. SMITH, D. F.: Science 141, 1039 (1963). 51. SANGHVI, M. D., and W. B. KAY: J. Chern. Engng. Data 4,121 (1959). 52. STOCKINGER, H. E.: AMA Arch. Ind. Hyg. Occ. Med. 1954, 366-83, vgl. auch Chern. Engng. News 34, 4704 (1956). 53. SAlIIOILOVICH, V. G., and Yu. V. FILIPPOV: Russ. J. Phys. Chern. [Lond.] 35: 1,94-6 (1961). 54. STAGE, H., und L. GEMMEKER: Glas- und Instr.-Technik 8, 143-9,206-7 (1964). 55. STRENG, A. G.: J. Chern. Engng. Data 6, 431-6 (1961). 56. STRENG, A. G., and A. V. GROSSE: J. Am. Chern. Soc. 81, 805-6 (1959). 57. SANDRI, R.: Comb. and Flame 2, 348-52 (1958). Literaturverzeichnis S 763

58. SANDRI, R.: Comb. and Flame 4, 284-5 (1960). 59. STRENG, A. G., C. S. STOKES, and L. A. STRENG: J. Chem. Phys. 29, 458-9 (1958). 60. STRENG, A. G., and A. V. GROSSE: J. Am. Chem. Soc. 79, 1517 (1957). 61. STRENG, A. G., and A. V. GROSSE: 6th Symp. on Combust .. Reinhold Pub!. Corp .. New York (1957), pp.264-273. 62. SENIOR, D. A.: Comb. and Flame 5,7-10 (1961). 63. STRENG, A. U.: Explosivstoffe 8, 225-35 (1960). 64. STRENG, A. G., and A. V. GROSSE: Comb. and Flame 5,81-6 (1961). 65. STRENG, A. G., and A. V. GROSSE: The Quenching Diameter of Ozone Flames, 17th IUPAC-KongreB Miinchen 1959. 66. SCHUMACHER, H. J.: J. Chem. Phys. 21, 1610-1 (1953). 67. STRENG, A. G., and A. V. GROSSE: J. Am. Chem. Soc. 79, 3296 (1957). 68. STRENG, A. G., and A. V. GROSSE: J. Am. Chem. Soc. 79, 5583 (1957). 69. SMITH, R. V., et a!.: Adv. Cryog. Engng. 9, 88-97 (1964). 70. STRAKHOV, B. V., and V. P. LEBEDEV: ARS-J. 32, 1454-5 (1962), Dbers. aus: Wesstnik Moskowskogo Uniwerssiteta. Chimii 2, No.4, 19-20 (1960). 71. SVIRBELY, J. L.: AMA Arch. Ind. Hyg. Occ. Health 10,298-304 (1954). 72. SVIRBELY, J. L.: AMA Arch. Ind. Hyg. Occ. Health 10, 305-11 (1954). 73. SLAVINSKAYA, N. A.: Russ. J. Phys. Chem. 34, 462-4 (1960). 74. STRENG, A. G., and A. V. GROSSE: J. Inorg. N uc!. Chem. 9, 315 (1959). 75. SIEVERS, R. F., et a!.: Toxic Effects of TNM, a Contaminant in Crude TNT, US Public Health Rept. 62, 1048 (1947). 76. STOKES, C. S., and A. G. STRENG: J. Chem. Phys. 37, 920-1 (1962). 77. STEHLING, K. R., and A. A. KOVITZ: J. ARS 23, 374 (1953), vg!. auch: KOVITz, A. A., and K. R. STEHLING: Compressibility Studies of Rocket Propellants, Bell Aircraft Corp. Rept. 56-982-013 (15 Sept. 1952). 78. SMITH, C. P.: Adv. Cryog. Engng. 4, 436-42 (1960). 79. SCHUFFLEBOTHAM, N.: A Method of Detecting the Fully Cooled State of a LOX-Pipeline, Brit. Rocket Establishment, RPE Tech. Note 193 (Sept. 1960), 8 p. 80. SIMPSON, G. E.: J. ARS 20, 18-23 (1950) und ARS-Preprint 8-39. 81. SCHULTZ, J. W.: Propellant Handling, Transfer and Storage, ARS-Preprint 748-59 (1959). 82. SHANLEY, E. S.: Ind. Engng. Chem. 45, 1520-4 (1953). 83. SHANLEY, E. S.: Ind. Engng. Chem. 39, 1536-43 (1947). 84. SCHUMB, W. C.: Ind. Engng. Chem. 41, 992-1003 (1949). 85. SCHUMB, W. C.: Ind. Engng. Chem. 49,1759-62 (1957). 86. SCHUMB, W. C.: Some Aspects on the Stabilization of Concentrated Solutions of H 20 2, Mass. Inst. Techno!., D3pt. Chem. Engng., Cambridge, Mass., Rept. 30 (Feb. 1957), 14 p. 87. SATTERFIELD, C. N., et a!.: Ind. Engng. Chem., Part I: 43, 2507-15 (1951), Part II: 47,1040-3 (1955). 88. SATTERFIELD, C. N., F. FEAKES, and N. SEKLER: J. Chem. Engng. Data 4,131-3 (1959), auch erschienen als Mass. Inst. Techn., Dept. Chem. Engng., Rept. 53 (June 1958), 9 p. 89. SATTERFIELD, C. N., and T. W. STEIN: Ind. Engng. Chem. 49,1173-80 (1957). 90. SATTERFIELD, C. N., E. KEHAT, and M. A. T. MENDES: Ignition of and Flames Above Hydrogen Peroxide Solutions, Mass. lnst. Techn., D~pt. Ch3m. Engng., Rept. 04 (15 Oct. 1958), 15 p., Rept. 59 (1958) AD 204894. 91. SATTERFIELD, C. N., and R. S. C. YOUNG: Ind. Engng. Chem. Fundamentals 2, 257-64 (1963). 92. SATTERFIELD, C. N., and K. KEHAT : Comb. and Flame 5, 273-82 (1961) vgl. auch: Mass. Inst. Techn., Dept. Chem. Engng., Rept. 56 (Sept. 1960), 26 p. 93. SATTERFIELD, C. N., E. KEHAT, and M. A. T. MENDES: Comb. and Flame 4,99-105 (1960). 94. SLATER, V. W., and W. S. WOOD: J. Brit. Interplanet. Soc. 7, 137-54 (1948). 95. SCHNEIDER, H.: Weltraumfahrt 8, 63-7 (1957). 96. SATTERFIELD, C. N., and F. P. AUDIBERT: Ind. Engng. Chem. Fundamentals 2,200-2 (1963). 97. SIMKIN, D. J., and C. O. HURD: Jet Propulsion 27,419-20 (1957). 98. SZETELA, E. J., et a!.: Heat Transfer Characteristics of 98% Hydrogen Peroxide, Pratt and Whitney Aircr. Corp., Report (5 May 1961). 99. SKOROKHODOV, 1. 1., L. 1. NEKRASOV, and N. 1. KOBOZEV: Russian J. Phys. Chem. [London] 35, No.8, 994-7 (Aug. 1961), Ref.: ARS-J. 32,1500 (1962). 100. SKOROKHODOV, 1. 1., et a!., Part III: Russ. J. Phys. Chem. [Lond.] 35, 443-6 (1961). 101. STAGE, H., und L. GEMMEKER: Chemiker-Zeitung 88,201-9 (1964). 102. SCATCHARD, C. S., G. M. KAVANAGH, and L. B. TICKNOR: J. Am. Chem. Soc. 74, 3715-20 (1952). 103. STIEL, L. J., and G. THODOS: Ind. Engng. Chem. Fundamentals 2: 3, 233-7 (1963), Ref.: Ind. Engng. Chem., Int. Ed. 55: 8, 77 (1963). 104. SZETELA, E. J.: ARS J. 32, 1289-92 (1962). 105. SMITH, A. L., N. C. HALLETT, and H. L. JOIDfSTON: J. Am. Chern. Soc. 76, 1486-8 (1954). 106. SCHMIDT, E. W.: Raketentechnik u. Raumfahrtf. 5, 24-6 (1961). 107. SlVIITH, T. D., E. L. WILSON, and E. J. SCULLY: Raketentechnik u. Raumfahrtf. 6. 142-6 (1962), 764 Literaturverzeichnis S

108. SCHMIDT, A. F., et al.: J. Res. Nat. Bur. Stand. 65C, 81-7 (1961). 109. SANGER·BREDT, 1.: Astronaut. Acta 3, 241-80 (1957). 110. STEWART, P. A. E.: J. BIS 18, 225-40 (1961-62). 111. STREETT, W. B., et al.: J. Chern. Phys. 40, 1390-5 (1964). 112. STEHLING, K. R.: J. BIS 18, 245-7 (1961-62). 113. SMITH, L. R.: Adv. Cryog. Engng. 6, 334-42 (1961). 114. SCHMUELI, K.: Adv. Cryog. Engng. 6, 406-10 (1961). 115. SCHARLE, W. J.: Adv. Cryog. Engng. 3, 149-59 (1960). 116. SMITH, H. J.: Adv. Cryog. Engng. 3, 179-90 (1960). 117. SANDELL, D. J., et al.: Adv. Cryog. Engng.1, 114-21 (1960). 118. SCHUMB, W. C., et al.: Ind, Engng. Chern. 39, 244-8 (1947). 119. SLESSER, C., and S. R. SCHRAM: Preparation, Properties and Technology of Fluorine and Organic Fluoro Compounds, McGraw Hill Book Comp., New York 1951. 120. STAMPER, J. G., and R. F. BARROW: Trans. Farad. Soc. 54,1592-4 (1958). 121. STAPLE, E., J. G. SCHAFFNER, and E. WIGGIN: US AEC MDDC-1610 (1946). 122. SEAVER, R. E.: Analysis of Fluorine Gas by Reaction with Mercury, NASA TN D-1412 (1962), 6 p. 123. SCHMIDT, H. W., and E. A. ROTHENBERG: Some Problems in Using Fluorine in Rocket Systems, Proc. of the Propellant Thermodynamics and Handling Conf., Ohio State Univ., Spec. Rept. 12 (June 1960), p. 183-202. 124. SUITE, J. J., and R. W. MASON: Study of the Corrosion of Metals in Fluorine, Allied Chemical Corp. Publication (7 Feb. 1959). 125. STEIN, L., and R. VOGEL: The Behavior of U, Th and Other Selected Materials in BrFa, CIFa, CIFs and F2 at Elevated Temperatures, Argonne Nat. Laboratory Rep. No. 5441 (May 1955). 126. STEINDLER, M. J.: Corrosion of Materials in the Presence of Fluorine at Elevated Temperatures, Argonne Nat. Laboratory Rep. No. 5662 (Jan. 1957). 127. SCHMIDT, H. W.: Compatibility of Metals with Liquid Fluorine at High Pressures and Flow Velocities, NACA RM E58-D11 (15 July 1958). 128. SLABEY, V. A., and B. A. FLETCHER: Rate of Reaction of Gaseous Fluorine with Water Vapor at 35°C, NACA TN 4374 (Sept. 1958), 16 p. 129. SCHMIDT, H. W.: Design and Operating Criteria for Fluorine Disposal by Reaction with Charcoal, NASA Memo 1-27-59E (Febr. 1959), 18 p. 130. SCHMIDT, H. W.: Reaction of Fluorine with Charcoal as a Means of Fluorine Disposal, NACA RME57-E02 (July 1957), 17 p. 131. SIEGMUND, J. M.: Transportation, Transfer, Storage of Liquid Fluorine, Proc. of the Propellant Thermo• dynamics and Handling Conf. 1959, Ohio State Univ., Spec. Rept. 12 (June 1960), p 151-60. 132. SMILEY, S. H., and C. R. SCHMITT: Ind. Engng. Chern. 46, 244-7 (1954). 133. SCHMITT, C. R.: Reaction of Fluorine with Steam at Elevated Temperatures, Oak Ridge, Tenn.: Union Carbide and Chern. Corp. Rep. No. K 892 (3 April 1952). 134. SIEGMUND, J. M.: Decontamination of Fluorine Spills, Proc. of the Propellant Thermodyn. and Handling Conf., Ohio State Univ., Spec. Rept. No. 12 (June 1960), p. 267-76. 135. STRENG, A. G.: Combustion and Flame 6, 89-92 (1962). 136. STEIN, L., E. RODZITIS, and J. L. SETTLE: Purification of Fluorine by Distillation, US AEC Argonne Nat. Lab., Rept. 6364 (1961), 16 p., Ref.: CA 56, 12687b. 137. SCHMIDT-TINTEMANN, U.: Munchener Med. Wochenschrift 102: 3,1548 (1960). 138. STARIeCO, E. H., J. E. SIeRE, and H. J. SCHUMACHER: Z. phys. Chern. NF 31,385-96 (1962). 139. SIeRE, J. E., and H. J. SCHUMACHER: Kinetik del' thermischen Reaktion zwischen Fluor und Ozon (in Spanisch), Anales asoc. quim. argo 46, 38-54 (1958), Ref.: CA 52, 16844h (1958). 140. SLABEY: Hydrocarbon and Nonhydrocarbon Derivatives of Cyclopropane, NACA Rept. 1112 (1953), 18 p. 141. STEMMER, J.: Raketenantriebe, Schweizer Druck- u. Verlagshaus AG, Zurich (1952). 142. SINGLETON. A. H., et al.: Long and Short Term Compatibility of Metals in Gaseous and Liquid Fluorine, Ind. Engng. Chern., Research Results Service, Preprint 64-142, 39 p., Ind. Engng. Chern. 57: 3, 47 -53 (1965). 143. SCHNITZLEIN, J. G., J. L. SHEARD, et al.: J. Phys. Chern. 56, 233-4 (1952).r 144. SCHUMB, W. C., and R. F. O'MALLEY: Inorg. Chern. 3, 922 (1964). 145. SANGER, E.: Kohlenwasserstoffe mit Metallzusatz. Bemerkung in: Schriften der dt. Akad. d. Luftfahrt• forschung No. 1071/43 (1943), S. 55-64. 146. STOKES, C. S., and A. V. GROSSE: Ind. Engng. Chern. 49, 1311 (1957). 147. STRAIGHT, D. M., and E. A. ROTHENBERG: Ignition of H 2/02 Rocket Engine with Fluorine, NASA TM X-101 (1959). 148. SMITH, D. D., and R. W. LAWRENCE: Study of Mixed Fluorine-Oxygen Oxidizers for Liquid Propellant with Pentaborane, Aerojet-General Corp., US Dept. Com., Office Techn. Serv., AD 264655, 90 p,. (1961), Ref.: CA 58, 12362a (1963). 149. SEEL, F., und O. DETMER: Z. anorg. allg. Chern. 301, 113-36 (1959). Literaturverzeichnis S 765

150. SCHMIDT, E. W.: Raumfahrtforschung 8, 126-7 (1964). 151. SCHMIDT, E. W.: Raketentechnik u. Raumfahrtf. 3, 83 (1959). 152. SCHAPIRO, J. B.: Preliminary Screening of New and Improved Liquid Rocket Propellants: Ethylene Oxide, US Naval Air Rocket Test Station, Inyokern, Calif., Rept. 17 (Febr. 1952). 153. STOY, S. T.: Adv. Cryog. Engng. 5, 216-21 (1960). 154. SCHMIDT, A. F., et a1.: Adv. Cryog. Engng. 5, 487 -97 (1960). 155. SMITH, C. P.: Adv. Cryog. Engng. 5, 545-8 (1960). 156. SMITH, 1. E., and 1. GLASSMAN: Combustion Processes in Liquid Propellant Rocket Motors, J. Forrestal, Res. Center, Princeton Univ., AEL Rept. 334a, Quart. Progr. Rept. No.1 (23 Jan. 1956), 21 p., AD 84357. 157. SIEVERS, G. K., W. A. TOMAZIC, and G. R. KINNEY: Theoretical Performance of Hydrogen-Oxygen Rocket Thrust Chambers, NASA TR-111 (1961). 158. SMOLAK, G. R., R. H. KNOLL, and L. E. WALLNER: Analysis of Thermal Protection Systems for Space Vehicle Cryogenic-Propellant Tanks, NASA TR R-130 (1962), 96 p. 159. SIMMONS, F. S.: ARS-J. 30, 193-4 (1960). 160. STRENG, A. G., and A. D_ KIRSHENBAUM: J. Chem. Engng. Data 4,127-31 (1959). 161. STEIN, S.: A High-Performance 250 Pound Thrust Rocket Engine Utilizing Coaxial-Flow Injection of JP-4 Fuel and Liquid Oxygen, NASA TN D-126 (Oct. 1959), 14 p. 162. SANGER, E.: tJber einen Raketenantrieb fUr Fernbomber, Mitteilungen aus dem Forschg. Inst. f. Phy~ik der Strahlantriebe Stuttgart No. 13, Verlag Flugtechnik Stuttgart (1957), vg1. auch [S 145]. 163. SCHMIDT, E. W.: Raketentechnik u. Raumfahrtf. 2, 20-1 (1958). 164. SCHMIDT, E. W.: Raketentechnik u. Raumfahrtf. 2, 98-9 (1958). 165. SCHELLER, K., and W. E. McKNIGHT: 7 th Symp. on Combust., Butterworths Scientific Publications, Lon• don (1959), p. 369-76. 166. SCIDLLING, M.: The V-2 Rocket Engine, in: History of German Guided Missiles Development, AGARDo- graph No. 20 (1956), p. 281-96. 167. STAHL, G.: Z. f. Flugwiss. 10, 24-30 (1962), Ref.: CA 57,16951 (1962). 168. SAMPLE, P. E., and H. P. SIMONS: Ind. Engng. Chern. 50,1699-702 (1958). 169. SOLOMON, 1. J., et a1.: Inorg. Chern. 3, 457 (1964). 170. SHERLEY, J. E.: Adv. Cryog. Engng. 8, 495-500 (1963). 171. SCHMIDT, A. F.: Adv. Cryog. Engng. 8, 521-8 (1963). 172. SMELSER, P.: Adv. Cryog. Engng. 8, 378-86 (1963). 173. STEWART, R. B., and V. J. JOHNSON: Adv. Cryog. Engng. 5, 557-65 (1960). 174. STREICH, M.: Verfliissigung, Lagerung und Transport von Wasserstoff und Fluor im technischen MaBstab, A. Messer GmbH., Frankfurt/M., Vortragsm'1nuskript zur WGLR/DGRR-Tagung Berlin (1964), 19 S. 175. SCANLON, J. J., and K. FISCH: US Pat. 3116187 (17.3.1961/31. 12. 1963), Inh.: US D3pt_ Army, Ref.: CA 60, 7864c (1964). 176. SCHNEEBELI, P., et H. MOUTET: La Rech. Aeron. No. 87, 33-46 (1962). 177. SCHALLA, C. A.: Adv. Cryog. Engng. 9, 521-8 (1964). 178. STRENG, A. G.: Chern. Rev. 61, 607 -24 (1963). 179. ScmuDT, E. W.: H'Jrstellung von Stickstofffluoriden durch Elektrolyse DLR FB 66-65 (1966) 39 S. 180. SKINNER, G. B., W. H. HEDLEY, and A. D. SNYDER: Mechanism and Chemical Inhibition of the Hydrazine• Nitrogen Tetroxide Reaction, Monsanto Res. Corp. Final Rept. Aug. 1961 - Oct. 1962, Contracts AF 33(616)7757 and AF 33(6.57)7617, Wright Patterson AFB, ASD-TDR-62-1041 (Dec. 1962),35 p., N63-12170. 181. SOMOGYI, D., and C. E. FEILER: Liquid-phase Hcat-releasc Rates of the Systems Hydrazine-Nitric Acid and UDMH-Nitric Acid, NASA TN D-469 (S3pt. 1960), 16 p. 182. SHORT, J. N., and C. R. SCOTT: VS Pat. 2920199 (1960), Ref.: CA 54, 14690i (1960), vg1. US Pat. 2898732. 183. STENGEL, L. A.: US Pat. 2958182 (1. 11. 1960), Inh.: Commercial Solvents Co., Ref.: CA 55, 5958c. 184. STENGEL, L. A.: US Pat. 2978864 (11. 4.1961) Inh.: Commercial Solvents Co., Ref.: CA 55,1924.';. 185. SCHALLA, R. L., and E. A. FLETCHI

192. SCHWARTZBERG, F. R, T. F. KIEFER, and R. D. KEYS: Adv. Cryog. Engng. 10, 1-13 (1965). 193. SCHIELER, L.: Low Thrust Devices Velocity Control Experiment Program: Catalytic Decomposition of Hydrazine, Aerospace Corp., El Segundo, Calif., Semiannual Tech. Rept. (30 June 1961), 6 p., AD 264852. 194. STENGEL, L. A., and E. E. Toops: US Pat. 3016489 (19. 5. 1958/30. 10. 1962), Inh.: Commercial Solvents Co., Ref.: CA 58, 407 a (1963). 195. SJOBLON, J. J., and P. J. PIZZOLATO: Problems with Monopropellants, ARS Preprint 1244-60 (1960). 196. STEINBERGER, R, C. A. ORLIK, and V. P. SCHAAF: J. Am. Chern. Soc. 77,4748-50 (1955). 197. STEINBERGER, R: Ind. Engng. Chern. 48, 766-8 (1956). 198. STEINBERGER, R, and V. P. SCHAAF: J. Phys. Chern. 62, 280-5 (1958). 199. STEINBERGER, R: 5th Symp. on Combust., Reinhold Publ. Corp., New York (1955), p. 205-11. 200. SHAPIRO, J., and H. G. WEISS: J. Am. Chern. Soc. 76, 1205 (1954) undJ. Am. Chern. Soc. 76,6020-1 (1954), Ref.: CZ 19M, 8992, 1956, 1528. 201. SAMUELSON, L. E.: Pentaborane Thermal Stability at Temperatures of 100°, 125° and 150°C for 7% Ullage, Callery C. C., Rept. on Contract No.a (s)58-454-d (21 Dec. 1961) AD 269203. 202. SCHECHTER, W. H.: Miss. and Rockets 3: 4, 85-6 (1958). 203. SMITH, S. H., and R R MILLER: J. Am. Chern. Soc. 72, 1452-8 (1950). 204. STONE, F. G. A.: Quart. (Chern.) Rev. [London] 9, 174-201 (1955). 205. SCHLESINGER, H. J., et al.: J. Am. Chern. Soc. 75, 186-224 (1953). 206. SUAREZ-ALFONSO, E., A. E. CHAMBERS, and D. J. HATZ: Mechanical System Design-Criteria for Penta• borane, Rocketdyne Rept. R-3133, Contract AF 33(616)6939 (Sept. 1961), 80 p., AD 266118. 207. SUAREZ-ALFONSO, E., A. E. CHAMBERS, and D. J. HATZ: Pentaborane Handling Manual, Rocketdyne Rept. R-3137 (Sept. 1961),49 p., AD 266131. 208. SCHALLA, R L.: Spontaneous Ignition Limits of Pentaborane, NACA RM E55-B03 (1957). 209. SMITH, S. H., and R. R. MILLER: Thermal Decomposition of Gaseous Borane Mixtures at 21°C, Naval Res. Lab., Washington, Final Rept. NRL 5018 (23 Jan. 1958), 30 p., AD 152986. 210. SMITH, W. L., and I. M. MILLS: J. Chern. Phys. 41,1479-85 (1964). 211. SCHOETTLIN, C. E., et al.: Toxicological Research on Central Nervous System Effects of Borane Fuels, North Am. Av., Final Rept. ASD TR 61-438, AD 268610. 212. SCHLESINGER, H. I., et al.: J. Am. Chern. Soc. 62, 3421-5 (1940). 213. SIMONS, H. P., and E. L. POLING: Die explosive Reaktion von Diboran in trockener und feuchtigkeits• gesattigter Luft (in Englisch), Callery C. C. Rept. CCC-l024-TR-141 (Oct. 1955). 214. SKINNER, G. B., and A. D. SNYDER: Mechanism and Chemical Inhibition of the Diborane-Oxygen Reac- tion, AIAA-Preprint 63-502 (1963). 215. SPENGLER, G., und A. LEPIE: I: Z. f. Flugwiss.ll, 197-203 (1963), II: Z. f. Flugwiss.ll. 241-7 (1963)_ 216. SCOTT, R W.: Chern. Engng. 71: 5, 79-82 (1964). 217. SUTTON, N. V.: Anal. Chern. 36, 2120-1 (1964). 218. SUTTON. N. V.: Microchem. J. 8, 23-7 (1964), Ref.: CA 61, 4139f. (1964). 219. STARK, T. M., and J. JOFFE: J. Chern. Engng. Data 9,327-30 (1964). 220. SCURLOCK, A. C.: US Pat. 3132978 (22.6. 1962/12.5. 1964), Ref.: CA 61, 4142c (1964), Zusatzpatent zu US Pat. 3095334, CA 59, 7311d (1963). 221. SCHMEISSER, M., und P. SARTORI: Chcmie-Ingenieur-Technik 36,9-14 (1964). 222. SCHMEISSER. M., and K. BRANDLE: Adv. Inorg. Chern. Radiochem. 5, 42-89 (1963). 223. STRENG, L. V., and A. G. STRENG: J. Chern. Phys. 38, 1788 (1963). 224. STRENG, A. G., and A. V. GROSSE: Storing Gaseous Ozone under Pressure, Ind. Engng. Chern., Int. Edtn. 53: 5, 61A-64A (1961). 225. SCHUMB, W. C., and C. N. SATTERFIELD: Stability and Reaction Studies of Hydrogen Peroxide, Mass. Inst. Technol., Cambridge, Quart. Period. Status Report (30 June 1958), 16 p .. AD 200576. 226. SILVERSTEIN, A., and E. W. HALL: Liquid Hydrogen As a Jet Fuel for High-Altitude Aircraft, NACA RM E55-C28a (15 Apr. 1955),57 p., N63-12541. 227. SOTAK, R E.: Development Tests for the Liquid Hydrogen Servicing Systems, Complex 37 B, Saturn C 1, Cape Canaveral, Fla., Air Products and Chern. Inc .• Allentown, Pa., Rept. on NASA Contr. NAS 8-1546, APCI Proj. 00-1-31 400, NASA CR-51733 (28 Febr. 1962), 105 p., N63-22161. 228. SCHIGATSCH, A. F., E. B. KASAKOWA iRA. KIGELJ: Metod Analisa Pentaborana, Sch. anal. Chimii 14, 746-7 (1959). 229. SCHLESINGER, H. I.: Hydrides and Borohydrides of Light Weight Elements and Related Compounds, Chicago Univ., Ill., Annual Tech. Rept. (1. 8.1955 - 31. 7. 1956), 46 p., AD 108168. 230. SEKLEMAN, H. V., and R. W. LAWRENCE: Reaction of Pentaborane and Hydrazine and the Structure of the Adduct, AIAA Preprint 63-503 (1963). 231. SKOLNIK, S., and H. W. KRUSE: US Pat. 2712496 (5. 7. 1955), Inh.: US Government, Ref.: CA 49, 14298i (1955). 232. SCHULZE, W. A.: US Pat. 2934417 (26.4. 1960), Inh.: Phillips Petrol. Co., Ref.: CA 04, 15936c (1960). 233. STEINDLER, M. J., and H. J. SCHLESINGER: Hydrazine Reaction with Diborane, J. Am. Chern. Soc. 75, 756 (1953). Literaturverzeichnis S 767

234. SCHAPIRO, J. B.: Preliminary Screening of New and Improved Liquid Rocket Propellants, Naval Air Rocket Test Station, Lake Denmark, NARTS Rep. 27 (Nov. 1952), 24 p., AD 10122. 235. SAGGIOMO, A. J.: J. Org. Chern. 22,1171-75 (1957). 236. SAGGIOMO, A. J.: Hexacarbon Dinitride or Dieyanodiacetylene, Res. Inst. Temple Univ., Philadelphia, Pa., Tech. Note No.3 (19 Dec. 1956), AD 115068. 237. SCHMITZ, E.: Angew. Chern. 76, 197-206 (1964), Nachr. Chern. u. Technik 12: 5, 92 (1964). 238. STEELE, A. J.: RIFT Radiation Effects Program, Irradiation No.9: Monomethyl Hydrazine, Lockheed Missiles and Space Co., Sunnyvale, Calif.. NSP 64-10 (15 Febr. 1964), 37 p., N64-18470. 239. STENGEL, L. A.: US Pat. 2951335 (19. 5. 1958/6.9. 1960), Inh.: Commercial Solvents Corp., Ref.: CZ 1962, 1856. 240. STOKES, C. S.: Ind. Engng. Chern. 51, 1494 (1959). 241. SHANLEY, E. S., and J. R. PERRIN: Jet Propulsion 28,382-5 (1958). 242. STOKES, C. S., et al.: Ind. Engng. Chern. 52, 75-8 (1960). 243. STEPHENSON, M. E.: Property Values of Parahydrogen, Argonne National Lab. Rept. ANL 7004, AEC Res. and Dev. Rept. (March 1965), 164 p. 244. SWALLEY, F. E., and C. D. NEVINS: Adv. Cryog. Engng. 10, 208-15 (1965). 245. SEGEL, M., et P. BERARD: Etude des Transferts de Chaleur Durant la Vidange des Reservoirs d'un Etage Cryogenique, Institut International du Froid, Grenoble, France (Juin 1965), Preprint. 246. SEGEL, M. P.: Internat. Adv. Cryog. Engng. 10 MU, 308-13 (1965). 247. SANGER, E., und 1. BREDT: Dber einen Raketenantrieb fUr Fernbomber, Deutsche Forsch.-Anstalt f. Segelfiug, Ainring, Deutsche Luftfahrtforschung Mitt. 3538 (August 1944), S. 97 -105. 248. STAI, D. F., F. BIZJAK, and S. E. STEPHANOU: J. of Spacecr. and Rockets 2: 5, 742-5 (1965). 249. SALTZMAN, B. E.: Analytical Chemistry 26: 12, p. 1949-55 (1954). 250. SCHUMACHER, J. C.: Perchlorates, Th?ir Prop2rties, Manufacture and Uses, Am. Chern. Soc. Monograph S~ries, Vol. 146, Reinhold PubI. Corp. New York (1960), 257 p. 251. SCHLESINGER, H. 1., and A. B. BURG: J. Am. Chern. Soc. 59, 780 (1937). 252. SCHLESINGER, H. L H. C. BROWN. and E. K. HYDE: J. Am Soc. 75,209-13 (1953). 253. SARTEN, P.: UnvDriiff9ntlichte Versuchsberichte, Forschungsinstitut fUr Physik der Strahlantriebe, Stuttgart 1962. 254. SHELBERG, W. E.: The Radiolytic Decomposition of 1,1-Dimcthylhydrazine, Diethylenetriamine and Hydyne Rocket Fuels, US Nav. Rad. Dei. L'1b. San Francisco (August 1965), 14 p., USNRDL-TR- 896, AD 622334, Ref.: CA 6-1, 14016 (1966). 255. SUTTON, N. V., ani H. SCH'IEIDER: ~icrocI13m. J. 9, 209-17 (1965) CA 63, 8112d (1965). 256. SUSSiHAN, M., M. LUPERI, an:l A. MERRILL: Exp~rim3ntal Performance of OF2/B2Hs Under Sea Level and Simulated Space Conditions, AIAA Pap~r 65-621 (1965), 24 p. 257. SHIEBER, H., and R. C. RUPERT: Assuran~C) of Service Life of the Mira 150A Variable Thrust Rocket Engine, AIAA Paper 65-608 (1965), 21 p. 258. SPENGLER, G., und J. BAUER: Brennstoff-Chemie 46,117 (1965). 259. SOBOLEV, N. N., et al.: Flame Temp. of a Liquid Fuel Jet Engine, Soviet Phys.-Techn. Phys. 4: 1,24-31 (1959). 260. SMOOT, L. D., and C. F. PRICE: AIAA J. 3. 1408-13 (1965). 261. SHIEBER, H., and R. C. RUPERT: J. of Spacecraft and Roc-L,ts 3, 1034-8 (1966). 262. SEMEL, G.: Chemie-Ingenieur-Technik 38,888-9 (1966). 263. STOKES, C. S., W. J. MURPHY, and T. R. FLINT: Ind. Engng. Chern., Prod. Res. and Dev. 4, 176-80 (1965). 264. SEADER, J. D., and \V. R. WAGNER: Regenerative Cooling of Rocket Engines, in: Chemical Engineering Techniques in Aerospace, Chern. Engng. Progr., Symposium Series No. 52, Vol. 60 (1964), p. 130-50. 26;3. SILER, R. K.: Meteorological Considerations in the Handling of a Mixture of Liquid Fluorine and Liquid Oxygen, Weather Bureau, Wash., D. C., NASA CR-62579 (15 Oct. 1964),49 p., N 33760. 266. SHELBERG. \V. E.: Radiolytic Decomposition of Hydrazine, RP-1 and Hydyne Rocket Fuels, Naval Radiol. Defense Lab., San Francisco, Rept. AEC 25118, AD 632461, Ref.: CA 65,19917 (1966). 267. SHELBERG, W. E.: Radiolysis of Monomcthylhydrazine, Xature 210,524-6 (1966). 268. SHELBERG, W. E.: Radiolytic Decomposition of Monomethylhydrazine Rocket Fuel, Naval Radiol. Defense Lab., San. Francisco, AEC No. 30237, Rept. USNRDL-TR-843 (1965), 18 p., Ref.: CA 64, 14015-6 (1966). 269. SCHMITZ, B. W., T. A. GROUDLE, and J. H. KELLEY: Development of the Post-Injection Propulsion System for the MARINER-C Spacecraft, JPL TR 32-830, NASA CR 75553 (Apr. 19(6), 53 p., N 66- 27746. 270. SCHlI1ITZ, B. W., D. A. WILLIAMS, W. W. SMITH, and D. MAYBEE: Design and Scaling Criteria for Mono• propellant Hydrazine Rocket Engines and Gas Generators Employing Shell 405 Catalyst, AIAA Paper 66-594 (1966), 67 p. 271. SANDRI, R., and R. BILLINGHAM: AIAA-J. 5, 770-3 (1967). 272. SAWYER, R. F.: The Homogeneous Gas Phase Kinetics of Reactions in the Hydrazine-Nitrogen Tetroxide Propellant System, Princeton Univ., Guggenheim Labs. TR-761, AFOSR 66-0855, AD 634277, N 66-34154. 768 Literaturverzeichnis T

273. SEAMANS, T. F., M. VANPEE, and V. D. AGOSTA: AIAA Paper 66-950. 274. SMOOT, L. D., and C. F. PRICE: AIAA-J. 4, 910-5 (1966), AIAA-J. 5, 102-6 (1967). 275. STRICKER, W.: Z. f. Naturforschung 22a, 1137 (1967). 276. SOLOMON, 1. J.: Research on Chemistry of OaF2 and 02F2' Illinois Inst. of Technology, Res. Inst. Chicago, II!., Summary Rept. 1965, AF 49(638)·1175, AFOSR-66-0953, AD 634440, N66·34614. 277. SCHMIDT, H. W., and J. T. HARPER: Handling and Use of Fluorine and Fluorine.Oxygen Mixtures in Rocket Systems, NASA SP-3037 (1967) 279 p., N67·26000. 278. SIMA, J. J.: TOFLOX Synthesizer Study, Air Reduction Co., Final Rept. RE·66-085-CRE·36, NASA CR-76071 (13 May 1966), N66-29969. 279. STRENG, A. G., and L. V. STRENG: Inorg. Nuc!. Chern. Letters 2,107-10 (1966). 280. SARNER, S. F.: Propellant Chemistry, Reinhold Pub!. Corp., New York (1966) 417 p. 281. SAWYER, R. F., E. T. McMULLEN, and P. PURGALIS: The Reaction of Hydrazine and Chlorine Penta• fluoride in a Laboratory Rocket Combustor, AIAA Paper 68-92 (1968). 282. SAWYER, R. F.: Mass Spectroscopic Observation of Ignition Phenomena in a Small Rocket Combustion Chamber, Combustion Institute, Western States Section, 1967 Fall Meeting, Seattle, Wash., Paper WSCI 67-39. 283. SMYTH, H. F.: Military and Space Short-Term Inhalation Standards, Arch. Environmental Health 12, 488-90 (1966). 284. SEIDEL, A.: Raumfahrtforschung 11, 177-82 (1967). 285. STAKE, A. M.: Resistance of Polymeric Materials to Nitrogen Tetroxide, Illinois Inst. of Technology, IIT Res. Inst., Chicago, Ill., IIT-RI-U6046·7, NAS 7-100, NASA CR-84 844 (15 March 1967) 30 p., N67-28828. 286. SPENCER, R. T.: Development of a Facility for Remote Vibration Testing with Hazardous Cryogens, AIAA Paper 67-278. 287. SETZE, P. C., and H. C. BARNETT: A Review of NACA Research Through 1957 on Boron Compounds as Fuels for Jet Aircraft, NASA Memo iO-7-58E (Dec. 1958) Declassified N67-31872. 288. SIVO, J. N., and J. P. WANHAINEN: Altitude Performance of a Full Scale High-Temperature Turbojet Engine Using Pentaborane Fuel and HEF-2, NASA Memo 12-31-58E (Jan. 1959), Declassified N67-31544. 289. SAWYER, R. F.: J. of Spacecraft and Rockets 5, 116 (1968). 290. SUMMERS, W. H., and E. T. McMULLEN: Combustion of the N2H4iN204 Propellant System, AIAA Paper 66-662.

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1. TANNENBAUM, S.: The Development of Packaged Liquid Propellants, ARS-Preprint 1269-60 (July 1960) 18 p. 2. TSCHUIKOW-Roux, E.: J. Phys. Chern. 66, 1636-9 (1962). 3. TAYLOR, G. D.: Effect of Hydrazine on Blood Glucose and Muscle and Liver Glycogen, School of Aerospace Medicine, Brooks AFB, SAM-TR-66-13 (March 1966) 16 p., AD 633 164, N66-30702. 4. TENENBAUM, D. M.: Testing With Storables, ARS-Preprint 1263-60 (1960),20 p. 5. THEILACKER, W., und E. WEGNER: Angew. Chemie 72, 127 (1960). 6. TOMAZIC, W. A., and G. R. KINNEY: Experimental Performance of the Mixed-Oxides-of-Nitrogen and Ammonia Propellant Combination with Several Injection Methods in a iOOO-pound Thrust Rocket Engine, NACA RM E55-A07 (March 1955), 30 p. 7. TAIT, C. W., et al.: J. Am. Chern. Soc. 78, 2670-3 (1956). 8. THORPE and ROGER: Phil. Trans. 185, 397 (1895). 9. TROYAN, J. E.: Ind. Engng. Chern. 45, 2608-12 (1953). 10. TANS, A. M. P.: Chern. Engng. 69: 14, 162 (1962). 11. THORP, C. E., L. C. KINNEY, and R. F. REMALY: US Pat. 2700648 (25 Jan. 1955), Inh.: Air Reduction Co., Inc., Ref.: Angew. Chern. 68, 469 (1956) und CA 49, 4912a (1955). 12. THORP, C. E.: Bibliography of Ozone Technology, Vol. I: Analytical Procedures and Patent Index (1954), Vol. II: Physical and Pharmacological Properties (1955), Armour Research Foundation, Ill., Inst. Techn. Center, Chicago, Ill. 13. THOMAS, W. H.: Missiles and Rockets 1957: 9, 131-2 (1957). 14. TSCHINKEL, J. G.: Jet Propulsion 26,569-71 (1956). 15. TSCIDNKEL, J. G., and A. E. GRAVES: Jet Propulsion 27,796-8 (1957). 16. TSCIDNKEL, J. G., and T. D. CANTRELL: Jet Propulsion 27, 290-2 (1957). 17. TSENTSIPER, A. B., et al.: Russian J. inorg. Chern. 4: 9, 886-9 (1959). 18. TURKHEIMER, P.: Adv. Cryog. Engng. 4, 403-9 (1960). 19. TKACHENKO, E. A.: ARS-J. 30, 566-8 (1960). 20. TOWER, L. K., R. BREITWIESER, and B. E. GAMMON: Theoretical Combustion Performance of Several High• Energy Fuels for Ramjet Engines, NACA Tech. Rept. 1362 (1958), 18 p. 21. TURNBULL, S. G., et al.: Ind. Engng. Chern. 39, 286-8 (1947). Literaturverzeiehnis T 769

22. TRENT, C. H., and M. J. ZUCROW: J. ARS 21, 129-31 (1951). 23. TSCHINKEL, J. G.: Physico-Chemical Properties of Kerosene, Army Ballistic Missile Agency ABMA, Com• bustion and Fuels Section Memo. No. 46 (28 FC'br. 1956), 15 p. 24. TURNER, J. J., and G. C. PIMENTEL: Science 140, 974 (1963). 25. THOMPSON, R. J.: High Temperature Tlwrmodynamics and Theoretical Performance Evaluation of Rocket Propellants, in: S. S. PENNER and J. DUCAR~lE: The Chemistry of Propellants, Pergamon Press, Oxford-London-New York 1960, p. 2.3-120. 26. To MAZIC, IV. A., and E. A. ROTHENBlmo: ExperinH'ntal Roeht Pl'rformance with 15% Fluorine and 85% Oxygen and JP-4, NACA HM E55-D29 (1955). 27. TRAYEHS, M. W., and C. G. SILCOCKS: Nature 139,1018 (1937), Rd.: CA 31,5659 (1937). 28. TANTAilI, D. H., and A. ALLEN: ,\dy. Cryog. En;wg. 5, 299-30G (1960). 29. THOMPSON, ,Yo R., and E. L. GEEHY: Ady. Cryoi'. Engng. 7. :JIH -400 (1962). 30. THmIAs,]'\., A. G. GAYDON, and L. IhmwEH: J. Chem. Ph."';. 20, 369-74 (March 1952). 31. THOMAS, D. D.: Optimllm FueJ Study fur KIKE-AJAX, Douglas Airel'. Co., Rept. No. S1\127 4:35 (V; Aug. 19(7), :{9 p., AD 151347. 32. TATmr, J. '1'., et al.: Adv. Cryog. Engllg. 9, 265-72 (1964). 33. TO~ILINSON, E. M.: ;\hterials Selection for Propellant Systems, Airel'. and Missiles 4,24 (FebI'. 19(;1). 34. TnOi\IPSON, R. J.: Research on Nitric Acid Supported Combustion, Rocketdyne Final Progr. Rept. R-1157, 'YADC TR 59-1 (l\fareh 1959) AD 208301. 35. TAYLOH, F. R., et al.: Reaction of Nitric Acid and/or Its Decomposition Produc:ts and GaSf'OWl H.\'llro• cnrbolls, Franklin Illst., Lab". for Rps. all(l Dl'V., Fillal Techn. Rept. F-24i52 (Period 11. 6. 1954- 31. 12. 1956), 54 p., 'VADC TR 57-1:38, AD 11810;~. 36. THOMAS, D. D.: A Stud." of the l)>:(' of Starting FlI('ls for Ignition of RFXA-JP-3-Rol'ket Motor, CIT-JPL Pmgr. Rept. 1-77 (Sept. 19D1). I) p. 37. THOMPSON. n. J.: The Xitric A"id-,lmlllollia Pmpl'llant Cuml,ination for Roc-kels, AIlS Proprint 82-5~ (1I)i)2). 38. THENT, C. H., and .l\I. J. ZUCIW\\': Ind. EIl)Ing. Ch~'m. -f-f. 2(lG8-73 (1952). 39. TAIT, C. W., A. O. WHITTAKER, l'l1d H. ,rlLLLUiS: ,\J::S-J. 21, 8:1-8 (1951). 40. TAYLOR, F. lL ll. G. FlU;';KLIN. and O. X. H l' DYJ: l\Il'chanism amI Kim)tics of thl'Reaction between Fuming Nitric Acid and(II' it-; D~"'''lllJlr,,'ilion Products nIHl C;ao;l'ous Hydrocarbons, Franklin III,-;(., Philadl'lphin, La\;,.;, fur J~('s. nnd IkY., H"pL COlli]'. AI<' :1:1(616)3840. WADC TH 58-228 (Jlnn·h 19(8) :~() p., AD lii5;),')il (:«'l' ai-:o AD 14:HJ1.3). 41. TscHIxKEL, J. G.: U:S Pelt. :!I.:17Hil Ui. 5.1!);):~), Inh.: LTc"; 8('l'1'. of til(' _\nny, Rd.: CA 4., ,iG2(' (1%3). 42. Tuom'soN: Ignition D:.'Ll} 'l\A. of S'!f-Tgllilillg Gas-Gl'!lL'i'

Datlieu-Damm·Schmitlt, Raketeutrcibstoffe 49 770 Literaturverzeichnis U

60. TSIEN, H. S.: ARS J. 23, 17-24 (1953). 61. THURSTON, R. S.: Pressure Oscillations Induced by Forced Convection Heat Transfer to Two Phase and Supercritical Hydrogen; Preliminary Experiments, Los Alamos Sci. Lab., New Mex., Contract W·7405·ENG·36·LAMS-3070, Rept. (22 May 1964),93 p., N64·21055. 62. TYSON, G. N.: US Pat. 3140582 (14.4. 1959/14.7. 1964), Inh.: Olin Mathieson C. C., Ref.: CA 61, 10527 g (1964). 63. TRAVERSE, G.: US Pat. 2775863, Ref.: CA 51, 6160 (1957). 64. Toops, E. E.: US Pat. 2944385 (19.5.1958/12.7.1960), Inh.: Commercial Solvents Corp., Ref.: CZ 1962, 2603. 65. TSUCHIYA, S.: Bull. Chern. Soc. Jap. 34, 854-9 (1961), Ref.: CZ 1963, 16778. 66. TITTLE, B., and G. H. CADY: Inorg. Chern. 4: 2,259-60 (1965). 67. TOTR, J. M.: Adv. Cryog. Engng.10, 126-53 (1965). 68. TOTR, J. M., and J. R. BARBER: Adv. Cryog. Engng.10, 134-44 (1965). 69. TOTH, L. W., and A. H. KARIOTIS: Adv. Cryog. Engng. 10, 126-33 (1965). 70. TOTH, J. M.: Adv. Cryog. Engng. 9, 537-44 (1964). 71. THURSTON: Adv. Cryog. Engng.10, 305-12 (1965). 72. THURSTON, R. S.: The Generation of Oscillations Having Acoustic Properties in Forced Convective Heat Transfer to Cryogens, Institut Internat. du Froid, Cours sur l'Hydrogene, Grenoble (Juin 1965), Preprint. 73. TRUCKS, H. F., and W. O. RANDOLPH: Adv. Cryog. Engng. 10, 341-52 (1965). 74. THOMAS, M. D., et al.: Anal. Chern. 28, 1810-6 (1956). 75. TOULMIN, H. A.: US Pat. 3032451 (29.9. 1954/1. 5. 1962), Commonwealth Engng. Co., Dayton. 76. THAYER, J. R.: Effect on Launch Probability Due to 30% FLOX in ATLAS, AIAA Paper 65-535 (July 1965), 8p. 77. TSUCHIYA, S.: Bull. chern. Soc. Japan 34,854-9 (1961) und CZ 1963, 16778. 78. THOMPSON, J. F., and M. E. NEIN: Prediction of Propellant Tank Pressurization Requirements by Dimen• sional Analysis; NASA TN D·3451 (June 1966), 21 p., N 66-29070. 79. THIEME, J.O., and R. L. EVERY: Ignition and Combustion Characteristics of Liquid·Oxygen and Liquid• Methane Mixtures, Chern. Engng. Progr., Sympos. Series 62,113-7 (1966), Ref.: CA64, 17346-7 (1966). 80. TOMAZIC, W. A., E. R. BARTOO, and J. R. ROLLBUHLER: Experiments with Hydrogen and Oxygen in Rege• nerative Engines at Chamber Pressures from 100 to 300 psia, NASA TM X-253 (Apr. 1960), De• classified, N 66-33344. 81. TYLER, W. H., and R. N. PORTER: An Experimental Evaluation of 100 Ib Thrust Ablatively Cooled Rocket Engines, JPL TR·32-978, NASA CR-78440, CR 78548 (Oct. 1966), N 66-37805, N 66-38503. 82. TABATA, W. K., R. J. ANTL, and D. W. VINCENT: Storable Propellant Combustion Instability Program at Lewis Research Center, AIAA Paper 66-602. 83. TOTH, L. R., H. B. STANFORD, and W. F. MAC GLASHAN: Advanced Liquid Propulsion Systems, JPL Space Programs Summ. 37-40, Vol. IV, p. 47-9 (31 Aug. 1966) N67-15796, N67-15712. 84. TOLBERG, W. E., et al.: Inorg. Nuc!. Chern. Letters 2, 79 (1966). 85. TINER, N. A.: Adv. Cryog. Engng. 12, 771-9 (1967). 86. THURSTON, R. S., and J. D_ ROGERS: Adv. Cryog. Engng. 12, 438-51 (1967). 87. THOMPSON, W_ R., and C. S. BONCORE: Adv. Cryog. Engng. 12, 207-17 (1967). 88. TOWNSEND, C. R., G. A. GIARUSSO, and H.-P. SILVERMAN: Thin Film Personal Dosimeters for Detecting Toxic Propellants, Magna Corp., Anaheim, Calif., TRW-6302-6001-R, AMRL-TR-66-231, AF 33- (615)1751 (Feb. 1967) 71 p., AD 652849, N67-32874. 89. TYLER, W. E., and J. R. LOVETT: Organic Nitrates Containing Difluoroamino Groups for Use as High Energy Oxidizers in Rocket Propellants, US Pat. 3346619 (22.8. 1962/10. 10. 1967), Inh.: Esso Res. Engng. Co., Ref.: CA 67, 10416 (1967). 90. TOMAZIK, W. A., F. J. KUTINA, and E. A. ROTHENBERG: Experimental Performance of a 5000 Pound Thrust Rocket Chamber Using a 20% F 2/80% O2 Mixture With RP-l, NACA RM E57-B08 (24 Apr. 1957) 30 p., Declassified N66-39529.

u

1. United States, Office of the Director of Defense Research and Engineering, Washington: The Handling and Storage of Propellants (March 1961), 248 p. Revised Edition 1963. 2. ULLMANNS: Enzyklopadie der techno Chemie, Herausgeber: W. FOERST, 3. Aufi., Verlag Urban & Schwarzen- berg, Miinchen-Berlin (1951-1965). 3. US-Navy Medical News Letter, AMA Arch. Ind. Health 13, 104 (1956). 4. Union Carbide-Linde Company: Liquid Hydrogen Capabilities, Prod. Sheet. 5. URBANSKI, T., et a!.: Thermal Analysis of Tetranitromethane Mixtures with Benzene and Aromatic Nitro Compounds, Bull. Acad. Sci. Polon., Ser. Sci. Chim. 10, 263-6 (1962), Ref.: CA57, 16951 (1962). 6. Soc. d'Electrochimie UGINE, Firmenschrift (1967). Literaturverzeichnis V 771

v

1. VINCENT, L. A., E. A. FOWLER, and M. M. BRAIDECH: Nitroparaffins and Their Hazards, National Bureau of Fire Underwriters, Res. Rept. 12, 1959. 2. VELEY: J. Chern. Soc. [London] 1903,1015-21 (1903). 3. VIALATTE, M. M., and C. E. APERT: Korrosion von rostfreiem Stahl in Gegenwart von wei13rauchender Salpetersaure (in Englisch), Mat. Res. Standards 2, 111 (1962), Ref.: CZ 1963, 9111. 4. VIGDORTSCHIK. N. A., et al.: The Symptomatology of Chronic Poisoning with Oxides of Nitrogen, J. Industr. Hyg. 19,469-73 (Nov. 1937). 5. VAN DER AREND, P. C., and W. J. SCHARLE: J. BIS 18,181-8 (1961-62). 6. VON ELBE, G., and H. T. SCOTT: Hazards of Liquid Hydrogen in Research and Development Facilities, Atlantic Res. Corp., Alexandria, Va., Wright Patterson AFB, ASD TDR 62·1027, Contract AF 33 (657)8952, Proj. 8119 (Dec. 1962), 75 p., N 63·11878. 7. VAN GUNDY, D. A., and R. B. JACOBS: Adv. Cryog. Engng. 2,156-62 (1960). 8. VOGT, P. R.: Application of Cryogenic Propellants to Space Flight, ARS Pre print 2265·61 (1961). 9. VON DER HEYDE, N. J., and R. P. RICKEY: Decontamination of Large Liquid Fluorine Spills, Proc. of the Propellant Thermodyn. and Handling Conf., Ohio State Univ., Spec. Rept. 12 (June 1960), p. 277 -91. 10. VAN DER AREND, P. C.: Adv. Cryog. Engng. 5, 49-54 (1960). 11. VON GUNDY, D. A., L. O. MULLEN, and R. B. JACOBS: Adv. Cryog. Engng. 0,162-70 (1960). 12. VON GLAHN, U. H., and J. P. LEWIS: Adv. Cryog. Engng. 5, 262-9 (1960). 13. VAN TIGGELEN, A.: Determination of Activation Energy and Reaction Order in Premixed Laminar Flames, Univ. Louvain, Belgium, Tech. Summ. Rept. AFOSR TR 59-36, Contract AF 61(514)1245 (Febr. 1959), 63 p., AD 213039. 14. VAN ITTERBEcK, A., and O. VERBECKE: Cryogenics 2,79-80 (Dec. 1961). 15. VAN ITTERBEcK, A., H. ZINK, and O. VAN PAEMEL: Cryogenics 2,210-1 (June 1962). 16. VAN ITTERBECK, A., and O. VERBECKE: Cryogenics 1, 77 -80 (1960). 17. VON ZBOROWSKI, H.: Raketentriebwerke auf der Salpetersaurebasis und ihre spezifischen Antriebsge• wichte, Schriften der dt. Akad. d. Luftfahrtforschung Nr. 1071/43 (1943), S. 90-126. 18. VERSCHOYLE, P. D.: The Ignition of Certain Monopropellants by the Adiabatic Compression of Bubbles, Part 1., ERDE Rept. 13R58 (JSRP Control No. 590403) (30. Jan. 1959), 18 p., AD 215075. 19. VOUK, V. B., and O. A. WEBER: Brit. J. Ind. Med. 9, 32 (1952). 20. VANDERHYDE, N. J.: Normal Propyl Nitrate Storage Test, US Air Force Flight Test Center, Edwards AFB, Calif., Rept. No. AFFTC TN 56·12 (Febr. 1956),40 p., AD 92050. 21. VON SCHICK, 0.: Angew. Chern. H2, 547 -56 (1950). 22. VAN VORST, W. D., and R. C. AHLERT: J. Chern. Engng. Data 9,345-8 (1964). 23. VANPEE, M., A. H. CLARK, and H. G. WOLFHARD: 9th Symp. on Combust., Academic Press, New York and London (1963), p. 127 -3:3. 24. VANPEE, M., H. G. WOLFHARD, and A. H. CLARK: Flame Studies of High Energy Fuels and Oxidizers, Reaction Motors Div., Rept. RMD-1·P (Oct. 1961), 26 p., AD 266086, vgl. auch: Combustion Insti• tute Paper WSS, CI 61/22 (1961), 17 p., Ref.: CA 08, 3263g (1963). 25. V ANGO, S. P., and J. B. KRASINSKY: Density, Vapor Pressure and Viscosity of Solutions of Hydrazine Mononitrate in Hydrazine, JPL TM 33·103, NASA CR-78593 (15 Oct. 1962) 19 p., N66-38789. Hydrazine Mononitrate in Hydrazine, Supplemental Physical Data, JPL TM 33-122, NASA CR 50970 (24 March 1963), 15 p., N63-21071. 26. VERDERAME, F. D., and M. CODELL: The Determination of Hydrazine, Hydrazine Nitrate and Ammonia in Experimental Mixtures, Pitman-Dunn Labs., Frankford Arsenal, Philadelphia, Pa., Proj. No. TSI.47-8, Memo Rept. MR·557 (Sept. 1953),7 p., AD 17095. 27. VAN ITTERBEcK, A., and W. VAN DAEL: Adv. Cryog. Engng. 9, 207-16 (1964). 28. VANICA, D. F., and J. H. BEVERIDGE: Adv. Cryog. Engng. 9, 513-20 (1964). 29. VAN ITTERBEcK, A., A. DE BOCK, and L. VERHAEGEN: Physica 15,624 (1949). 30. VAN ITTERBEcK, A., and A. DE BOCK: Physica 14,542-4 (1948). 31. VLIET, G. C., et al.: J. Space cr. and Rockets 1,666-72 (1964).' 32. VAN DER AREND, P. C.: The Large.Scale Production, Handling and Storage of Liquid Hydrogen, Pro• ceedings of the Propellant Thermodynamics and Handling Conference, Ohio State Univ. Columbus 1959 (1960), p. 57 -62. 33. VOYER, R., and L. WElL: Adv. Cryog. Engng. 10, 110-6 (1965). 34. VARGO, E. J., D. B. Coopo, and J. B. PEARSON: The Containment of Molten Lithium Hydride at Elevated Temperatures, Thompson Ramo Wooldridge, Engng. Rept. 1 Jan. 1962-1 Oct. 1963. NASA CR- 54053, ER-5787 (15 Feb. 1964),75 p., N64·22462. 35. VOGT, J. W.: Measurement of Thermal Properties of LiH and LiH-Li·Mixtures: Enthalpy, Heat of Fusion Conductivity. Thompson Ramo Wooldridge Inc., Cleveland Ohio, TAPCO Div., NASA CR-57047, ER·4809 (June 1962), 77 p., N65-18147.

49* 772 Literaturverzeichnis W

36. VAUGHAN, J. C.: Effect of Chamber Pressure on the Performance of a Small Reverse-Flow Rocket Engine Wright Patterson AFB, School of Engng., MS Thesis (1964), 97 p., AD·610179, N65-20453. 37. VAN METER, R. A., at al.: Hydrogen Safety, US Bureau of Mines, Pittsburgh, Pa., NASA CR-75387 (Oct. 1965), N 66·29454. 38. VANP~;E, lVI., E. C. HINCK, and T. F. SEAMANS: Comb. and Flame 9, 393~403 (1965).

w

1. \VILKINSON, G.: Nature 168, 514 (1951). 2. WEBER, A., and S.1\1. FERIGLE: J. Chern. Phys. 20,1497 (1952). 3. \VEYMOUTH, F. R.: Hydrazinc·Chlorine Trifluoride Combustion and Performance Calculations, Bell Aircr. Corp., Project Rascal, Rept. 56·982, Contract W33-03Sac 14169 (1 Nov. 1947). 4. WHITTAKER, A., ct al.: J. Ani. Chern. Soc. 74, 4794~7 (1952). 5. WEAVER, R. D., G. C. WHITNAK, and E. S. C. GANTZ: Anal. Chern. 28, 329~32 (1956). 6. Westvaco Food Machinery anll Chemical Corp., New York: Storage and Handling of Dimazine, 3rd Ed., AD 94766. 7. WITKI:S: AMA Arch. Ind. Health 13, 34~6 (1956). 8. VVASSERBAUER, J. F., and \V. TABATA: Performance of Small (100Ib) Rocket Motors Using Coaxial In• jection of Hydrazinc and Xitrogcn Tetroxide, NASA TN D-1162 (Dcc. 1961), 27 p. 9. VVANHAINEN, J. P., It. L. DEWITT, and P. :S. Ross: Performance of a Low Thrust Storable Bipropellant Rocket at Very Low Chamber Pressure, KASA T~ D-678 (:\Iarol1 1961), 22 p. 10. WHITE, L .. and W. BARHETT: Anal. Chenl. 28, 15:~S~42 (1956). 11. \VEEKS, lV1. H., G. C. MAXBY. et ,,1.: Vapor Toxicities of UDxIH in Rats and Dogs fromShoJ't Exposures, Army Chern. Rl'S. and D"v. Labs .. ArlllY Chern. C~ntcr, :\Id., Report Proj. 7165, ASD TR-61-526 (Oct. 1961), 1ij p., AD 273490. 12. WITTE, A. B.: Expl:rimcntal Investigation of Heat Flux at the Upper Limit of Nucleate Boiling for Two Mixtures of Hydrazine and Unsymm. Dimethylhydrazine, CIT-JPL Tl'ch. Hcpt. 32-78 (6 April 19(1), S p. 13. WATT, G. \Y., and D. J. CHRISP: Ind. Engng. CI1('m. 47, 1206~S (11)55). 14. WANNAGAT, U., und H. KOHNEN: Z. anorg. aUg. Chem. 304, 276~95 (1960). 15. WILSON, R. Q., et al.: Am. Inst. CIH'm. Engng. J. 1: 2, 22 (1955). 16. WHlTNAK, G. C.: Anal. Chc·m. 28, S:{3~G (1956). 17. WINNING, W.l. H.: J. Chpm. Soc. [Loll(l.] 1954, 926 (1954). 18. WILSON, G. L., and F. D. ~IrLES: Trans. Farad. SOC'. aG, 356~63 (1940). 19. \VOLF, H., F. L GRAY, and B."\. REESE: Jet Propulsion 26,979--84 (1956) undARS-Preprint 255-55 (1955). 20. WATER)IAN, T. R., D. P. KIRSH, allliR I. HRABETS: J. CIH'm. Phys. 29, 905~8 (1958), 32, 304~5 (1960). 21. WOOLEY, H. W.: oJ. Hp-;. NBS 40, 16:l (194S), ~BS ltcs. Pappr 18(;4 und NBS Rppt. 2611, ,\]) 19900. 22. WALSH: Dilution of LOX When Xitl'ogen is Used for Pressurization, ~,\CA RI\I E58-A03a (April 1958}, 17 p. 23. WHITTAKER, A. G., and C. 1\1. DREW: J. Ph~'s. Chem. 61, 3S2~4 (1957). 24. WILLIAMS, G. C., C. N. :SATTERFIELD, and H. S. ISBIN: ARS-J. 22, 70~7 (19;32) und ARS Preprint 29-51A. 25. WALTER, H.: Jet Pl'opuiBion 24, 166~71 (1954) und ARS-Preprint 120-53. 26. \VALTER, H.: Bprieht libel' die RakeiPntriebwcrke auf Grundlage des 1'-Stoffes, Sc:hriften d. dtsch. Akad. d. Luftfahrtf., Heft 1071/43 (1943), S. 65-89. 27. \VILLIS, C. M.: The Effect of Catalyst-Bed ,\rrangpment on Thrust Buildup and Decay Time for a 90% Hydrogen Peroxide Control Rocket, KASA TX D-51G (Sept. 1960). 25 p. 2S. \VANHAlNEN, J. P., P. S. l{oss, an(l R. L. DEWITT: Effect of Propellant and Catalyst Bcd TpmppraturE's on Thrust Buildup in Scyeral Hydrogen Peroxide Reaction Control Hockets, NASA TN D-480 (Oct. 1960), 25 p. 29. WHITE, D., A. S. FRIlm:.\IA)[, and H. L. JOHNSTON: J. Am. Chem. Soc. 72, 3927~30 (1950). 30. WAGMAN, D. D.: oJ. Rps. Nat. Bur. Stand. 34, 143~61 (1945). 31. \YILKINS. R. G.: The Insulation of Tanks for the Storage of Liquid Hydrogen, British Rocket Propulsion Establishment RPE Tech. Note 200 (~larch 1961), 16 p. 32. \YI:-;TERSTEBN and MATHEWSO)[: Safe Ibndling of Liquid Hydrogen in til(' Laboratory, l~adiation Lab. R:'p. UCRL-3072, Univ. of ralif., Bl'rkeky. Calif. (1955). 33. WYATT, O. H.: oJ. HIS 18, 240~5 (1961~62). 34. WEBST~JH, T. J., and K. C. S:.\IITll: J. BIS 18. 172--S0 (19(i1~G2). 35. WILCOX, K. K.: Adv. Cryog. Engng. 2, 125 (1960). 36. WEITZEL, D. H., and R. K. HERSHEY: Adv. Cryog. Engng. 1, 122~30 (1960). 37. WOOLEY, H. W., R. B. SCOTT, and F. G. BRICKWEDE: J. Res. Nat. Bur. Stand. 41, 379~475 (1948) und NBS Res. Paper RP 1932, USDC. 3S. WHITE, D., H. Ru, and H. L. JOHNSTON: J. Am. Chem. Soc. 76, 2584~6 (1954). 39. WICKE, E., und E. U. FRANCK: Angew. Chemic 66, 701 (1954). Literaturverzeichnis W 773

40. 'WHITE, E. L., and F. W. FINK: Materials of (Jonstruction for Handling Fluorinf', Proceedings of the Pro• pellant Thermodynamics and Handling ConferPllcC', Ohio State Univ., Special Rept. No. 12 (June 1960), p. 161-81. 41. WHIT ACKER, G. C.: Corrosion 6, 283 (1950). 42. WICKE, E., und H. FRIz: Z. f. Elektrochemie 57, 9-16 (1953). 43. WITZKE, W. R., G.M. PROK, and T. A. KELLER: Design Considerations of a Condensing System for Vapori• zed Magnesium, NACA RM E55-120 (1955). 44. VVRIGHT, C. C., and H. H. WALTERS: Single Tube Heat Transfer Tests to Gaseous and Liquid Hydrogen, Wright Air Dev. Center WADe Rppt. 59-423 (Aug. 1959). 45. WEEKS, J. L., C. L. CHERNICK, and M. S. MATHESON: J. Am. CIlC'm. ::-loc. 81,4612-3 (1962). 46. 'WILSON, R. H.: J. Am. Chern. Soc. 73, 5514 (1951). 47. VVILSON, R. G., et al.: Nat. Bur. Stand. Cire. 523, 111 (1954). 48. VVILSON, E. 1\1.: An Investigation of the Gawline and Mixed Fluorine and Oxygen Propellant Combination, ..\nojet Gen. Corp. Rep. 763 (1 June-15 Aug. 19(3). Contraet X:462, Task Order III. 49. WILSON, 1'1.: J. ARS 23, 368-9 (1953). 50. WILSON, E. M.: US Pat. :104:3099 (10 July 1962), Rd.: C.. \ 57, 12778a (1962). 51. WALTERS, C. J., and J. :\1. S~nTJ[: Volumetric Behavior and Thermodynamic Propertie, of Ethylene Oxide, CIll'Ill. Engng. Progr. 48. 337 -43 (1952). 52. \VEISS, S., and 1. A. (;OONIAN: Adv. Cryog. Engng. 5, 1I"i7-·61 (1960). 53. \VINTERNITZ: Theoretical, Labomtory and Experinwntal InvC'stigations of High Encrgy Propellants: DiboraJlP, Reaction Motors Tne .. SUlllmluy Ropt. H1\U-293-52 (1950), 17 p.

;)4. WIKTERNITZ: Theoretil·al, I~aboratory and ExperilllcntallnHst igations of High Encrgy Propellants: C2H 2 NH3 -I- O2, Reaction J1otors Inc., Summar~' Report lUH·2B:3-;)1 (Out. 1950). unelas,ified. X1'1181169. 55. 'VISE, H., and M. F. FRECH: Kim·ties of lkaction Bl'tw('ell Ammonia and Oxygen, CIT-JPL Progress R<:pt. 20-192 (0) Jan. 1954),18 p., )\1) 27894. 56. WHATLEY. A. T., and R N. PEASE: J. Am. CIH'm. SOl'. 76, 19B7 ~-9 (19M). :57. WALTON, A. L .. anll A. n. TA~"lm: NIKIh\.JAX 1'I'Opdlant Ckanlilll'~' Invpstigatipn. Douglas Airel'. Co., Strr. jlonica. nept. S::\I·:2i:107. l'ontmct IH :1O-(Hi9·0HD-1295 (10 .. \priI19iii). o\D 143421. ;"i8. WEBER, L. A., et al.: Cryogenies 2. 236--tl (June 1B(2). 59. WARD, D. L., D. G. PEAHCE, aJHl D. J.;\IERHETT: .. \dv. CrY0i!. Engng. 9. :390-400 (19(j4). 60. \YIUSS, H. G., et a!.: AL\O\ J. 2, 2222 :3 (1B64). 61. WAYMAK, D. H., and R. L. POTTER: ('c··mb. ami Flanll' 1, 321--9 (1957). 62. \\'ILLUl\lS. \\'. H.: Th(']'m()d~-namie Charl~ for til(' ComiJustion Products of NitriC' "\"id andK{'1'oSelle. Brit. Aeron. TIps. Counl'il. Hep. & Mnl1. 29H2 (FOl'nwrl,\- c\ HC H'port 16 50;i) (l9ii!l). R 1'. 63. WlIITTAKER, A. G .. et al.: J. l'hys. Chcm. lY: liO, \)04- 9 (l!li;O), Y: (;1. 3Htl-94 (1!!;"i7), 64. "'ILLIAiIlSON, F .. and E .•JD!: Yariahlc-Thl'm:t Propubioll for a Soft-Landini! Yehiek. AHS l'n'print 24H1· 62 (19(;2), 7 p. 65. WALTEH, H.: Develupment of Hydrogpn Peroxidp Hoekets. in: History of Gellllan (iuidecll\Iissill's 1)(>\"(·• lopnwnt, AGAHDogrnph 20, Yerlag Appelhan~ & Co., Braunsehwpig (1957), p. :W3--2NO. 66. \VINTUC](Y: Anal~-tieal Comparison of Hydrazine with Primary Propellants a~ the TurbiJl(' Dli\(' Fluid for Hydrogen-Fluorinp and Hydrog"n-Oxygen Altitm!(' Stag!' Hockets, KM'.. \ '1'1\ D·78 ().ot. 1\l(9), 26 p. 67. \YILSOK, F. jI., and J. I\". FELInLU(K: .. \(1\'. Cryog. Engng. 111, 145-5:1 (19(j5). 68. 'WILLIS, \N. L., and J. H. S,nTJl: Detel'liOl] of Density Yal'int i('n~ in Flowing Two-Phase Hyc\lCW n. A(;\". Cryog. Engng. to. :12:3-- 9 (1\lG5). 69. \\"INTERKITZ. P. F.: Test Jldlwtl~ for Jlolloprop,·lIanl,. ,\HS.Prcprim 2:~li·;i;; (19;);;). 70. WAESCHE, n. H. \\".: AH~-,r. 29. :l7ii-li (195B)' 71. WILDE, K ...\.: Tnd. Engllg. Chem. -tH. 7li9-73 (1\l;)li). 72. VYILDE. K ...\.: .J. Ph~-,. Chem. (it, :ltl5-tl (1957). 73. WHITTAKER, A. G., ('t ttl.: BUl'Iling Hate Studil'~, Part I: EfI'eet of Several Physical Variabl(·s Oll Consump• tion Rate During Burnillg of the Sptem 2-N'itrnpropanejWFN'A, XOT::-l 599, NAVOH]) Hept. 1999 (21 Nov. 19(2), 23 p., .AU ;)889. 74. WOLFHARD, H. G.: Fuel 34, 60-7 (Jan. 1955). 75. WILLIAMS, H., A. G. WHITTAKER, and P. M. RuST: Burning RateStudies, Part 2, NOTS 10tlii. X.-\VORD Rept. 1999, Part II (31 March 19(5), 48 p., AD 77096. 76. WHITTAKER, A. G., and H. WILLIAMS: Burning Rate Stmlil's, Part 7, NOTS 1470. XAVORD Rept. 1999, Part VII (25 May 19(6), 14 p., .-\D 116973. 77. \VEIR, F. VV., D. VV. BATH, and M. H. WEEKS: Short-Term Inhalation Exposun·s toPentaboranp-9, Army Res. and De\,. Labs., Army CIH'm. Center, Rept. Proj. 7165, A::-lD TR 61-663 (Dec. 1961), 6 p., AD 273484. 78. WIRTH, H. E., and E. D. PAL~fER: J. Phys. Clwm. 60, 914-6 (July 1956). 79. W ASZECIAK and MCCARTHY: Determination of Heats of Combustion of Compounds Containing Boron, Olin Mathieson Chem. Corp., Tech. Res. Rcpt. MCC-1023-TR-9 (17 Dec. 19(3). 80. WALLENSTEIN and PROSEN: Bond Energies and Heats of Formation of Some Boron Compounds, US Nat. Bur. Stand. Rept. 3455 (30 June 19(4). 774 Literaturverzeichnis Y

81. WAGMAN et al.: Thermodynamic Properties of Boron Compounds, USNat. Bur. Stand. Rept. 3456 (30 Aug. 1954). 82. WESTLAKE, E. F., and A. A. TAMAS: Safety Handling Instructions for HEF·2, Wright Patterson AFB, WADC, Aero Medical Lab., WADC·Tech. Rept. 58·321 (July 1958), 10 p., AD 155748. 83. WOLFHARD, H. G., A. H. CLARK, and M. V ANPEE: Characteristics of DiboraneFlames, AIAA·Preprint 63· 500 (1963). 84. WIEBENGA, E. H., et al.: Adv. Inorg. Chem. Radiochem. 3, 133-69 (1961). 85. WENTWORTH, R L.: Stability of Hydrogen Peroxide, Mass. Inst. Technol., Cambridge, Quart. Period. Status Rept. (31 Dec. 1952), 14 p., AD 2212. 86. WEISS, H. G., and E. B. KLUSMANN: J. Am. Chem. Soc. 84, 4993 (1962). 87. WHALEY, T.P.: US Pat. 2968917 (6.5.1954/24.1.1961), Inh.: Ethyl Corp., New York,Ref.:CZ1962, 7389. 88. WIBERG, K. B.: Bicyclic Small Compounds and the Chemistry of Cyclopropene and Its Compounds, Washington Univ., Seattle, AROD·2966·1 (1962), 7 p., AD 426877, N64·19271. 89. WEIR, F. W., et al.: A Study of the Mechanism of Acute Toxic Effects of Hydrazine, UDMH, MMH and SDMH, Hine Labs., Inc., San Francisco, Calif., Contract DA·18·108·AMC·19·A, AMRL·TDR·64·26 (April 1964), 32 p., N64·22373, AD 601234. 90. WURSTHORN, A. M.: Raketentechnik u. Raumfahrtf. 8,128-37 (1964). 91. WELEFF, W., W. F. EMMONS, and H. S. MCQUEEN: Adv. Cryog. Engng. 10, 50-55 (1965). 92. WOLFE, S. W., and R. F. YURCZYK: Adv. Cryog. Engng. 10, 259-64 (1965). 93. WILLIAMSON, K. D., and J. R. BARTLIT: Adv. Cryog. Engng. 10, 375-81 (1965). 94. WIBERG, E., und R BAUER: Z. Natud. 6b, 171 (1951). 95. WAHLQUIST, A. L., and G. C. PANELLI: J. of Spacecraft and Rockets 2,452-3 (1965). 96. WILSON, J. N.: Estimated Stability of Perfluoroammonium Ion and Its Salts, Am. Chem. Soc., Adv. in Chern. Series Vol. 54, Advanced Propellant Chemistry (1966). 97. WHITNEY, E. D., ct al.: J. Am. Chern. Soc. 86, 4340 (1964). 98. WOOLLEY, H. W., R B. SCOTT, and·F. G. BRICKWEDE: J. Res. NBS 41,379 (1948). 99. WALTER, R J., and W. T. CHANDLER: AIAA·J. 4, 302-6 (1966). 100. WHITE, W. D., D. M. CHIN, and J. L. JONES: Fluidized Metal Fuel Composition, US Pat. 3243326 (24. 3. 1958/29. 3. 1966), US Navy, Ref.: CA 64, 17348 (1966). 101. WELLMAN, H. B.: Ethylene Oxide Monopropellant, US Pat. 3236046 (11. 2. 1960/22.2. 1966), Ref.: CA 64, 14019 (1966). 102. WETMORE, W. H.: High Energy Upper Stages - Potential Applications and Selection Criteria, AIAA Paper 65·345 (1965). 103. WANHAINEN, J. P., H. E. BLOOMER, and D. W. VINCENT: NASA TM X·52253 (1966). 104. WILBER, P. C., et al.: On the Spontaneous Ignition of Systems at Low Pressures and Temperatures, Combustion Institute, WSS 1964 Fall Meeting, Paper 64·29. 105. WASKO, R A.: AIAA·J. 1, 1919-20 (1963). 106. WROBEL, J. R, and C. GRELECKI: J. of Spacecr. and Rockets 4,347-53 (1967). 107. WENGER, N. C., and J. SMETANA: Liquid Hydrogen Density Measurements Using an Open. Ended Micro· wave Cavity, NASA TN D·3880 (Oct. 1966) 17 p., N66·38144. 108. WEITZEL, D. H., et al.: Elastomeric Seals and Materials at Cryogenic Temperatures, Wright Patterson AFB, Reports ASD·TDR·62·31 (May 1963) 132 p.; AFML·TDR·6!·50 (March 1964) 141 p. Part II (March 1965) 100 p. Auch erschicnen als NBS Cryog. Lab. Repts. 7947, 8244 und 8809. 109. WHITTICK, J. S., J. NEFF, and R F. MURACA: Physical Properties of Liquid Oxygen Difluoride and Liquid Diborane: A Critical Review, Stanford Res. Inst., Menlo Park, Calif., SRI·951 581-4, NASA CR· 88519 (1 July 1967) 48 p., N67·37539. 110. WIESBOCK, R. A.: Alkyl Difluoroamines for Use in Propellants, US Pat. 3346639 (19.11. 1963/10. 10. 1967), Inh.: Rohm and Haas, Ref.: CA 67, 10416 (1967). 111. WEAST, R C. (Editor): Handbook of Chemistry and Physics, Publ. by The Chemical Rubber Co., 47th Edition (1966).

y

1. YAKOLEWA, T. V.: Spektroskopische Untersuchung des Systems HNOa/NOz/N204/H20 (in Russisch), Schurnal neorganitschesskoi chimii 2: 12, 2782-7 (1957). 2. YASTREBOV, V. V., and O. J. KOZUNENKO: Russian J. Phys. Chern. [London] 35: 12, 1319 (1961). 3. YASTREBOV, V. V., et al.: The Physical Chemistry of Concentrated Ozone, Russian J. Phys. Chern. Ab· stracts Issue 33, 26 (1959), Ref.: Explosivstoffe 9, 44 (1960). 4. YASTREBOV, V. V.: Russ. J. Phys. Chern. 34, 21-3 (1960). 5. YASTREBOV, V. V., and N. T. KOBOZEV: Russian J. Phys. Chem. 33,118-22 (1959). 6. YOUNG, D. A.: Research and Developmcnt of Hydrogen.Oxygen Rocket Engine, Model XLR·AJ·2, Aerojet Engng. Corp., Final Rept. 397, Contract NO a(s)8496 (28 Sept. 1949). 7. YOUNGLOVE, B. A., and D. E. DILLER: Cryogenics 2, 348-52 (Dec. 1962). Literaturverzeichnis Z 775

8. YOUNGLOVE, B. A., and D. E. DILLER: Cryogenics 2, 283-7 (Sept. 1962). 9. YOUNG, J. A., et al.: Ind. Engng. Chem. 48,1375-8 (1956). 10. YAMAMURA, S. S., and J. H. SIKES: Anal. Chem. 35, 1958-60 (1959). 11. YATES, G. B., and A. R. PERL: Spark Ignition Parameters of Cryogenic Hydrogen in Oxygen and Nitro• gen Mixtures, Adv. Cryog. Engng. 10, 265-72 (1965).

z

1. ZAHRINGER, A. J.: Propellant Notes, Missiles and Rockets 1957/5/82. 2. ZUBER, N., and E. FRIED: ARS·J. 32, 1332-41 (1962). 3. ZABETAKIS, M. G., A. L. FURNO, and G. H. MARTINDILL: Adv. Cryog. Engng. 6,185-94 (1961). 4. ZIMA, G. E., and R. N. DOESCHER: Metal Progress 59,660-3 (1951). 5. ZUCROW, M. J., and C. F. WARNER: ARS·J. 20,139-50 (1950) und ARS Preprint 14·49. 6. ZABETAKIS, M. G.: Adv. Cryog. Engng. 8, 236-41 (1963). 7. ZUCROW, M. J.: ARS·J. 22, 323-30 (1952) und ARS Preprint 55-52. 8. ZABELKA, R. J. (Purdue Univ., Lafayette, Ind.): The Combustion of a Hydrazine Gel, Western States Section, Combustion Institute Paper WSS CI 63-1 (March 1963), 33 p., N 63-21805. 9. ZWICKY, F., and F. J. EWING: US Pat. 3048007 (31. 3. 1944/7. 8.1962), Inh.: Aerojet Gen. Corp., Ref.: CA 57, 15403h (1962). 10. ZABETAKIS, M. G., C. M. MASON, and R. W. VAN DOLAH: Safety Characteristics of Normal Propyl Nitrate, US Bur. of Mines BM-RI-6058 (1962), 31 p. 11. ZABETAKIS, M. G., D. S. BURGESS, and C. M. MASON: Research on the Safety Characteristics of Normal Propyl Nitrate, US Bur. of Mines, Progr. Rept. No.1, Contract NOrd-03082, 14 Sept.-31 Oct. 1955, 19 p., AD 79183. 12. ZLETZ, A., and D. R. CARMODY: US Pat. 2970428 (7.2.1961), Inh.: Stand. Oil Co. Indiana, Ref.: CA 55, 11852a. 13. ZIEBLAND, H., and M. T. DUPREE: ARS-J. 31, 845-8 (1961). 14. ZELMAN, 1. M.: Adv. Cryog. Engng. 9, 153-60 (1964). 15. ZETTLE, E. V., R. W. RIEBLING, and S. D. CLAPP: Chamber Technology for Space Storable Propellants, AIAA First Propulsion Joint Conference (1965). Namenverzeichnis

Abel, E. 394, 717 [A 39] Altman, D. 73, 74, 76, 93, 97, Armstrong, D. L. 452. 457, 458, Abendroth, H. J. 742 [J 5] 117,196,217.284,594,595.607, 503, 552, 553, 564, 717 [A 50], Abransom, A. E. 663,717 [A .'54] 717 [A 62J, 718 [A 71, 72], 735 718 [A 86] Achilles 121, 176 [G 71] Armstrong. G. T. 299, 300, 339, Ackeret, J. 17, 25, 31 Altshuller, A. P. 501, 587, 718 [A 340, 343, 626, 716 [A 1, 2, 7]. Ackerson-Ogg, B. 521, 526, 717, 78J 750 [M 66] [A 24] Altwicker, E. R. 588, 589, 718 [A Army Chcmical Center 415, 449, Adam, A. R. 514, 717 [A 36] 81, 82] 716 [A 18], 717 [A 21,32] Adams 501, 587, 742 [J 37] Ambrook, G. S. 207, 218 Arnett, R. W. 361, 717 [A 52,56] Adams, D. F. 300, 717 [A 44] American Petrol Inst. 717 [A 37] Arnold 528, 717 [A 28] Adams, G. K. 597, 685, 717 [A 61, Amstcr, A. B. 117, 273, 274, 286, Arp, V. 477, 717 [A 55] 64],718 [A 651 335, 458, 610, 654, 665, 718 ARPA 10 Adelman 702, 717 [A 58] [A 74, 75, 76, 77, 98, 99], 730 Arrick. C. D. 355, 717 [A 42] Adelman, B. 699, 717 [A. 63] [D 86] ARS-Committee 606, 718 [A 69] Addison, C. C. 407,411,716 [A 16, Anacker, E. W. 278, 279, 286 Asew, S. 356, 742 [J 43] 17] Anctil, A. A. 718 [A 95] Ash, A. B. fi04, 742 [.J 31] Adkins, A. \Y. 480, 487, 717 [A. 41] Andcrsen, \V. H. 166, 170, 173, Ashlcy, E. 438, 717 [A 31] 718 [A 87,881 177 Ashmore, P. G. 676, 717 [A 22] Anderson 155, 177 Askey. P. J. 717 [A 27J Adrian, F. J. 716 [A 9],747 [L 80] Anderson, R. 332, 333, 347, 348, ASTIA 757 [P 52] Aprojet-General Co. 471,576,717 716 [A 8],717 [A 45J Aston. J. G. 336, 568. 575, 585, [A 19], 718 [A 100J Anderson. R. C. 601, 605, 756 [P 717 [A 20,30,34,35] Aerojet-General Nucleonics 717 31],757 [P 55] Astrosystems 666 [A 25] Anderson, R. D. 601, 759 Atlantic Research Corp. 44, 65 AGARD 117 [R 58] Atz\\'anger, H. 345, 730 [E 3] Agosta, V. D. 286, 681, 768 Andcrson, W. A. 357, 717 [A 40] Au, G. F. 23, 31 [fl 273] Anderson, W. E. 502, 718 [A 79] Auble. C.:tV!. 658. 717 [A 53]. 739 Agoston, G. A. 195, 217 Anderson, W. S. 356, 760 [R 94] [H 82] Agron, P. A. 345, 717 [A 49] Andreasen, A. H. 1\1. 270, 271, 286 Audibert, F. P. 592, 71\3 [S 96J Ahlert, R. C. 522, 524, 597, 657, Andrews, D. G. R. 663, 675, 717 Audril>th. L. F. 521, 526, 527, 528, 718 [A 85J, 722, [13 142]. 771 [A 57] 539,717 [A 23,24,26,29],718 [V 22]. Andrus, R. J. 445, 447, 451, 743 [A 68,83],756 [P 11J Air Products and Chern. Inc. 340, lK 21] Aukerman, C. 615, 718 [A 96] 342,343.344,716 [A 5] Andrussow, L. 178,683,718 [A 90] AusHindcr, D. M. 185, 191 Albert, A. A. 716 [A 10] Angeloff, G. T. 114, 117,265,266, Avcry, H. E. 597, 718 [A 89] Aldrich, F. L. 749 [M 6] 285, 595, 604, 718 [A 70], 735 Aviation Age 716 [A 14] Allen, A. 769 [T 28J [G 72] Ayers, A. L. 551, 560. 688, 717 Allen, H. 330, 588, 638, 657, 714, Angelus, Th. A, 214, 218 [A 46, 47, 59, 60], 765 716 [A 6], 718 [A 80, 91. 94], 724 Ankerman, C. A. 743 [J 49] [8 186, 187] [C 9] Anschiitz, R. H. 490, 652, 717 Aylett, B. J. 567, 568, 717 [A 33J Allen, P. L. 300, 327, 730 [E 4] [A 51] Allen, S. 361, 366, 717 [A 38] AntI, R. J. 681, 770 [T 82] Bachmaier, F. 118, 249, 252, 253, Alley, C. W. 412, 413, 716 [A 11, Antoine, A. C. 597, 718 [A 66, 67, 260,276,277,285,286,329.422, 15] 93] 423,424,537,538,540,705,723 Allied Chemical 294, 295, 296, 310, Apert, C. E. 445, 771 [V 3] [B 158, 189, 190].724 [204] 311,313,314,324,325,328,329, Appleton, J. P. 96, 98 Bachmann, D. 271. 272, 279, 286 330,331,332,333,334,363,406, Arbit, H. A. 718 [A 97] Back, K. C. 506, 581, 589, 719 407,410,411,414,716 [A 3, A 4, Arden, E. A. 609, 718 [A 73] [B 22, 23], 729 [D 58] 12, 13], 717 [A 431 Ardenne siehe unter von Ardenne Baddiel, C. B. 724 [C 8] Alspach, W. J. 361,491,718 [A 92J Armond. J. W. 382, 718 [A 84] Baden, H. C. 504, 655, 722 [B 130, Altman, 471, 717 [A 48] Armour, W. H. 309, 744 [K 41] 133] Namenverzeichnis 777

Baer, A, D. 156, 177 Bartlit, J. R. 475, 774 [W 93] Bens, E. M. 586, 722 [B 149], 752 Bahn, H. S. 98 Bartocha, B. 499, 723 [B 187] [M 140] Bailey, A. B. 461, 720 [867] Bartoo, E. R. 652, 770 [T 80] Reneon, 8. W. 605, 723 [13 178] Bailey, B. -:\1. 480, 487, 489, 720 Bartz, D. R. 354, 438, 512, 513, Berard, P. 486, 767 [S 24;"51 [B 66], 723 [B 167], 750 [M 70] 547, 527, 576, G37, 719 [B 81 Berger, A. W. 3.51, 368, 370, 372, Bailey, C. R. 652, 724 [B 199] 720 [B 76],738 [H 34] 373,374,381,720 LB 46, 47, 50], Bailey, T. E. 483,723 [B 172],724, Barua, A. K. 719 [B Hi] 738 [H 40] [B 198] Barura, A. K. 721 [B 101] Bergdorf, \Y. H. 445, 748 ]f. 92] Baisley, R. 1. 490 Basyrov, Z. B. 380, 720 [13 42] Ber!, E. 42G, 719 [B 36] Baisley, R. L. 740 [H 130] Bassyrow, S. B. 3.5;"}, 722 [13 1531 Ber!, W. G. 654, 655, 657, 705, 721 Baker, B. B. 300, 720 [B 74] Batel, :\I. 267, 285 [B 91, 92], 722 [E 131, 132, 141, Baker, D.l. 651, 652, 721 [881, Bath, D. W. 504, 773 lW 771 143],723 [B 1641 84,85] Battillo. H. 360, 414. 441, 458, Berlad, A. L. 376, 720 [13 4:3J Baker, D. J. 663, 721 [B 88] 487, 72-l [B 196] Berman, K. 203, 217, 710. 751 Baker, G. E. 298, 354, 527, 720 Bauer, H. F. 329, 724lB 211] [M 108, lOll] [B 75] BaneI', .J. 248, 251, 252, 254, 258, Berman, L. D. 412, i.,84, 71!l Baker, L. 200, 217, 255. 285, 285, 69H, ,H7 ]S 2;)8] lB 21J 549,652,673,683.686. (lBO, 721 Bauer. It. 4\)7, 774 [\\' 94] Bernard, J. J. 116, 118, 255 [B 82,95, 103, 105], i32 IF 39] BUlI?r, W. 501,722 [134J Bernard, i\1. L. 713, 721 [B 11-ll- Baker, L. L. 690, 702, 74;) [K 7S] Bau('r. \\'. H. 504, 587. G:34, 65;). 722 [B 11:3J Baker,~. L. 58H, 722 [Ii 1:).i] 721 lB HO]. 722 [n 1:)0.133,134, Bernard, ~I. L, J. 255, 2(jl, 28;i, Baldridge, J. H. 555, 720 [B SOJ 13Hl 69:3, 721 [B 109) Ball, J. J. 613, 723 [B li;i] Ball('r1~'. ( ;. L. :322, ;i24. 657, 718 Bernard, n. E. 415, 584, 681, 71\) BalL L. C. 321, 743 [.J .il] [,\ 8'i]. 722 [B 142] [B 20J R11y, E. C. C. 3;"iO, 720 [B 49] Reach,']L H. C. 502, ,i04, 737 [P65] Bernhardt. H. "L :l2;), 32(), 733 Bamford, C. H. Hi4, 721 [13 94] BealE', W. T. 20;l, 217 [G 3] Bamford, D. A. (i,4, 721 [13 94J lkatti. .J. It. 719 [13 l:l] BerllfsgenOSSi'llSchaft ,let" chemi• Banas, P. A. ;)37, 723 [B 16;3] Dentti('.1. R. 405, 723 [13 Li()] sehen Indllstrie 492, :37H, 723 Banehero, .J. T. :354. 3;i;". :")27. 720 Becro CIH'I11. Div. (P~IC) 109, 110, [B 1621 [B 75] 386, 3!!;;. 397, :)99, 400, 402, 404, Bessey. "'I..J. 4:"i0, 723 [13 15\)], 7G9 Bank" A. ,\. 325, 327, 711l ]B·!' ;jlll, (ii 1, ()72, G73, 710, 720 [T 5\)J 5,6] lB ;;;;1,722 [15 151,1 Be,-C"ridQP, J. H. 48!!. i71 [\' 28] Barbaras, G. D. 497, 72:l [B 184] Bcckett, J. A. :3\);"5, 72:3 [D 169] Bp),er, R. B. Hi6, 177 Barber, .J. R. 486. 770 [T 68] Beckmann. H. B. ;iOl, ;"j03, 722 BicgPr, \Y. 30 Bigplow, L. A. 300, 7ii() pi :"i:3] Barker, K F. ,j02, 718 [A 79] [D 127] Barnes, \\'. 681, 7a2 38] Biggers, g. A. 530. :383, 74H [M 81 P. [F Beebe.. J. L. 3i)9, 720 [B 54J Barnett, 6ii\!, 747 [1.. i')3] Billingham. n. fi:33, 7G7 [S 271] B('('f~, L. S. 725 [C 46] Bills, K. \\'. 1i7 Barnett, D. O. 48:), 72:l [B 183] Bedon, A. B. P. G60, 721 [13 89J Biltz, \Y. 40(i, 71\) [B 27] Barnett, H. C. 6;j5, 768 [S 287] Begulll, C. i\l. 329, 724 [13 Hl:i] Biondolillo, 8 .. 4;iO, 719 I B 38J Barr, \Y. J. 672, 721 [B 112] Beighh·y. C. ?II. .146, 547. (j()2, 720 Ban'ere, i\1. 30, ;")3, 65, \)7,101, l1H, Birch, H. J. 58\!. 752 PI 13;)] [B 71J Hm, Birdsall, C. )1. :l50. :),')3. :168. 369. 117,118,143,146, Hi4, 17U. Bpll Acro'ystems Co. mIl. 724 :171,372,373,72:) [13 174J, 742 l7G, 177, 178, 17\), 183, 184, 18'i. [13 2031 187, 188, 18\), 190, 1\l1, 1\)2, l!J4, [.J 14, 15, Hi] Bdl, J. E. 475, 483, 726 [C 73] 1\)8,202,206,207, 20S, 209, 210, Birdseye 719 [B 18] Bpll, H. K 706,709,757 [P ii2J 212,216,223,228,229, 23S, 248, Birley, H. \Y. 527, 664, 71!J [B 32] Bell, R P. 328, 7G1 [S H] 2,33,254,257,2.58, 2,3!l, 284, 28;"), Birmingham, B. W. 483, 72G [C 87] Bell('r, H. 605, 723 [13 1i7] 428, 42\), 430, 4i')0, 4\)\), 524, 5:W, Biron, D. 492, 726 [C 7:3] Belles, F, E. 437, 650, 721 [13 U7), ;i49, 575, 687, 61l9, 706, 71 L 712, Bisbee, \V. n. :):l3, 481. 720 [B 681 72\J [D 42],7-19 [M 28, 2H. 7H! [B 30], 722 [8121,122, 14-l]. BissC'!, E. R. 5()7, 71B [13 83J 30] 723 [B 185], 751 [M 1l7J, 7ii2 Bitten,!. F. 5:30, 732 l1" 2\11 Bellinger, F. 606, (i07, 722 [B 123, PI 120] Bittkcr, D. A. 96, \IS, G17, 723 Barrt'n', 8.97.98 124J [B 168J Barret, W. J. 445, 723 [B 160] Bellinger, T. F. 593, 720 [E 56J Bizjak, F. 767 [S 248J Barrett, W. 442, 443, 772 [W 10] Beltrami, R. T. 567, 71\) [B 33] Black, 1. A. 479, 480, 487. 717 Barrick, L. D. 719 [B 2\)] Beltran, 11. R. 681, 724 [B 202J [A 41], 718 l A 87, 88], 720 Barrick, P. L. 360, 361, 740 Bender 76 [B 77] [H 137] Bender, O. C, 412, 413. 414, 415, Black, R. P. S. 401, 720 [B 60] Barron, R. E. 562, 583, 749 [M 10] 416, :381, 584, U81, 71\) I.B 11], Blackman, A. \Y. 4\)9,723 [13 18(i] Barrow, R. l!'. 764 [S 120] 7G2 [S 24] Blackman, V. H. 17,31 Bartel, H. R. 178, 185, 190, 706, Bendcrsky, C. G54, 722 [B 118] Blackmon. J. B. 483, 723 [E 1821 722 [B 120] Benedict, D. C., 480, 489, 720 Blackwell, J. P. 595, 722 [B 147, Barth-Wehrenalp, G. 345, 719 [13 66], 723 [B 167] 148J [B 39] Benedict, W. S. 613, 719 [B 7] Blair, D. W. 263, 270, 273, 285 Bartlett, W. W. 403, 723 [B 155] Benguerd, F. 437, 732 [F 8] Blanchard, R. L. 360,720 [ll 64J 778 N amenverzeichnis

Blay, N. L. 588, 589, 722 [B 138] Breckenridge, H. L. 486, 723 Burden, F. A. 602, 723 [B 176] Bleich, A. 306, 321, 724 [B 212] [B 163] Bureau of Aeronautics 401, 720 Bleyle, G. A. 349, 720 [B 53] Bredemann, G. 291, 301, 321, 719 [B 61] Blind, P. P. 415, 743 [K 8] [B 26] Burg, A. B. 324, 341, 497, 504, Bloom, R. 386, 388, 395, 401, 403, Bredt, 1. siehe unter Sanger-Bredt 719 [B 1],722 [B 125], 723 593, 720 [B 57, 58, 62] Breen, B. P. 679, 748 [L 121] [B 188], 767 [S 251] Bloomer, H. E. 774 [W 103] Breisacher, P. 654, 721 [B 91] Burgeson, D. 489, 725 [C 49] Blundell, R. W. 588, 722 [B 137] Breitwieser, R. 461, 655, 722 Burgeson, D. A. 491, 720 [B 78], Bock, H. 522, 719 [B 28] [B 119], 768 ['1' 20] 723 [B 173] Boden 689, 721 [B 106] Brentari, E. Q. 355, 471, 722 Burgess, D. 415, 580, 719 [B 19] Boikina, B. S. 333, 756 [P 5] [B 146] Burgess, D. S. 459, 492 536 563, Boisson, J. 176 Breshears, R. R. 681, 753 [M 177] 719 [B 24], 734 [G 18].775 [Z 11] Boll, R. H. 298, 354, 527, 720 Breslin, A. J. 231, 238 Burgess, R. W. 479, 744 [K 57] [B 75] Brewer, J. 353, 720 [B 52] Burgoyne J. H. 602, 723 [B 176] Bollinger, L. E. 674,683, 721 [B93, Brewer, L. 769 [T 30] Burke, E. 602 732 [F 32] 96,98, 108] Brezing, D. 475, 723 [B 181] Burkhardt, B. 384 751 [M 110] Boncore, C. S. 770 [T 87] Brice, D. B. 418, 419, 420, 421, Burns 442, 444, 719 [B 25] Bond, A. C. 497, 733 [F 63] 719 [B 121 Burns, E. A. 529,584,723 [B 166], Booman, K. 437, 438, 719 [B 35] Brickwede, F. G. 464, 467, 468, 724 [B 191] Boorady, F. A. 724 [B 209] 469,470,772 [W 37],774 [W 98] Burns, J. 762 [S 40] Booth, H. S. 324, 331, 719 [B 3] Bridgforth, R. M. 617, 648, 707, Burrows, M. C. 652, 723 [B 171], Bormann, D. 340, 344, 760 [R 67] 721 [B 99, 100] 724 [B 200] Borok, M. T. 412, 719 [B 17] Brill, F. Z. 358, 757 [P 81] Burry, R. V. 631, 653, 678, Bosco, G. B. 488, 720 [B 70] Brinkley, S. R. 591, 690, 720 723 [B 170] Bost, J. J. 415, 584, 681, 719 [B 59], 721 [B 107] Burton, J. M. 174, 175, 177, 447, [B 20] Brinkman, F. E. 499, 723 [B 187] 563,719 [B 37], 721 [B 110, 111] Bost, J. L. 724 [B 201] Broadwell, J. E. 597, 722 [B 117) Burton, J. T. A. 354, 722 [B 152] Bostick, W. 17,30 Broatch, J. D. 249, 285, 674, 721 Burton, K. R. 488, 736 [G 142] Bougon, R., 724 [B 205] [B 113] Burton, M. 521, 728 [D 11] Bourgarel, M. H. 483, 724 [B 210] Brobysheva, L. A. 375, 756 [P 46] Burwell, W. G. 97, 98, 617, 724 Bovee, H. H. 417, 719 [B 40] Brocher, 652, 721 [B 83] [B 197] Bowen, E. J. 527, 664, 719 [B 32] Brockaw, R. S. 476, 614, 662, 917 Buscaglia, R. 417, 556, 580, 723 Bowen, J. R. 378, 722 [B 150] [B 14], 721 [B 86], 724 [B 192] [B 157] Bowers, V. A. 716 [A 9] Broihan, F. 537, 719 [B 34] Buschulte, W. 174, 175, 177, 706, Bowersock, D. C. 360, 487, 720 Bronson, J. C. 489, 720 [B 79] 709, 722 [B 116] [B 63,69] Brown, C. 351, 368, 369, 370, 372, Busemann, A. 657, 721 [B 87] Boyce, E. A. 562, 577, 578, 762 373,381, 720 [B 46,47,48, 50], Bussard, R. W. 14, 30 [S 26] 738 [H 40] Butler, E. M. 589, 722 [B 151] Boyd, W. K. 304, 731 [E 23], 742 Brown, D. D. 750 [M 76] Butz, J. S. jr. 195, 218 [J 42] Brown, H. C. 506, 767 [S 252] Byers, D. H. 417, 425, 720 Boyer, K. 475, 723 [B 180] Brown, M. H. 301, 720 [B 73] [B 41] Boyer, M. H. 686, 721 [B 104] Brown, P. E. 300, 303, 720 [B 72] Byington, H. W. 683, 687, 757 Boynton, C. F. 503, 722 [B 128] Brown, R. 155, 177 LP 78] Brabets, R. 1. 369, 371,720 [B 43, Browne, W. G. 72, 97 Byrkit, G. D. 528, 719 [B 31] 44],772 [W 20] Bruehl, H. 590, 722 [B 140] Bradley, J. N. 718 [A 89] Bruman, A. J. 414, 532, 724 Cabeal, J. A. 724 [B 201] Bradley, R. S. 407, 719 [B 15] [B 206] Cadogan, W. P. 349, 725 [C 45] Brandle, K. 345, 766 [S 222] Brunsvold, N. J. 388, 401, 593, Cady, G. H. 299, 302, 318, 331, Bragg, S. L. 353, 546, 720 [B 51] 720 [B 57] 345,348,724 [C 4], 726 [C 57], 729 Braidech, M. M. 453, 771 [V 1] Bryan,G.J.273,274,286 [D 35], 758 [R 7], 770 [T 66] Braman, R. S. 502, 504, 722 Buchanan, H. J. 413, 472, 724 Caine, G. 489, 725 [C 49] [B 126] [B 193] California Res. Corp. 703, 726 Bransford, J. W. 333, 719 [B 9] Bucknell, R. L. 360, 491, 721 [C 91] Branstetter, J. B. 655, 724 [B 102] Callery Chemical Co. 76, 103, 104, [B 207] Budd, S. M. 769 [T 51] 106,151,188,215,343,347,352, Branstetter, J. R. 589, 724 Buddery, J. H. 496, 730 [D 84] 469,495,501,503,505,506,507, [B 208] Buddery, L. H. 231, 238 511,586,587,588,590,612,634, Brauer, G. 324, 334, 339, 345, 347, Blichner 712, 724 [B 194] 639,641,642,649,670,676,708, 522, 719 [B 2] Buchner, E. 97 710, 711, 726 [C 63, 103, 104], Braun, R. J. 478, 720 [B 65] Bugg, F. M. 413, 472, 724 [B 193] 727 [C 107,108,111], 766[S 213] Bray, K. N. C. 72, 73, 96, 97, 98 Bull, W. C. 521, 728 [D 9] Cylvert, C. S. 617, 643, 671, 739 Brazinsky,1. 487, 723 [B 179] Bulter, G. W. 504, 722 [B 129] [H71] Breazeale, J. D. 346, 348, 719 Bumgardner, C. L. 722 [B 145] Cambell, P. G. 360, 720 [ll 63) [B 10] Bump, T. R. 430, 437, 438, 723 Campbell, E. S. 378, 725 [C 35] Brecht siehe unter von Brecht [B 161] Campbell, M. D. 486, 727 [C 134] Namenverzeichnis 779

Canright, R. B. 726 [C 88] Chern. and Engng. News 345, 726 Ooar, R. J. 461, 725 [C 52] Cantrell, T. D. 397, 768 [T 16] [C 61] Coates, G. E. 497, 727 [C 142] Canty, J. M. 479, 741 [13] Chern. Engng. 331, 586, 724 [C 3] Coates, R. L. 459, 727 [0147] Capener, B. L. 654, 665, 730 727 [C 106] Cochran, E. L. 716 [A 9] [D 86] Chern. Industries 324, 724 [C 5] Codell, M. 530, 771 [V 26] Caren, R. P. 486, 727 [C 136] Chemical Week, 293, 586, 725 Coe, C. S. 759 [R 59] Carey, L. 681, 728 [C 162] [C 54], 727 [C 105] Coffin, K. P. 409, 724 [C 12] Carhart, H. W. 537, 745 [K 83] Chemiker-Kalender 454, 456, 457, Cohen, 663, 726 [C 83] Carmichael, 509 460, 552, 553, 564, 587, 726 Cohen, A. D. 725 [C 46] Carmichael, J. L. 734 [G 52] [C 64] Cohen, M. S. 177,339,589,727 Carmody, C. R. 590, 705, 727 Cherenko, J. P. 727 [C 104] [C 109], 749 [M 1] [C 110] Chernick, C. L. 345, 726 [C 59, 60], Cohen, N. 238, 614, 743 [J 53] Carmody, D. R. 726 [C 92, 93, 94, 750 [M 64], 773 [W 45] Cohen, W. 221, 235, 238 95], 775 [Z 12] Cheung, H. 2~5, 238 Cohn, J. G. E. 577, 725 [C 16] Carnavos, T. C. 726 [C 90] Chevalerias, G. 194, 217 Colaluca, M. A. 757 [P 80] Carney, R. R. 483, 727 [C 125] Chi, J. W. H. 361, 473, 474, 490, Colbert, J. E. 618, 753 [M 175] Carpenter, C. D. 451, 725 [C 29] 727 [C 124, 132, 139], 728 Colburn, C. B., 339, 341, 342, 344, Carpenter, L. G. 521, 725 [C 24] [C 164J 724 [C 1, 2, 11], 726 [C 58], 727 Carpenter, R. A. 505, 586, 595, Chilenski, ,J. J. 598, 680, 727 [C 116, 130], 744 [K 27] 726 [C 102], 727 [C 113] [C 112], 728 [C 154] Colburn, J. L. 760 [R 92] Carstens, J. P. 644, 653, 678, 730 Chin, D. lVL 550, 774 [W 100] Cole, D. M. 10, 30 [D 82] Chrisp, D. J. 521, 772 [W 13] Cole, L. G. 674, 675, 724 [C 13], Cartan, F. 278, 279, 286 Christe, K. O. 327, 341, 460, 724 726 [C 56] Carter, 725 [C 22] [C 7], 727 [C 127, 128, 129, Cole, V. V. 506, 537, 725 [C 30, Carter, E. 591, 727 [C 122, 123] 148], 728 [C 156], 737 [G 150] 38] Carter, G. T. 310, 364, 366, 401, Christenson, H. 487, 755 [0 15] Coleman, H. 1., 451, 769 [T 50] 414,450,480,516,533,548,554, Christian, J. L. 357, 477, 727 Collins, J. D. 455, 727 [C 141] 555, 728 [C 157] [C 131] Colodny, P. C. 153, 176, 177 Carter, H. G. 476, 727 [C 118] Christos, T. 679, 681, 728 [C 161] Colora MeBtechnik 282, 286 Carter, J. M. 74, 93, 97, 594, 717 Chuan, R. L. 679, 728 [C 153) Colton, E. 521, 742 [J 9] [A 62] Church, B. E. 615, 718 [A 96] Comer, S. W. 412, 529, 727 [C 140, Carter, T. A. 360, 488, 720 [B 70], Ciepluch, C. C. 330, 638, 714, 724 144] 725 [C 44] [C 9] Commercial Solvents Corp. 726 Cinjarew, G. D. 207, 208, 218 Cass, W. G. 606, 726 [C 99] [0100] Claasen, H. H. 345, 726 [C 60, Castron. 366, 725 [C 40] Comstock, C. C. 404, 537, 725 62] Cassut, L. 726 [C 75] [031, 32], 755 [0 7] Clair-Ganz, E. S. 529, 728 [D 12] Casutt, L. H. 480, 492, 493, 725 Condit, P. C. 757 [P 79] Clapp, S. D. 646, 718 [A 97], 775 [C 47, 48], 726 [C 70, 84] Conelly, J. G. 477, 479, 481, 725 [Z 15] [0 53], 727 [C 138] Cavecche, E. H. 706, 739 [H 95] Clark, A. H. 504, 654, 705, 771 Connaughton,J. W. 709, 728 Cera, A. 724 [B 201] [V 23, 24], 774 [W 83] [0 155] Chaiken, R. F. 166, 170, 177 Clark, B. J. 663, 757 [P 57] Chakraborti, P. K. 719 [B 16] Clark, C. C. 521, 522, 523, 526, Connors, J. F. 30 Challonder, A. R. 284, 286 725 [C 23] Conolly, J. W. 459, 760 [R 88] Chamberlain, D. L. 319, 727 Clark, H. C. 323, 324, 724 [C 6] Conway, 1. B. 661, 662, 726 [C 79, [C 115] Clark, J. A. 358, 361, 483, 485, 487, 80, 81, 82] Chamberlain, D. W. 486, 727 726 [C 72], 727 [C 133], 747 Cook, G. A. 374, 378, 379, 483, 484, [C 135] [1, 57] 725 [C 36], 727 [C 117], 728 Chamberlin, R. 1. 231, 238 Clark, J. D. 442, 443, 451, 530, [C 159], 729 [D 46], 730 [D 72] Chambers, A. E. 328, 412, 413, 570, 686, 715 [C 17, 18, 19, 20, Cook, G. B. 597, 717 [A 64] 414, 480, 504, 761 [S 9], 761 21, 26, 33], 726 [C 89] Cooper, F. M. 710, 751 [M 107] [S 10, 21, 22], 766 [S 206, 207] Clark, W. J. 726 [C 68] Cooper, J. 751 [M 86] Chandler, W. T. 774 [W 99] Clark, W. L. 411, 727 [C 146] Coopo, D. B. 495, 771 [V 34] Chan, Yick-Kwong 417, 743 Clarke, R. F. 320,321,761 [R 123J Cope, 572, 581, 758 [R 18] [K22] Class, C. R. 471, 479, 726 [071] Copeland, B. K. 476, 614, 748 Chang, E. T. 526,727 [C 145, 149] Class, J. B. 567, 725 [C 27] [1, 107] Chang, F., 753 [M 156] Claude, G. 374, 725 [C 41] Coplen, H. 1,. 462, 480, 725 [C 50] Chanson, W. W. 6, 30 Clauser,M. U.17, 31 Corbett, R. J. 475, 483, 490, 726 Chao, G. T. Y. 350, 353, 546, 725 Claussen, W. H. 294, 725 [C 55] [0 73], 756 [P 39] [C 39] Cleaver, A. V. 401, 461, 593, 725 Corcoran, J. M. 727 [C 119], 755 Chatelet, 1. 724 [B 205] [C 42, 43, 51], 740 [H 119] [025] Chatelier, Le 68 Cleaver, C. S. 342, 724 [C 10] Corcoran, W. H. 428, 436, 437, Chelton, D. B. 358, 466, 483, 726 Clegg, J. W. 532, 756 [P 12] 441, 725 [C 28], 728 [D 18], [C 87], 728 [C 150] Clever, H. L. 360, 414, 441, 458, 758 [R 23, 24], 759 [R 31, Chelton, P. B. 462, 750 [M 52] 487,724 [B 196] 35] 780 Namenverzeichnis

Cordes, H, F, 441, 460, 529, 570, DAS Pat. Au~legeschrift 483, 729 Devoto, R. S. 730 [D 85] 576, 577, 725 [C 15, 21], 727 [D 48] De Vries, J. E. 529, 728 [D 12] [C 114, 14-3] Dauerman, 1...427,730 [D 76] De Witt, R. L. 309, 592, 679, 730 Corelli, R. 706, 726 [C 96] Davidson, D. L. 334, 730 [D 88J [D 67], 772 [W 9, 28] Corelli, R. M. 421, 607, 705, 726 Davies, A. 719 [B 4] Dexter, T. H. 738 [H 26] [C 101], 727 [C 121 J Davis 591 DORR Raumfahrttypenbl. 238 Corliss, O. 30 Davis, 1... 735 [071] Diamond, P. 578, 581, 728 [D 8] Corliss, W. R. 10, 12, 30 Davis, N. S. 400, 402, 593, 720 Di Cianni, N. 333, 746 [1.. 19] Corner,J. 144, 176 [B 58], 728 [D 23,24],729 [D 25, Dickinson, L. A. 654, 665, 730 Corrucini, R. .J. 471, 727 [C 137] 26, 56] [D 86] Cottrell, T. 1... 726 [C 981 Davis, W. 299, 318. 729 [D 33] Dieckamp, H. 1\I. 23, 24, 31 Courtney, W. O. 74, 98, 726 Davison. \1'. R. 644. 653, 678, 730 Diehl, J. M. 654, 671. 760 [R 73. [C 68] [D 82] 83] Covington, L. C. 304, 750 [M 57] Dawson, B. E. 333,334,728 [D 4], Dierdorff, L. H. 391, 728 [D 27] Cowan, P. L. 155, 156, 177 730 [D 66] Diesen, R. W. 597, 729 [D 51] Cowling, T. O. 31 Day, W. A. 414, 753 [M 1781 Diggle, W. 1\1. 38:3, 425, 728 [D 19J Coxe, Eo F. 478,726 [C 74, 85] DBP 209,217,282,286 Diller, D. E. 468, 774 [Y 7], 776 Coyle, C. F. 343, 716 [A 2] Dean, J. 462, 750 [M 52] [Y 8] Crabtree, J. M. 300, 303, 720 Dean, J. W. 483, 726 [C 87] Din, F. 511. 729 [D 29] [B 72] Dean. L. E. 438. 475, 54-G, 547, DIN-Normblatt 52612 280 Cragoe. C. S. 508, 725 [C 34] 602.720 [B 71],728 [D 17],729 DIN-Normblatt 52613 286 Cramer, K. H. 478, 726 [C 77] [D G2] DIN-Normblatt 51562 279. 286 Crampel, B. 97, 98 Dc Angelis, L. 744 [K 68] Di Paolo. F. S. 350. :368. 370, 372, Crane, C. H. 413, 727 [C 126] Dcnring, D. L. 730 [D 70,71] 373. 742 [J 13. 15] Crane, W. E. 755 [032] D8 Bock, "1.. 350, 351, 771 [V 2!), Disher, J. H. G55. 657, 729 [D 54] Crawford, B. L. 142, 161, 164, 176, 30] Ditter, J. F. 504, 729 [D ii7] 177,261,262,263,285 Dc Booy. H. T. 350, 361, 730 Dobbins, T. O. 228, 2:38 Crawford, R. F. 477, 728 [C 163] [D 87] Dobrowolski, 207,208 Cremer, J. 522, 732 [F 61 Dechema, 729 rD 32] Dodd, R. Eo 333, 728 [D 3] Crittenden 406,725 [C 14] Decker, W. H. BOO, 730 [D 77] Doerner, lVI. P. 567, 728 [D 13] Crocco, L. 116, 118,209, 217, 218, De Dapper, J. \\'. 507. 531. 532. Doescher, R. N. 29:3. 298. 301, 314, 602,604,726 [C 66, 67, 69. 761. 728 CD Hi], 729 [D 50] 729 [D 31],731 [E 22]. 775 [Z 4-] 727 [C 120] Dee, L.A. 52~ 571. 578. 730 Dolah, R. W. 533, 728 [D 14] Croomers, E ..F. 639,728 (C 151] [D 89] Donnan, F. O. 350, 720 [B 49] Cruddac:,. R.. O. 461, 720 [B 67] De Hartonlari, R. 597,757 [P 53] Donohue, J. A. 331. 730 [D 64] Cruico. W. 459, 737 [0 146J Deisenroth, U. 127, 176, 233. 2:34. Donovan, T. 1\1. 586, 729 [D 45] Cruslln, C. R. 360, 725 [C 44J 238 Dorf, C. J. 4-85, 739 lH 86] Cuddy, W. A. 116, 117, 600. 726 De Jaegere, S. 60G. 664, 677, 729 Dorsch, R. G. 657, 733 [F 53] [C 97J [D 4-3, 4-9] Doss, It. C. 595, 722 [B 148J. 729 Cullis, C. F. 657, 724 [C 8], 728 Dekker, K. W. 177 [D 52, 53] [C 152J Delgado, J. 1\I. R. 506, 589, 729 Dotson, R. E. 618, 753 PI 176J Curme, O. O. 554, 726 [C 65] [D 58] Douglass, D. A. 685, 724 [B 209] Curron, A. N. 616, 726 [C 78J, 728 Del Kotario, P. P. 597, 769 Douglass, H. W. 200, 217, 301. 307, [C 160] [T 45] 308,320,615,616,617,618,624, Curry, J. Eo 357, 728 [C 158J De Long, W. B. 301, 303. 750 627, 628, 629, 051, 659, 726 Curtiss, C. F. 160, 177 [M 5G] [C 78], 729 [D 37, :39], 730 [D 83], Cusack, J. H. 521, 725 [C 25] Dembro\\", D. 654, 721 [B 91], 722 754 [N 35], 755 [0 14J, 756 [B 141] [P 28, 29], 760 [R 66] Daclieu, A. 118, 224, 229, 231,238, Demetriades. S. T. 17,31 Douglass, J. B. 614, 737 [0147] 496,728 [D lJ, 730 [D 74] Dc MOllpY, F. VL 357. 477, 730 Do\\". R. H. 360, 491, 729 [D 47] Dale, J. W. 327. 3:33, 348, 728 [D 68] Dow Chemical Co.. 76. 584, 730 [D 2] Dempster, \Y. E. 483, 729 [D 63]. [D 80] D'Alellio. G. F. 500, 730 [D 75] 755 [08] Downes, H. 1. 592, 729 [D 59] Dalla Valle, J. 1\L 2G7, 285 Dengler, R. P. 357, 413, 533, 577, Downing, R. C. 291, 729 [D 30] Damm, R. 229. 2:38, G80 729 [D 61] Doyle, W. L. 557, 614, 625, 652, Dane, N. E. 70ii, 74:3 [J 45] De Palma, J. V. 730 [D 78] 662, 729 [D 38], 7:31 [E 25], 742 Daney, D. E. 485, 730 [D 79] Deppe, O. R. 3GO, 491,729 [D 47] [J 32]. Dangle, E. E. 461. 729 [D 34] Deremin, A. X. 606, 729 [D55, Draeger, A. O. 573, 728 [D 7] Daniels, F. 164, 425, 731 [E 17] 60] Drago, R. S. 537, 730 [D 65] Dannon, G. H. 562, 57G, 577, 580, Derr, D. F. 573, 728 [D 6] Drake, O. W. 719 [B 29] 737 [H 16] Derr, P. F. 578. 760 [R 98] Drayer, D. E. 471, 729 [D 41] Dantzig, O. B. 98 Dess, H. M. 345, 728 [D 5] Drell, 1. L. 650, 729 [D 42] DardarI', M. 488, 6£)3, 730 [D 69] Detmer, 0.327,764 [S 149] Drellishak, K. S. 618, 622, 735 Darwin, O. E. 231, 238, 496, 730 Deutschmann, A. J. 521, 728 [D 9] [062] [D 84] Devins, J. C. 521, 728 [D 10, 11] Dresdner, R. D. 343, 728 [D 21] Xamenverzeichnis 781

Drew, O. 1\1. 394, 728 [D 22], 772 Engelbrecht, A. 300, 331,.333, 339, I Filippov, Yu. V. 368, 731 [E 18], [W 23] 341, 345, 730 [E 1, 3. 7], 731 732 [F 16, 17], 762 [S 53] Drew, J. G. 480, 748 [L 109] [E 27, 35] Fine, A. L. 537, 732 [F 7] Driscoll, D. G. 486, 729 [D 40J English, W. D. 310, 731 [E 41] Fine, B. 430, 437, 732 [F 9, 10, Driscoll, D. H. 710, 751 [M 107, Epstein,:\1. 360. 487, U14, 731 15] 108] [E 36, 37J Fineman, S. 185, 191 Duboz, J. 442. 728 [D 16J Erdmann, V. O. 617,643,671,739 Finger, H. B. 30 Dllcarme, J. 65, !n [H 71J Finholt, A. E. 497, 733 [F 63J Dudley, F. B. 345, 729 [D 35] Erieson, G. L. 304, 731 [E 23J Fink, F. W. 301, 302, 30-1, 305, 306, Duffy, O. H. 436, 728 [D 18] Erikson, T. A. 606, 731 [E 24, 32J 471, 773 [W 40] Dufur 480, 728 [D 28] ErnwJl(" E. D. 415. 730 [E 9J Finkelnburg, W. lG, 30 Dugger, G. L. 590, 657, 740 Etlll'ridge, B. R. 477, 479, 481, Finn, R. F. 744 [IC 44] [H 118] 725 [C 53], 727 [0 138] Fisch, K. 6S1, 76;3 [S 175] Dumont, L. P. 730 [D 81J Etherington, T. L. 502, 731 [E 34] Fisch, K. R. 733 [F 5t!] Duncan, J. F. 300, 303, 720 [B 72J i~uckell, A. 275, 27U, 286 Fischer, J. :303, 742 [J 41], 758 Dunning, W. J. 74,98 Euler, Hi2 [R 1], 761 [S 2] Du Pont de ;";ctllours & 00. 343, Ellhwr, R. 613, 781 [E 2U] Fischer, W. 40G, 719 [E 27] 394, 728 [D 20J, 730 [D 73] Evans, D. D. 747 [L 70] Fischer, W. G. 368. 732 [F 20J Dupree, M. T. 548, 775 [Z 13] I~Hlils, U. n. :301, 4i1. 532, 731 Fish, A. 657, 728 [e 1;)2] Durie, R. A. 613, 729 [D 3U] [1£ 141 Fish, D. W. 460, 7;);') [028] Dwyer. R. F. 483,484,728 [0 159 J. Evans.. \L W. GOI, 731 [E 31] Fish, W. It. 414, ;)84, G81, 732 729 [D 46J, 730 [D 72] Evaas. ~. 317. 7,;8 I!{' 11]. 759 [F 42J Dykema, O. W. U.38. 66el, 729 [It 62] Fishburne, E. S. 378. 732 [F 21J [DH] E~'er('d, D. S. 29G, :l.31 , 407, 430, Fishman. N. 15G, 177, 418, 41\), 4:H. 43;3, 4;)7, 4(i4. 4ll7. 409, 420, 421, 719 [is 12] Eagan, E. P. 437, 731 [E 15J ;,)2\j, 564, 606, mJ7, 6\l8, 743 Fitzgerald, F. ;3;')1, 732 [F 2t!J Eb,n'stein, 1. J. 597,598,731 [E30, [K. 14] Fivel, H .•J. 6;)5, 657, 7:33 [F 48] 33J E\"'r;-st, D. A. i:31 [E -131 .Flage, It. A. G15, 7;');3 [0 12, 13] Eckert, E. R. U. 218 En I',\", R. L. G;,)8, 731 [E 40]. Flanagan, J. R 610, G18, 624, 733 Edeskllty, F. J. 461, 481, 483, 731 i/O ['1' 70] [F 67] [E 29,39].748 [L 100J Ewing, F .•J. 607, 77;j [Z 9] Flatt. It. 437, 732 [F 8] Edse, R. 378, 614, 651, 652, 674, Eylps, A. U. 47!J, 731 [E 3t!] Fletdwr, n. A. 299, 302, 318, 764 683, 721 [H 93, 96, 98, 108]. [~Yl'illg, H. -12.), i:31 [I~: 17 J [S 128J 731 [E 25,28],732 [F 21] Fletcher. E. A. 25G. 2;39, 260, 28;'), Edwards, U. D. 718 [A 74, 75J F,wth. G.}I. GlI). 7:~3 [F 711 :330,638, G55. H57, G91, 700, 701, Edwards, H. E. 591, 720 [B 59J Fagc-!'. .J. ;\. 7:33 LF (il] 714. 718 [,\!J1. 94J, 72-1 [09], Egerton 407. 731 [E 12] Fan. S. C. 3;)8. IfH [R lO-iJ 733 [F ;')0. ;j3, (jG], 71);') [S 185, Ehlers, It. O. 472.663,7:16 [G 141). Fan. S. S. T.W!J, 7-1H [:\1 ;')j 18!J] 747 [L 55] Farber, }L 7:W ra 5Ul FleteilCr, W. H. 32!J, 724 IB 1!J;)] Farquahr, J. -leSe). 70] W. U. LF Ehringell, A. O. 1;:52, 154, 177 n:3 IF Flieclel'. 48!J, 732 33J Eiscnbud, }I. 231, 238 Farrar, R. L. 328, 3-1". 7:H [1" 1] Flint, T.1:. 3:38. 37-i, G17, 734 Elbc sieh:- unt8r von Elbe Farrington. D. 2G1. 2U2. :l1l'') [C 22 J. 7(i7 [S :W:31 Fa';3tow,d,ij. W. (;. :3GS. n2 [F 19] Fin]'}" P. 127. 17(j Eldridge 603, 750 [1\1 68J J. Fatino. C. C. 413, 7;37 [1' 72] Floyd, U. 47;), 7:33 LF U8] Ellion. ThI. E. 681, 781 [E 42] J. Elliot, D. ;)93. 731 [E 201 F,wth, ~l. 1. 60;;. /:3:3 rF 51 J li'lyllll, T. }l. 491, 718 LA !J21 Fochtman, E. G. ;');)0, n2 [F 29J Ellis, 72;3 LO 22] Fcttkcs, F. 3n.~. 763 I.S 88J ~Fearn. It. F. 4.'\:3, 72:3[11 172J Fogelberg, C. \'. 48G, 7411 L ;')] Ellis, G. ~:. 98 Folt'}', \\'. T. 386, 389, 7:12 [F :l5] Ellis, .J. F. 300,327, 730 [E 4, 5, 6, FNt'!', J. 74, !!7 F,-(lor. A.. 4.38. 7;')2 PI 1-i 71 FOl\l'obel't, E. 367 8] J. .1'\'1161', F. 522. 7:52 [1" iii FontalHl, }l. C. 42S. 44;'), n2 Ellis, S. R. }I. 521, 731 [E 13] ll\'igl'l, H. 644, 733 [F (j!J] LF 13]. 743 IE. 1!JJ Elrod, O. W. 483, 731 [E 21] Feihor, O. E. 20U, 217, 3Ul, 30;'), 30G, FoO(l. }Ia(·h. and C]H'II1. Corp. 573, Elvcrum, O. W. 293, 294, 436. USIi. 702, 70:3, 7:32 [F 39], 734 I 7:31 [F 5] 437, 438, 678, 680, 719 [B 35]. [G 4

Foster, 607,733 [F 49] Gallaghan, J. 528, 736 [G 120] Gill, W. E. 412, 733 [G 13] Foster, R. H. 356, 732 [F 23] Gammon, B. E. 461, 654, 655, 736 Gilliland, A. A. 460, 736 [G 131, Fowle, A. A. 479, 480, 487, 490, [G 117, 118J, 768 [T 20] 132] Ginell, R. 162, 163, 164, 177 494, 720 [B 77], 742 [J 23], 750 Gantz, K S. C. 525, 529, 576, 578, Girdhar, H. L. 699, 702, 760 [R 82J, [M 70] 772 [W 5] Gard, G. 345, 729 [D 35] 761 [R 119] Fowler, E. A. 453, 771 [V 1] Gardner, J. B. 349, 364, 462, 480, Given, F. I. 601, 731 [E 31] Fowler, J. M. 474, 732 [F 30] 488, 736 [0 36] Glahn siehe unter von Glahn Fox, H. M. 500, 674, 721 [B 110], Gardner, D. ::\1. 454, 736 [G 110] Glaser, P. E. 479, 720 [B 77], 735 731 [F 3], 733 [F 64] Gartmann, H. 692, 699, 735 [G 93] B. Fraeijs de Veubeke, 30, 53, Glassman, I. 597, 598, 602, 603, 65, 97, 101, 117,143,146,176, [G 96] Gatti, R. 329, 333, 346, 733 [G 9, 604, 607, 726 [C 69, 76], 731 192, 194, 198, 202, 206, 207, [E 30, 33], 735 [G 69], 765 [S 208, 209, 210, 212, 216, 253, 10], 737 [G 157] Gause, R. L. 479, 753 [M 169] 156] 254, 257, 258, 284, 428, 429, Glemscr, O. 344, 760 [R 67] 430, 524, 526, 549, 575, 699, Gaydon, A. G. 769 [T 30] Gayle, J. B. 357, 366, 737 [G 159], Glockling, F. 497, 727 [C 142] 719] B 30] 745 [K 92], 761 [R 106] Glueck, A. R. 663, 735 [G 82] Frainier, R. J. 479, 486, 713, 733 Gaynor, A. J. 322, 734 [G 50], 741 Gluck, D. F. 487, 735 [G 77] [F 60], 756 [P 38] [H 135] Gmelin 351, 405, 406, 407,408,425, Franck, E. U. 294, 296, 298, 732 Geckler, R. D. 158, 160, 164, 454,464,467,509,510,525,734 [F 18, 27], 772 [W 39] 176 [G 27J, 736 [G 109] Francon, J. 687, 732 [F 40, 43] Geery, E. L. 475, 737 [G 152], 769 Godfrey, N. B. 560, 736 [G 133] Frankel, M. B. 733 [F 65] [T 29] Godwin, T. W. 302, 746 [L 39] Franklin, R. G. 686, 769 [T 40] Gelder, T. F. 735 [G 74] Gogorischwili, P. V. 529, 734 [G 24] Franson, K. D. 369, 720 [B 48] Gelernter, G. 751 [M 86] Gokcen. N. A. 526, 582, 727 [C 145, Fraser, R. P. 195,217 Gemmeker, L. 368,762 [S 54], 763 149] Frazer, J. W. 342, 731 [F 2], 733 [S 101] Goldbaum, G. C. 614, 737 [G 147] [F 56] Genco, R. S. 654, 736 [G 118] Goldberg, S. R. 417, 450, 734 Frech, M. F. 773 [W 55] General Dynamics/Astronautics [G 15, 31, 32] Freisinger, J. 21, 31 319, 321, 480, 736 [G 127], 737 Goldstein, M. S. 654, 721 [B 90] Friebertshauser, P. E. 686, 721 [G 153] Golzschmidt, W. A. 275, 286 [B 104] Genthe, D. 331, 367, 734 [G 29, Gonell, H. W. 270, 285 Fried, E. 473, 775 [Z 2] 47] Gonigle 406, 725 [C 14] Friedel, R. A. 444, 732 [F 12] George, D. 195, 218 Good, R. J. 472, 483, 735 [G 91] Friedman, A. S. 470, 742 [J 21],772 George, H. 289, 332, 334,353, 364, Goodfriend, P. L. 737 [H 12] [W 29] 471, 495, 503, 737 [G 158] Goodman, I. A. 478, 773 [W 52] Friedman, J. 316, 759 [R 54] George, J. W. 347, 737 [0151] Goodwin, R. D. 464, 470, 471, 735 Friedman, P. A. 680, 745 [K 98J George, P. D. 502, 734 [G 34] [G 90, 92], 736 [G 128] Friedman, R. 98, 166, 174, 536, Georgius, H. K. 487, 731 [E 37] Gorai, A. S. 417, 719 [B 40] 580,602,681,732 [F 32, 38], 737 Gerhart, F. J. 588, 755 [0 23] Gordon, J. 339, 733 [G 7J, 734 [H 17], 738 [H 24] Oerstein, M. 597, 654, 658, 735 [G 48] Friz, H. 298,476,773 [W 42] [G 68, 79], 736 [G 104, 118] Gordon, J. S. 436, 437, 438, 685, Froning, J. E. 292, 732 [F 26] Gerstenberg, H. 271, 286 734 [G 25], 735 [G 95, 98J, 736 Fruchtman, I. 732 [F 35J Getz, J. W. 573, 728 [D 7] [G 126, 145J Fuchs, R. 247, 284, 691, 692, 696, Giannini, G. M. 16, 30 Gordon, L. J. 189, 191, 228, 229, 238, 500, 603, 604, 734 [G 56], 697,699,732 [F 45, 46J Giarusso, G. A. 301, 412, 578, 770 Fuller, P. D. 463, 734 [G 42] [T 88] 735 [G 70], 736 [G 113] Gordon, S. 97, 98, 189, 191, 228, Furgason, R. R. 409, 731 [F 4], Giauque, W. F. 350, 352, 406, 408, 409, 429, 430, 508, 732 [F 11], 229, 238, 538, 617, 618, 619, 733 [F 57J 733 [G 12], 734 [G 33, 39], 755 620,621,622,625,626,627,628, Furno, A. L. 480, 492, 493, 597, [06] 631,644,645,646,650,663,707, 733 [F 47], 775 [Z 3] Gibb, J. W. 743 [J 49] 734 [G 57, 58], 735 [G 59, 60, Furukawa, G. I. 733 [F 52] Gibbs, J. B. 655,657,733 [F 48] G 61, 62, 63, 64, 65, 66, 78, 82], Furukawa, G. T. 732 [F 22] Giedt, R. R. 614, 743 [J 53] 737 [H 11], 739 [H 72] Giese, R. H. 48, 65 Gordon, W. E. 377, 739 [H 97] Gage, J. C. 383, 425, 728 [D 19] Giffin, E. 195, 217 Gortsema, F. P. 329, 737 [G 149J Gaines, J. M. 382, 736 [G 125J Gifford, W. E. 463, 734 [G 42] Goshgarian, B. B. 504, 705, 742 Gakle, P. S. 681, 736 [G 115], 737 Gift, R. D. 681, 737 [G 155] [J 36],743 [J 45J [G 154] Giguere, P. A. 386, 389, 390, 394, Gosnell, R. B. 357, 736 [G 139J Galbraith, H. J. 501, 504, 587, 589, 732 [F 25], 734 [G 37, 38, 51, 52J Gottfried, B. S. 487, 723 [B 179] 736 [G 116], 742 [J 37J Gilbeau, J. J. 488, 736 [G 142] Gottzman, C. F. 487, 735 [G 76] Gale, H. W. 654, 736 [G 137] Gilbert 664, 735 [G 86] Gould, J. 655, 660, 735 [G 94] Gall, J. F. 289, 290, 291, 323, 331, Gilbert, M. 185, 191, 597, 706, Gould, J. R. 342, 588, 589, 687, 338, 610, 734 [G 44, 45, 49] 735 [G 71, 100, 101, 102], 736 732 [F 44], 733 [G 1, 2], 736 Gallaccio, A. 445, 755 [0 3J [G 103], 752 [M 119] [0 119], 737 [G 148], 757 [P 68] N amenverzeichnis 783

Gould, R. F. 1)00, 501, 503, 504, Groesbeek, 'V. A. 472, 483, 737 Hamel, E. E. 460, 755 [0 28J 736 [G 114J [G 161 J Hamilton, B. R. 695, 739 [H 92] Gourdine, M. 0.17,31 Gross.Gronomski, L. 437, 736 Hamlin, A. G. 300, 741 [H 134J Grace, W. R. 573, 734 [G 17J [G 123] Hammel, E. F. 461, 475, 481, 731 GraefE" A. F. 566, 567, 734 [G 19, Grosse, A. V. 310, 335, 336, 337, [E 29J, 740 [H 132J, 741 [H 140J 20J 338,345,372,374,375,377,613, Hammond, J. A. 655, 739 Graham, R. W. 438, 472, 473, 734 614, 617, 661, 662, 667, 726 [H 85J [G 41J, 736 [G 140, 141, 144J, [081, 82], 733 [G 8, 11], 734 Hamrik, J. T. 595, 723 [B 169] 759 [R 37, R 38J [G 22,30,53],735 [G 80, 81J, Hannah, R. G. 477, 728 [0 163J Graham, T. E. 726 [0 98J 736 [G 124J, 743 [K 3, 4J, 744 Hannum, J. A, 455, 607, 608, 740 Grant 617, 707, 734 [G 55J [K 45, 52J, 756 [P 30, 34J, 762 [H 111J Grant, A. F. 598, 599, 720 [B 76J, [S 16J. 763 [S 60, 61, G4, 65, 67, Hannum, N. P. 652, 741 [H 155J 736 [G 106J, 752 [M 115, 116J 68, 74J, 764 [S 146J, 765 Hanratty, T. J. 528, 738 [H 33J Graven, W. M. 675, 71)6 [P 47J [S 190J. 766 [S 224J Hansen, O. A. 359, 738 [H 57J Graves, A. E. 403, 768 [T 15J Groudle, T. A. 599, 767 [S 269J Hanzlick, P. 330, 737 [H 3J Graves, G. A. 476, 736 [G 129J Grove, E. L. 606, 731 [E 32J Happe, J. A. 441, 725 [0 21J Gray, E.L. 417, 450, 733 [G14J, Groves, K. O. 705, 736 [G 121J Happel, J. 551, 739 [H 66J 734 [G 15, 26J Grumer, J. 415, 492, 536, 563, 580, Harden, D. G. 741 [H 147J Gray, F. L. 438, 772 [W 19] 719 [B 19, 24J, 734 [G 18J Hardin, M. O. 707, 739 [H 73, Gray, L. E. 417, 734 [G. 31, 32J Gruss, L. L. 445, 755 [0 3J 96J Gray, O. 663, 675, 717 [A 57] Guelich, J. 321, 750 [M 59] Hardy, L. 231, 238 Gray, P. 524, 576, 597, 609, Giinthard, H. 554, 735 [G 73J Harman, B. N. 354, 747 [L 56J 664, 674, 734 [G 23], 735 [G 83, Guenther, M. E. 636, 757 [P 77] Harmony, M. D. 339, 737 [H 13J 85, 87, 89, 99], 736 [G 111, 112, Guertin, J. P. 327, 341, 460, 727 Harnisch, H. 521, 738 [H 28J 122, 135, 136] [0 127, 128, 129, 148J. 737 Harper, E. Y. 483, 741 [H 163J Gray, P. D. 222, 238, 643 [G 1501 Harper, J. T. 289, 301, 306, 309, Gray, V. H. 479, 735 [G 74], 736 Gundzik, R. M. 301, 305, 306, 734 310, 316, 321, 768 [S 277J [G 143] [G 46J Harper, i:-l. A. 377, 739 [H 97J Green 660, 739 [H 84] Gunn,S. V. 249, 284, 689,697, 735 Harpoothian, E. 479, 741 [H 142J Green,J. 328,414, 571, 737[G 156, [G 97J Harries, O. 367 160] Gunning, H, E. 521, 736 [G 130J Harris, E. L. 447, 740 [H 125J Green, L. jr. 97,144,145,176,178, Gunther, W. H. 303, 742 [J 41J Harris, W. B. 231, 238 183, 191,202,217,309,706,736 Gupta, A. K. 555, 735 [G 67] Harrje, D. T, 364,740 [H 122] [G 107], 744 [K 41] Gustavson, J. 706, 709, 733 [G 6J Harshman, R. C. 566, 568, 585, Greene, E. A. 537, 725 [031] Guth, E. D, 549, 747 [L 47J 737 [H 19] Greene, S. A. 558, 603, 604, 658, Hart, A. B. 394, 738 [H 45J 664, 729 [D 44], 735 [G 70], 736 Haase, G. 293, 307, 315,738 [H 61J Hart, R. W. 209, 218 [G 113, G 134] Hackley, E. B. 404, 755 [0 7J Hartunian, R. A. 98 Greenfield, S. 207, 218, 360, 548, Haendler, H. M. 301, 738 [H 63] Haskins, J. F. 486, 741 [H 139J 661, 734 [G 35, 43], 735 [G 88J Haeuseler, E. 154, 177, 273, 286, Hast, D. R. 679, 738 [H 23J Gregory, O. A. 673, 684, 760 395, 738 [H 47J Hastings, G. A. 472, 483, 741 [R75] Hagen 279 [H 160J Gregory, J. W. 635, 653, 733 [G 5] Hager, K. F. 454, 740 [H 108J Haszeldine, R. N. 291, 738 Grclecki, O. J. 459, 636, 678, 681, Haggerty, W. 580, 737 [H 17], 738 [H 60] 684, 736 [G 138J, 737 [G 146J, [H 24J Hatcher, J. B. 438, 547, 738 [H 34, 774 [W 106] Hala, E. 275, 286 59J Grcnus, M. 714, 736 [G 108] Halbig, J. 412, 444, 532, 579, 738 Hatt, N. 573, 737 [H 14] Grey, J. 360, 604, 727 [0 120J, 734 [H 25J Hattori, K. 589, 740 [H 116J [G 40J Halford, F. B. 593, 740 [H 119J Hatz, D, J. 328, 412, 413, 414, 504, Gribova, E. I. 379, 734 [G 28] Hall, A. R. 597, 663, 664, 739 761 [S 9], 762 [S 10,21, 22J, 766 Grier, N. T. 475, 735 [G 75J [H 99J, 750 [M 75J [8206,207] Griesser, H. 30 Hall, D, M. 73, 98 Hauel, A. P. 598, 739 [H 101] Griffin, D. N. 114, 117, 265,266, Hall, E. N, 290, 738 [H 36J Haugh, J. F. 505, 740 [H 114J 285, 604, 735 [G 72J, 736 Hall, E. W. 461, 766 [S 226J Haurden 567, 737 [H 21J [G 105] Hall, J. G. 72, 97 Hausen 208 Griffin, J. J. 624, 745 [K 102] Hall, L, A, 297,467,740 [H 133J, Hauser, R. L. 357, 739 [H 87J, 756 Griffith, J. R. 417, 535, 580, 734 741 [H 141J [P 22J [G 16, 21J Hall, L. M. 578, 740 [H 129] Hauser, T. J. 709, 740 [H 105J Grigger, J. 0.327,347,454,733 Hall, M. 327, 761 [S 7] Hausner, H. W. 499, 741 [H 146J [G 4],736 [G 110] Haller, J. F. 521, 528, 738, [H 26, Hawkes, R. 740 [H 126] Grilly, E. R. 352, 742 [J 17] 27J, 740 [H 127J Haws, J. L. 741 [H 1471 Grisard, J. 325, 326, 733 [G 3] Hallett, No O. 468, 469, 615, 743 Hawthorne 593, 740 [H 120] Grocholskaja, N. W. 417, 757 [J 54J, 763 [S 105J Hayford, A. W. 412, 413, 716 [A 11, [P 71] Halliday, K. O. 686, 739 [H 90, 91J 15] Groennings, S. 397, 754 [N 33J Halpern, O. 638, 737 [H 10J Head, E. L. 497, 741 [H 145] 784 N amcnverzeichnis

Head, R R 754 [N 19] Hicks, B. L. 155, 177 Huber, F. 339, 342, 737 [H 7], 7G2 Heckert, W. H. 602, 604, 739 Hicks, J. A. 609, 740 [H 112] [S 12J [H 75] Hieber 738 [H 31] Huckaba, C. E. 387, 738 [H 46] Hedley, W. H. 765 [S 180] Hill, D. C. 537, 725 [C 30] Hudders, R. S. 485, 73ll [H 8G] Heidmann, 1\I.l<'. 195,217,298, Hill, D. L. 506, 725 [C 38J Huff, V. N. 538, 614, 617,621,625, 355, 513, 527, 652, 658, 739 Hill, G. R. 501, 752 [l\I 121)] G2G,G27, 628,631,G43,G44, G45, (H 81, 82], 740 [H 131], 741 Hill, 1\I. E. 610, 761 [R 126] 646, 654, 657, 659, 671, 707, 732 [H 149], 756 [P 27] Hill, W. H. 738 [H 41],740 [H 115] [F 31, 34], 734 [G 54, 57]. 735 Heidt, L. J. 37:"), 738 [H 56] Hillenbrand. L. J. GOG, 740 [H 107] l G 59. 60, 63, G4, 65]. 737 [H 11 J, Heilbronner, E. 554, 735 [G 73] Hilsenrath 7G 739 [H 71,72, 83J Heinrich, G. 738 [H 30] Hilsenrath, J. 353, 471, 738 [H 58] Hugget, C. 158, 159, 177,261,262, Heller, G. 16, 30 Hilton, A. R. 333. 737 lIi 8] 263, 285 Hellund, E. J. 17,31 Himpan, J. 19l1, 217 Hughes, A. 1\1. 525, 526, 738 Helm, R. V. 4;)1. 769 [T 50] Hinck. E. C. 657. 772 [V 38] [H 32] Helmkamp, G. F. 573, 743 (K 10] Hinckley. It. B. 362, 720 [B 53], Hughes, P. R. 490, 740 [H 130J Hendel, F. J. 706, 713, 737 [H 6J, 738 [H 44] Hummel Chern. Corp. 454, 704. 739 [H 95] Hines, W. S. 527. 547, 548, 73ll 740 [H 109] Henderson, U. V. 707, 709, 737 [H 69], 741 [H 148. 154] Humplm'Y, J. C. 19:). 217. 382, [H 12]. 739 [H 67, 68, 94], 740 Hirata, T. 737 IH Il] ()77, 738 [H 65],743 [K 25] [H 103, 104, lOti] Hiroshi-Tsnji 597, 73!J [H 100] Humphrey, N. 13. GOl, 75H [It 58J Hend"rwll. \V. P. 449, 450, 740 Hirsehfelder, J. O. 160, 177 Hunt, H. 509, 756 [P 15] [H 123.1241 Hirth, .J. P. 74, 97 Hendricks. R. C. 472,473,475.734 Hobart, H. F. 4ll1, 750 PI71, 72] Hunt, 1\1. S. 4Gl, 738 [H 53] [G 41], 736 [n 141], 738 [H 48, Hodge, H. :3:34, 737 [H 2] Hunt, W. l\l. G90, 740 [H 117] 49,50] Hoclzgen, H. J. 367, 738 [H 37J Hunter, B. J. 477, 731l [H 77] Hendrix, C. D. 659, 732 [F 34] Hopfner, A. 286 Hurd, C. O. 389, 391, 763 [S 97] H('ngsknberg, J. 275, 281; Hocrning, J. 361, 744 [K 58] Hurd. D. T. 500,6;').5, 741 [H 1M]. Hennings, F. G. 517, 677, 737 Hoffman, C. J. 338, 339, 348. 737 7G4 LX 25] [H 22] [H 1], 741 [H 150] Hurd. S. E. 4H3, 741 [H 163] Hennings, G. 615, 677, 686, 694, Hoffman, D. J. 74, 1l8, 205, 217 HllI·dcll. D. 461, 671, 738 [H 52], 730 [D 83], 739 [H 88, 89] 743 Hofland, R 98 73ll [H 93] [K 25] Hohman, J. 415, 75G [1' 7] Hurley. F. R 673, 734 [G 17] Henry, It. A. 60G. 740 [H 110] Holben, C. D. 486, 741 [151 Hnrst. e. L. 341, 740 LH 136J Herb,'rt, 1" S. G;,)l, 739 LH 7H] Holcombe, A. II. 485, 731l [H 86] Hunyitz, l\1. 761 lH 128] Herickes, .J. A. 562, 576, 577, 580, Holley, Ch. E. 497, 741 [H 144. Hutcheon GGO. 73\J lH 84] 737 LH Hi] 145] Hyde, E. K. 50U, 767 lS 252] HermancC'. C. E. 155, 156, 177 Hollml", 73ll [H 76] [I 7 J Inco 301, 304, 327,754 [N 1()] 381. 720 [B 4ti, 47. 50], 738 Hoppe. R. 345. 731l [H 70] Ingebo, R. D. 195, 217 [H 38, 39, 40]. 739 [H 98J, Horn, H. 1. 329, 737 [ll 4. 5] Ingold, K. J. 602, 747 [L .Jill 741 (H 13,3]. 7ii(; [1' 17] Horn, H. J. 4G5, 738 (H 3;3, 42] Internat. Critical Tables 350, 352, Hershey, E.-K. 772 LW 3ti] Horrwr, J. W. i)\)G.I)Ol, 739 [H 102J 508. 501l, 741 [12] Hertel. W. 5;il. i")G5, G89, G99, 738 Hon-it~, D. 567, fi68, 573, 737 lrlllselwr 660. 741 [I 41 [H G;)] [H 1:'i. 18, 20], 740 lH 121], 7ii5 In'ing, J. P. G36. 7G7 [F 77J Hertz. J. 306. 321. 486,724 [B 212], [020,2GJ Isakson, V. E. 486, 741 [15] 741 IH 13H] Houben,J. 275, 283, 286 [n' Herzberg. F. 361. 73ll [H 78] House, P. A. 328, 400, 414, 584, Isbin, H. S. 51l1, 772 24] bhaghoff, 1. 471l, 741 [13] Herzfeld, K. F. 353, 738 [H 43] 741 [H 158] Isserow, S. 56ll, 575, 585, 717 Hess, F. D. 411, 741 [H 1611 Houser, T. 706, 709, 757 [P 52] Hess. L. G. 555. 556, 73H IH 74] Housser. T. J. 178, lll0 LA 34] 1veson, G. 300, 327, 730 [E 8J, 740 Hetherington, G. 347, 348. 741 Houwink, R. 127, 152. 153, 176 [H 134], 741 [11] [H 151. 152] Howard, O. H. 301, 738 [H G4] Heuse. 464, 738 [H 51J Howell, J. R. 475, 741 [H 143] Heyde siehe unter von del' Heyde Hsieh, P. Y. 532, 740 [H 128] Jache, A. W. 333, 719 LB 9] Heymer, G. 521, 738 [H 28] Hsu, A. C. T. 356, 741 [H 138J Jack, R. 16,30 Hibbard, R. R. 5ll0, 657, 740 Hu, H. 772 [W 38] Jackson, D. R. 604, 742 [J 31J [H 118] Hu, J. D. 293, 295, 296, 297,298, Jackson, H. D. 357, 742 [J 42] Hickling, A. 521, 738 [H 29] 738 [H 62] Jackson, R. 333, 746 [L 19] N amenverzeichnis 785

Jacobs, R. B. 361, 366, 481, 482, Johnson, V. J. 470, 765 [8 173] Kaufman, J. J. 339, 744 [J( 28] 489, 742 [J 18, 24, 34], 760 Johnson, W.E. 164, 177 J(aufman. W. B. 589, 655, 724 [R 69], 771 [V 7, 11] Johnson, W. II. 460, 736 [G 132], [B 208] Jacobs, T. A. 614, 743 [J 53] 757 [P 64] J(aufman, W. F. 309, 744 [J( 41] Jacobson, J(. II. 536, 572, 581, 742 Johnson, W. R. 487, 743 [J 55] J(avall, A. J. 712, 744 [J( 64J [J 7, 8] Johnston, II. 601, 743 [J 52] Kavanagh 744 [J( 63] Jaffe, J. 273, 286 Johnston, II.·L. 293, 294. 295, 296, J(avanagh, G. M. 387, 763 [8 102] James, W. D. 537, 756 [P 13] 297,298.350,352,463,464.468, Kay, W. B. 428, 439, 440. 441. 743 Jamnow, P. A. 356, 742 [J 43] 469, 470, 615, 652, 734 [G 33], [K 18, 19, 20], 744 [J( 29]. 762 738 [II 62].742 [J 17, 21, 22, 25, JANAF Thermochem. Tables 76, [843, 51] 32]. 743 [J 54], 763 [8105], 772 98, 296, 326, 346, 353, 405, 408, J(aye, 8. 588,613, 744 [J( 47], 748 [W 29,38] 409,425,430,471,501,503,505, [L 82] Johnston, II. 8.345.441,742 [J 11, 511,554,743 [J 50] Kayser, L. T. 677, 744 [J( 56].745 29] [J( 85] Janes, 8. G. 17,31 Johnston, 8. A. 51, 65. 210. 215, Kazmirowski, II. G. 573, 743 Jarry, R. 339, 340, 341, 742 216, 217 [J( 9] [J 1] Johnston, W. II. 521, 742 [J 10] J(eefe, J. II. 400,401,402, 591. Jarry, R. J. 346, 742 [J 3] Jolly, W. L, 598, 718 [A 83] 728 [D 23], 729 [D 261, 744 Jarry, R. L. 293, 294, 303, 742 Jonas II. 290, 573, 742 [J 5. 26] [J( 37, 38] [J 27,41],762 [8 15] Jones, B. 703, 755 [0 17] Keeler, M. J. 445, 745 [J( 81] Jallbert, J. 97, 98 Jones, B. P. 16, 30 J(ehat, E. 357, 395, 396, 744 [J( 50], Jallmotte, A. 30, 53, 65, 97, 101, Jones, J. L. 550, 774 [W 100] 763 [8 90, 92, 93] 117,143,146,176,192,194,198, Jones, 1\1. M. 521, 742 [J 9] J(eller, R. C. 328, 414, 571, 737 202,206,207,208,209,210,212. Jones, P. 394, 742 [J 19] [G 160] 216,253,254.257,258,284,428, Jones, R. 1\-1. 571. 742 [J 40] J(eller, T. A. 550, 773 [W 43] 429,430.524,526,549,575,699, Jones, W. L. 743 [J 49] J(eller, W. E. 470, 742 [J 21] 719 [B 30] Jortner, J. 345, 614, 653, 678, 723 J(elley, 744 [J( 63] Jefferson. T. B. 358, 742 [J 44] [B 170], 742 [J 30] J(elley, J. II. 599, 745 [J( 106], 767 Jelinek, J. G. 414, 753 [M 178] Jost, A. 597, 742 [J 47] [8269] Jellllm, E. 578. 581, 742 [J 6] Jost, \V. 241. 284, 286 J(ellog Co., M. W. 254, 285 Jenkins, A. C. 350, 368, 369, 370, Joyner 501, 587, 742 [J 37] J(elso 677, 743 [J( 12] 371,372,373.382,742 [J 13, 14, Judge, J. F. 706, 742 [J 4] J(emp, J. D. 406, 408, 409. 733 15, 16, 35] [G 12] Jenkins, II. P. 703, 752 [M 138] Kalil, E. O. 517, 672, 684, 689, 743 J(endall 362 Jensen, A. V. 412, 503, 504, 705, [J( 26] J(endall, R. E. 738 [II 44] 727 [C 140], 742 [J 36], 743 J(amenctskaya, 8. A. 377, 744 J(ennebeck, 1\1. 530, 578, 681, 745 [J 45] [J( 30] [J( 96] Jesskowa, W. \V. 356, 742 [J 43] J(ananova, E.·Ja. 756 [P 33] J(ennedy. A. 339, 341, 342, 344, Jessup, R. 8. 299, 300, 339, 626, J(anareck, C. A. 625, 744 [J( 46] 724 [C 1, 11], 744 [K 27] 716 [A 1] J(anarek, 1. A. 358, 366, 610, 743 Kenney, R. J. 449,680,745 [J( 89, [K 7]. 744 [K 33] 98] Jet Propulsion 310, 586, 742 [J 2, J(anda, E. 294, 296, 744 [K 42] J(ent, B. M. 505, 760 [R 89] 33, 38] J(ane, J. E. 357, 717 [A 40] J(ephinger, M. L. 321, 745 [J( 100] Jewett, C. L. 480, 490, 494, 720 Kant, A. 597, 744 lJ( 66] J(erslake, W. R. 461, 729 [D 34] [B 53], 742 [J 23], 756 [P 25] J(antrowitz, A. R. 17, 31 Key, C. F. 357, 745 [J( 92], 761 Jim, E. 684,773 [W 64] J(aplan, N. 445, 447, 451, 743 [R 106] Jimenez·Barbera, J. 118. 279, 286, [J( 21] J(eyes, F. G. 387, 738 [II 46] 537. 538. 539. 540 723 [B 189, J(appl. J. J. 681, 748 [L 115] Keys, R. D. 357,477,766 [8 192] 190], 743 [J 46] J(apralova, G. A. 614, 745 [J( 101] J(hariton 380 Jinno, II. 98 J(arapetjanz, M. Ch. 275, 286 Khayat, 8. 1. 341, 741 [II 136] Joffe, J. 551, 766 [8219] Karhan. B. L. 610, 733 [F 71] Kidwell, A. 8. 448, 555, 750 John, E. C. 321, 743 [J 51] J(ariotis. A. II. 486, 770 [T 69] [M 73] John, R. R. 16,30 Karkarschwili, M. U. 529, 734 Kiefer, T. F. 357, 477, 766 [8 192] Johns, H. E. 465, 742 [J 20] [G 24] Kigeli, R. A. 504, 766 [8 228] Johnson 528, 717 [A 28] J(arman siehe unter von Karman Killian, W. R. 490, 744 rK 49],756 Johnson, E. J. 683. 751 [M 82] Kasakowa, E. B. 504, 766 [8 228] [P 39] Johnson, F. A. 339, 343, 344, 724 Kash, 8. W. 9, 30 Kilner, 8. B. 222, 238, 635, 636, [C 11],726 [C 58]. 742lJ 12],743 J(astner, M. E. 619, 620, 735 678, 743 [K 2] [J 48] [G 61] Kilpatrick, M. 255, 257, 259, 285, Johnson, J. II. 347, 758 [R 11],759 J(atz, f-l. 550, 732 [F 29] 673, 690, 702, 745 [J( 78] [R 62] J(auffman, G. 537, 756 [P 13] J(ilpatrick, M. L. 606. 740 [II 107] Johnson, K D. 232,238, 500, 742 J(aufman, J. 502, 504, 744 [K 72]. Kimball, A. R. 306, 744lJ( 31] [J 39] 745 [J( 74] J(indsvater. II. 442, 749 [M 11] Johnson, P. G. 30 J(aufman, J. G. 357, 717 [A 40], King, C. II. 461, 725 [C 52], 744 Johnson, 8. M. 98 745 [K 90] [J( 67]

Dadieu· Damm ·Schm idt, Raketentreibstoll'e 50 786 Namenverzeichnis

King, M. 384,751 [M 110] Kovitz, A. A. 525, 546, 763 [8 77J Lamberti 502, 505, 748 [L 84J Kinney, G. R. 319, 650, 651, 677, Kozunenko, O. J. 377, 774 [Y 2J Lambrecht, J. 702, 747 [L 61J 678, 743 [K 25], 759 [R 56], 765 Krackow, E. H. 404, 502, 504, 505, Lammeck, J. H. 382, 588, 748 [S 157], 768 [T 6] 744 [K 70J, 756 [P 21J [L 82, 91J Kinney, L. C. 368, 768 [T 11] Kramer, L. 655, 656, 752 [;VI 136J Landau, R. 296,301, 303, 317, 746 Kinney, L. W. 349, 725 [C 45] Kramer, P. 202, 203, 204, 217 [L 37,40,41,42,43] Kinsley, E. J. 445, 748 [L 92] Kramer, P. A. 684, 745 [K 86] Landri, V. R. 375, 738 [H 56J Kirk, B. S. 353,471, 750 [M 38, 79, Kramers, H. 415, 743 [K 8J Landrum, R. G. 334, 730 [D 88J 80] Krascella, N. L. 471, 745 [K 99J Landshoff, R. K. 1\1. 31 Kirk, R. E. 290, 745 [K 103J Krasinsky, J. B. 541, 771 [V 25] Lang, K. 5il9, 748 [L 86J Kirsh, D. P. 370, 772 [W 20] Krebs, C. H. 652, 745 [K 94] Lange, N. A. 408 746 [L 12J Kirshenbaum, A. D. 335, 336, 337, Krebs, E. 264, 285, 286 Langemeyer, A. 182, 191 338, 345, 374, 613, 661, 733 Krebs, H. J. 310. 745 [K 105] Lapin, A. 481, 748 [L 117J [G 8], 734 [G 53J, 743 [K 3, 4, 5J, Kretschmar, G. G. 430, 451, 523, Laporte Chemicals Ltd. 386, 387, 744 [K 45, 52J, 745 [K 104], 762 525, 743 [K 17J, 744 [K 32, 3il8,389,390,392,393,395,396, [S 16J, 765 [S 160J 40J 397,402, 591, 746 [L 25, 28] Kirtchik, H. 333, 743 [K 6] Krieger, R. L. 329, 737 [G 157J Laquer, H. L. 480, 486, 487, 747 Kishore, K. 689, 702, 761 [R 120, Krop, S. 450, 537, 564, 743 [K 23], [L 50, 51J 121] 744 [K 51J, 749 [M 32] LarrazabaI. J. IVI. S. 597, 769 [T 46J Kistiakowsky, G. B. 686, 744 Kropschot, R. H. 479, 744 [K 48, Larson, O. E. 436, 549, 746 [L 18], [K 59] 57J 747 [L 47] Kit, B. 296,351,407,429,430,431, Kriille, G. 16, 30 Larsen, P. S. 361, 485, 747 [L 57] 435,457,464,469,526,564,606, Krull, H. G. 203. 217 Larson, R. L. 1)99, 747 [L 73] 698, 743 [K 14] Kruse, H. W. 537, 578, 586, 723 Klager, K. 139, 153, 156, 176, 573, [13 165J, 727 [C 119],740 [H 129], Lauer, O. 267, 268, 269, 273, 743 [K lOJ 752 [M 141], 755 [0 25J, 766 285 Klein, E. 195,217 [8231] Laughrey, J. A. 674, 721 [B 96, Klemenc, A. 436, 437, 743 [K 16] Kruska, E. 402, 593, 670, 673, 744 98) Kline, J. F. 487, 735 [G 77] [K 34,35] Laval 58 Kling, R. 193, 217 Krynitzky, J. A. 537, 745 [K 83J Lavrov, F. A. 551, 68S, 747 [I. 46] Klingelhofer, W. C. 514, 743 Kubala, T. A. 536, 563, 580, 734 Lawler, A. E. 307, 309. 748 [L 116] [K 24] [G 18] LawiBr, E. A. 723 [B 166J Klusmann, E. B. 705, 774 [W 86] Kubaschewski, O. 387, 744 [K 39] Lawler, J. H. L. 651, 747 [L 52] Knight, O. A. 568, 569, 743 [K 13] Kuby, W. C. 98, 617, 745 [K 97] Lawrence, E. A. 607, 747 [I, 74) Knight, W. 442, 749 [;Vll1J Kuehl, D. K. 499, 723 [B 186J Lawrence, E. K. 609, 747 [L 79J Knight, W. P. 609, 718 [A 86],745 Kuhn, L. P. 609, 744 [K 68] Lawrence, R. W. 60H, 618, 705, 747 [K 801, 747 [L 76J Kuhn, S. J. 327, 755 [0 4J [L 76J, 764 [8 148], 766 [8230J Knoll, E. F. 445, 745 [K 81J Kuhns, L. J. 502, 504, 505, 744 Lawson, L. 537, 725 [C 31J Knoll, R. H. 479, 765 [S 158J [K 69, 73J Lawton, E. A. 343, 588, 748 [L 83, Kobozev, N. T. 385, 763 [S 99J Kula, E. B. 718 [A 95J 1101 Koch, J. H. 430, 432, 598, 601, 743 Kuley, C. J. 355, 745 [K 91] Lawver, B. R. 679, 681, 748 [L 114, [K 15J Kunkel, 347, 743 [K 11J 115, 121 J Koch, S. D. 551, 744 [K 43] Kunkle, A. C. 333, 719 [B 9] Lea, R. H. 359, 480, 748 [L 10H] Kocher, R. M. 745 [K 93] Kunugi, ;VI. 98 Lebedev, V. P. 350, 378, 731 [E 19J. Kolle, D. E. 653, 671, 672,684, 744 Kunzler, J. E. 30 763 [8 70J [K 61, 62, 65], 745 [K 87, 88] Kurz, P. F. 654, 744 [K 53,54, 55J Lebedaw, M. Je. 358, 746 [L 22J Koelle, H. H. 117, 128, 176, 192, Kushida, R. 72, 97 Leboeuf, R. 217 202,203,206,210,216,324,353, Kutateladze 355 Leece, J. V. 522, 524, 718 [A 85] 429,561,562,568,569, 592, 743 Kutina, F. J. 770 [T 90J Leduc, A. 408, 746 [L 13J [K 1] Kuwada, D. M. 529, 745 [K 84] Lee, D. H. 595, 598, 601, 680, 728 Koenen, H. 154, 177, 273, 286 Kwasnik, W. 291, 293, 745 [K 79] [C 154], 747 [L 70,71, 72J Koester, R. 500, 586, 587, 590, 744 Kwawer, A. J. 624, 745 [K 102] Lee, J. B. 189, 191, 228, 229, 238 [K 71],745 [K 75.76, 77J 500, 617, 734 [G 56] Kohnen, H. 521, 772 [W 14] La Belle 334, 745 [L 1] Lee, J. C. 597, 664, 735 [G 83,85, Kohlrausch, F. 275, 283, 284, 286 Lacaze, A. 471, 748 [L 99] 87J, 736 [G 122J Kolfenbach, J. J. 551, 744 [K 44] Ladanyi, D. J. 677, 686, 737 [H 22], Lee, Suh Yong 706,752 [M 121J Kooiker, R. H. 417, 743 [K 22] 751 [M 85] Lee, W. B. 654, 748 [L 113, 120] Kooy, J. I\I. J. 702, 744 [K 60] Ladanyi, D. L. 248, 249, 254, 284, Leech, H. R. 291, 2\l3. 746 [I, 7, Kopituk, R. C. 357, 401, 744 285, 609, 673, 689, 691, 696, 698, 35J [K 36J 699, 702, 703, 747 [L 59, 60,63, Lehrman, A. 451, 725 [C 29] Koshar, M. M. 361, 744 [K 58] 64, 67J, 748 [L 87] Lemaitrc, M. P. 97, 98 Kosky, P. G. 354, 747 [L 56] Ladd, J. W. 360, 492, 746 [L 33] Lemnons, J. F. 497, 741 [H 144] Kosstrjukow, W. l\'. 745 [K 95] La Lande, W. A. 345, 745 [L 2] Lemon, J. T. 420, 422, 746 [L 6] Kosting, P. R. 445, 745 [K 82] Lalanne, F. 529, 746 [L 16] Lenehan 451, 746 [L 10] Kosvic, T. C. 681, 724 [B 202] Lalli, G. 502, 572, 581, 748 [L 88] Lenji, L. 451, 452, 607, 752 [M 124J N amen verzeiehnis 787

Lenoir, J. M. 144, 176 Lockheed 133, 134, 135, 471, 748 Maman, A. 194, 217 Leonard, A. S. 617, 707, 747 [L 48] [L 118] Mandell, B. 652, 750 [M 69J Leopold, L. C. 319, 759 [R 56] Lodwig, R. M. 178, 181, 185, 186, Manheimer, Y. 754 [N 23J Lepie, A. 249, 250, 252, 254, 259, 190, 638, 706. 709, 746 [L 3], Manley, T. C. 368, 383. 751 260,285,560,691,695,698,699, 757 [P 52] [M 111J 747 [L 62],766 [S 215] L6b, H. 21, 22, 31 Mann, D. B. 466, 485, 728 [C 150J, Leslie, R. S. E. 72, 98 Logan, J. L. 374, 748 [L 90] 730 [D 79J Lester, J. M. 475, 483, 726 [C 73] Logan, S. E. 479, 748 [L 98] Mann, D. E. 613,626,723 [B 175], Leupold, M. 652, 748 [L 96] Long 502, 505, 748 [L 85] 750 [M 65,66] Le Valley, W. H. 746 [L 32] Long, S. A. 445, 748 [L 92] Mannion, J. P. 512, 749 [M 19J Levine, N. B. 328, 414, 571, 737 Long, W.S. 207,218 Manson, L. 753 [M 163] [G 156, 160] Lorenc, S. A. 74, 98, 206, 217 Mantell, R. M. 598, 757 [P 761 Levine, O. 658, 735 [G 79] Lorenzo, C. F. 746 [L 39] Marano, D. 357, 753 [~1181] Levine, R. S. 209, 212, 213, 214, Louis, P. 333, 746 [L 19] Marantz, S. 343, 716 LA 2] 217 Lossing, F. P. 602, 747 [L 49] Marcus, J. P. 414, 753 [M 178] Levine, S. D. 593, 720 [B 58] Love 593, 748 [L 95] Margrave, J. L. 346, 638, 746 Levinsky 502, 505, 748 [L 85] Lovell, J. C. 659, 747 [L 53, 54] [L 3],749 [M 4J, 754 [N 4] Levitt 471,759 [R 61] Lovett, J. R. 610, 770 [T 89] Mark, H. 127, 176 Levitt, B. P. 676, 717 [A 22] Lovingham, J .•J. 643, 748 [L 108] Markels, M. 492, 536, 580, U81. Levoe, C. E. 445, 746 [L 17] Lowry, T. M. 420, 422, 746 [L 6] 732 [F 38], 737 [H 17]. 752 Levy, J. B. 115, 117, 166, 174, 176. Lubick, R. J. 615, 757 [P 92] [M 148J 344,457,458,459,476,609,610. Lucien, H. 577, 748 [L 112] Marsch, C. J. 551, 739 [H 66] 614, 718 [A 76, 77], 747 [L 75, Lucien, H. W. 528, 746 [L 14, 15], Marse), J. 655, 656, 752 [M 136J 78,80],748 [L 101, 107, 111] 748 [L 94] Marsh, F. D. 347, 749 [M 3] Levy, R. H. 9, 30 Ludtke, P. R. 359, 761 [R 103] Marshall, M. D. 460, 753 [M 1701 Lewis, B. 65, 98, 590, 657, 748 Ludwig, J. R. 503, 722 [B 128] Marshall, S. B. 757 [P 60] [L 106], 762 [S 40] Luft, F. 339, 758 [R 1] l\IarteJ, C. R. 490, 732 [F 36] Lewis, G. D. 610, 747 [L 77] Lum, A. F. 730 [D 66] Martin, C. H. 539, 753 [M 182] Lewis, G. J. 485, 748 [L 93] Luperi, M. 35, 65, 643, 748 [L 108], Martin, K. B. 479, 753 [M 164] Lewis, G. L. 351, 370, 746 [L 20] 767 [S 256] Martin, M. 550, 753 [M 150J Lewis, J. D. 747 [L 69] Lutz, O. 174, 175, 177, 178, 190, Martindale, D. L. 488, 736 [G 142J Lewis, J. P. 473, 771 [V 12] 248,284,689.697,702,711,747 Martindill, G. H. 480, 492, 493, Lewis, L. L. 753 [M 170] [L 61, 65, 66J 597,733 [F 47].775 [Z 3] Lewis, R. 298, 746 [L. 36] Lynn, S. 444, 746 [L 8,9, 11J Martinez, F. 385, 750 [M 44J Lewis, T. J. 394, 398, 746 [I. 26, Lyon, D. N. 354, 747 [L 56] Martinez, J. S. 13, 30, 599, 678, 44] Lysyj, 1. 300, 747 [L 68] 731 [E 10], 752 [M 115, 116J Lezberg 657,748 [L 81] Marx, P. C. 598, 751 [M 114J Lezberg, E. A. 98 ~Iac Glashan, W. F. 414, 770 Marxman, G. 185, 191 Liberto, R. R. 411, 414, 415, 529, [T 83] Marxman, G. A. 706, 752 [M 119J 584, 681, 746 [L 4, 5] Machu, W. 394, 7[SO [M 39] Mascolo 513, 749 [1\135] Liebenberg, D. H. 483, 748 [L 100] Macinko, J. 462, 750 [M 52] 1Iasi, J. J<'. 501, 502, 504, 589, 736 Lieber, E. 537, 723 [B 165] Mack, E. 602, 604, 739 [H 75] [G 116J, 744 [K 69] Liebermann, P. 359, 746 [L 34] Mackey, D. R. 589, 752 [M 135] Mason, C. M. 459, 594, 606, 686, Liebert, C. H. 663, 747 [L 55] Mac Millan, J. A. 394, 528, 749 751 [M 86]. 752 [M 118J. 775 Liebman, 1. 492, 757 [P 74] [M 21] [Z 10, l1J Liepmann, H. W. 351,353,746 Macomber. H. 16, 30 Mason, D. M. 409, 429, 433, 434, [L 21] Mac Wood, G. E. 757 [P 66] 435,436,437,438,439,441,442. Lijewski, A. 401, 750 [M 41] ~Iaddocks, F. E. 478, 479, 480, 444,445,446,523,553,554.561, Lindenbaum, A. 231, 238 492, 493, 725 [C 47, 48], 726 693. 719 [B 35], 731 [E 16], Lindley, B. K. 489, 733 [F 70] [C 70] 746 [L 8J. 749 [M 5, 12, 13, 16. Lindquist, C. R. 478, 479, 747 l\1aecker, H. 16, 18, 30, :H 24, 25, 26, 27J, 750 [M 60J, 7.51 [L 58] Maham, J. E. 560, 765 [S 186] [1191, 92J, 758 [R 23, 24J, 7:)9 Line, L. E. 739 [H 68] Mahieux, F. 374, 752 [M 144] [R 32, 36, 39J Lingnau, E. 301, 303, 746 [L 38] Maim, J. G. 345, 726 [C 60] Mason, R. W. 301, 764 [S 124J Little, A. D. 356, 360, 361, 394, 1Iajor, C. J. 500, 752 [M 130] Massonne, .J. 339, 753 [M 159J 478, 480, 494, 746 [I. 23, 24. Makovsky, A. 451, 452, 607, 751 Masters, A. 1. 618, 707, 739 [H 73, 27, 29, 30, 31], 748 [L 89, 119] [M 88],752 [M 124] 96J, 753 [M 171, 175J Little, R. 333, 728 [D 3] Malina, F. J. 686, 7.51 [M 89] Matsch. L. C. 461, 480, 750 Liu,1. D. 390, 394, 734 [G 37, 38] Mallory, H. D. 606, 753 [M 157J [M50] Lo, R. E. 182, 187, 191, 231, 238, Maim, J. G. 345, 726 [C 62J, 750 Matheson, J. C. 618, 753 [M 183J 278, 286, 291, 495, 496, 517, [M 64J, 753 [M 160J Matheson, M. S. 345, 773 [W 45J 518, 519, 707, 730 [D 74], 746 Malone, H. E. 443. 444, 530, 562, Mathewson 480, 772 [W 32] [L 45], 748 [L 97, 102, 103, 104, 577, 583, 749 [M 8, 9, 10, 15J, Mathieu 592, 750 [M 40] 105] 752 [M 146J, 753 [M 155J Matos, S. R. 683, 751 [M 82] Lochte, H. L. 719 [B 29] Maloney, C. J. 555. 750 [M 73J Matthews, G. B. 604,727 [C 120]

Dadieu· Darnrn·Schrnidt. Raketentreibstoffc 51 788 Namenverzeichnis

Maxey, G. C. 581, 772 [W 11] McNerney, C. F. 733 [F 51] 748 [L 87], 750 [M 36, 37,76], May, J. R. 272, 286 McQueen, ll. S. 477, 774 [W 91] 751 [M 87,93,94,95,96,99] Maya, W. 340, 750 [M 62] McReynolds, L. S. 483, 723 [B 183] Miller, R. R. 501, 503, 506, 766 Maybee, D. 599, 667 [S 270] McWilliams, P. 475, 759 [R 57] [S 203,209] Mayer, E. 300, 333, 341, 731 Mead, G. A. 115, 117, 606, 752 Miller, W. S. 521, 749 [M 18], [E 35] [M 117] 753 [M 166] Mayer, L. 321, 750 [M 59] Meckert 401,750 [M 43] Miller, W. T. 300, 750 (M 55] McAdams, A. J. 450, 749 [M 32] Medard, L. 395, 606, 750 [M 46], Mill hiser, D. R. 361, 717 [A 56] McAlevy, R. F. III, 155, 156, 177, 752 [M 126] Milligan, D. E. 345, 750 [M 63] 706, 752 [M 121] Meehan 603, 750 [M 68] Mills, I. :tVt 502, 766 [S 210] McBride 749 [M 7] Meldau, R. 267, 285 Minkin, H. L. 491, 750 [M 71, McBride, B. J. 650, 735 [G 78] Melville, J. C. 577, 752 [M 155] 72] McBride, R. H. 314, 750 [M 58] Menard, J. 477, 750 [M 51] Mironer, A. 16, 30 McBride, W. R. 729 [D 45], 752 Mendes, M. A. T. 395, 396, 763 Mittler, S. 384, 751 [M 110] [M 140, 141] [S 90,93] Mitz, M. A. 749 [M 6] McCafferty, J. 681, 752 [M 177] Menzel, W. 331, 333, 334, 347, Moberg, M. 442, 749 [M 11] McCamy, C. S. 366, 750 [M 47] 758 [R 5, 6, 8] Moberly, W. H. 706, 709, 751 McCarthy 501, 587, 773 [W 79] Meraz, D. 449, 752 [M 145] [M 106], 757 [P 52] McCarthy, J. R. 474, 513, 750 Merrett, D. J. 494, 773 [W 59] Moedt, P. C. 654, 736 [G 137] [M 61], 753 [M 174] Merrill, H. K. 479, 643, 750 [M 78], Moehrbach, O. K. 618, 753 McCarty, L. V. 502, 731 [E 34], 767 [S 256] [M 176] 752 [M 133] Merrington, A. C. 747 [L 69] Moffat, W. H. 706, 751 [M 105] McCarty, R. D. 297, 740 [H 133] Merritt, F. L. 616, 730 [D 81] Mohr, C. M. 364, 759 [R 48] McClure, F. T. 209, 218 Mertens, J. 613, 686, 731 [E 26], Mohr, P. H. 527, 528, 717 [A 29] McCormick, J. C. 391, 393, 401, 751 [M 83, 84] Momenthy, A. M. 360,486,753 593, 669, 729 [D 56], 750 [M 41, Messina, J. 584, 753 [M 154] [M 158] 42] Metal Hydrides Inc. 506, 507, 752 Moore, F. M. 513, 759 [R 43] McCoskey, R. E. 732 [F 22] [M 139] Moore, G. E. 710,751 [M 107, 108, McCroskey, J. G. 681, 750 [M 81] Metz, F. I. 333, 752 [:\1137] 109] McCullough, F. 703, 752 [M 138] Metz, T. R. 412, 531, 741 Moore, R. L. 533, 749 [M 22] McCullough, I. P. 451, 452, 752 [ll 157] Moore, R. W. 487, 750 [M 70] [M 125] Metzer, T. H. 414, 753 [M 179] Moorman, D. W. 414, 681, 754 McCurdy, G. L. 451, 749 [M 31] Metzler, C. V. 709, 751 [M 106] [N 37] McDermott, C. E. 681, 753 [M 177] Meyer, K. H. 127,176 Morrell, G. 686, 690, 739 [H 88], McDonald 521,749 [M 20] Meyer, R. E. 573, 758 [R 16] 750 [M 74], 751 [M 85, 98] McDonald, C. 503, 504, 752 [M 128, Meyers, C. H. 508, 725 [C 34] Morrell, J. C. 687, 753 [M 172] 132] Michalek, G. A. 528, 719 [B 31] Morrey, J. R. 501, 752 [M 129] McDonald, G. E. 588, 735 [G 68], Michel, K. W. 597, 751 [M 113] Morrissey, J. E. 30 752 [M 134] Mickle, E. A. 6, 8, 30 Morrison, J. D. 300, 720 [B 74] McDonald, R. S. 502, 504, 752 Middleton, R. L. 479, 753 [M 168] Morrow, S. 737 [H 9] [M 133] Miesse, C. C. 195, 217 Morrow, S. I. 339, 749 [M 1, 2] McDonough, J. M. 369, 720 [B 43] Mignotte, P. 582, 583, 584, 756 Mortenson, L. N. 360, 415, 491, McGonigle, T. J. 676, 760 [R 77] [P 35, 36, 37] 681, 749 [M 17], 750 [M 49] McGrew, J. L. 479, 750 [M 77] Mikesell, R. P. 357, 477, 761 Moshier, R. W. 563, 751 [M 100] McIntosh, G. E. 481, 750 [M 53] [R 102] Mosier, S. A. 618, 753 [M 176] McIntyre, R. W. 72, 73, 97, 98 Mikhailov, B. M. 500, 501, 752 Mottram, A. W. T. 461, 653, 750 McKannan, E. C. 479, 753 [M 131] [M48] [M 169] Milek, J. T. 753 [M 149] Moulton, J. F. 366, 752 [M 143] McKee, H. C. 411, 753 [M 180] Miles, F. D. 772 [W 18] Mouraour, H. 142, 176, 261, 285 McKennis, H. 537, 570, 749 [M 33, Mill, T. 610, 761 [R 126] Moutet, A. 178, 179, 182, 183, 184, 34] Millan, G. 597, 751 [M 112] 185, 189, 190, 191, 223, 228, McKeown, A. B. 437, 749 [M 28, Millaway, E. E. 304, 750 [M 57] 229,238,248,254,258,259.284, 29,30] Miller, D. E. 464, 735 [G 90] 285,450,499,699,706,711,712, McKinley, C. 355, 356, 741 [ll 138], Miller, G. H. 25, 31 713, 722, [B 122, 144], 723 750 [M 45] Miller, H. C. 293, 294, 327, 339, [B 185],751 [M 97,101,102,103, McKnight, W. E. 661, 662, 765 340, 341, 347, 733 [G 4], 742 104],752 [M 120], 753 [M 173] [S 165] [J 1, 27] Moutet, H. 229, 238, 691, 699, 701. McLaren, R. O. 347, 348, 716 Miller, P. C. 357,477, 753 [M 161] 712, 713, 751 [M 101, 102, 103, [A 8] Miller, P. D. 304, 731 [E 23], 742 104], 752 [M 122], 753 [M 173], McMaho, H. O. 511, 762 [S 49] [J 42] 765 [S 176] McMahon, W. A. 411, 597, 744 Miller, R. N. 478, 753 [M 167] Moyle, M. P. 458, 752 [M 147] [K 66], 753.[M 180] Miller, R. O. 248, 249, 254, 284, Mueller, K. H. 602, 606, 607, 750 McMullen, E. T. 638, 679, 768 285,367,378,379,382,383,563, [M 67], 752 [M 123, 127] [S 281, 290] 666,673,685,694,695,696,699, Muller, W. 702, 747 [L 61] McNamee, J. K. 450, 734 [G 15] 700, 702, 703, 705, 747 (L 60], Mugnier, D. 477, 753 [M 165] N amen verzeichnis 789

Mullen, L. O. 489, 771 [V 11] Newkirk, A. E. 754 [N 26] Oniak, T. P. 588, 755 [023] Muller, G. M. 601, 731 [E 31] Newns, G. R. 521, 738 [H 29] Opalovskii, A. A. 326, 761 [S 6] Mullins, J. C. 353, 471, 750 [M 38, Newton, ,J. 3 Ordahl, D. D. 706, 755 [0 21, 79,80] Newton, P. R. 300, 747 [L 68J 29J ::\1unjal, N. L. 699, 702, 760 [R 82], Nicholaisen, B. H. 521, 754 [N 6, Ordin, P. ::\1. 487,538,616,617,618, 761 [R 119, 120] 7J 623, 624, 629, 636, 654, 671, 755 Munson, S. B. 602, 605, 757 [P 55] Nicholson, A. J. C. 754 [N 22] [0 1, 10, 14, 15], 760 [R 65, 73, Muraca, R. F. 332, 444, 445, 549, Nickel, Co. 754 [N 16] 83] 554, 749 [M 14, 23J, 751 PI 90], Nieciecki siehe unter von Nieciecki Orlik, C. A. 609, 766 [S 196] 753 [:\1151, 152, 156]. 774 Niendorf, 1.. R. 478, 479, 483, 747 Orr, J. A. 238 [W 109] [L 58],754 [N 31J Orr, J. W. 310, 755 [032] Muraszew, A. 195,217 Nilson, E. N. 98 Orysh, M. S. 445, 755 [0 3J Murphy, D. W. 362, 479, 750 Nishibayashi, 1\1. 366, 758 [P 97] Osborg, H. 755 [0 20, 26] [1\1 78],753 [::\1162J Noeggerath 178 Osborn, G. 703, 755 [0 17] Murphy, W. J. 374, 767 [S 263] Noel, 1\1. B. 458, 511, 512, 527, 720 Osmon, R. U. 709, 755 [0 31] Murray, R. C. 597, 663, 664, 750 [B 76], 754 [N 9, 171 Othmer, D. F. 290, 745 [K 103J [M 75] Noichl, O. J. 483, 754 [N 31] Otto 464, 738 [H 51 J Murray, R. L. 291, 750 [::\154] Noll, P. B. 589, 754 [N 27J Otto, E. W. 615, 755 [0 12, 13] Musgrave, W. K. R. 323. 752 Noonan, E. C. 273, 286, 609, 737 Overall, R. E. 202, 217 [M 142] [1. 79] Overstreet, R. 508, 511, 755 [06] Myers, R. J. 339, 737 [H 13] Nored, D. 1.. 624, 754 [N 35J Myers, W. R. 301, 304, 750 [M 56] North American Aviation 359, 618, Pace, E. L. 339, 340, 341, 755 Myskiewicz, T. "'1. 681, 754 [N 5] 754 [N 8, 18, 29J [P 1], 756 [P 14] Nosova, V. V. 299, 754 [N 28] Paivanas, J. A. 479, 757 [P 84J NACA 588, 619, 620 Novotny, R. 199,217 Palmer, E. D. 773 [W 78] Nachbar, W. 164, 166, 169, 170, Novotny, R. J. 663. 754 [N 20] Panell, C. E. 567, 758 [P 89] 177 Nudelman, C. 378, 725 [C 35] Panelli, G. C. 706, 774 [W 95] Naehbaur, E. 300, 333, 339, 341, Nudo, A. 411, 727 [C 146] Pankratov, A. V. 339, 341, 375, 730 [E 7], 731 [E 27,35] Nunnely, J. R. 397, 759 [R 46] 380,720 [B 42], 756 [P 6, 33, 46] Nadaud, L. 166, 170, 177 Nyberg, D. G. 758 [P 96J Pannetier, G. 582, 583, 584, 597, Nadler, M. 532, 728 [D 15J Nye, H. H. 414, 681, 754 [N 37J Nagai, C. K. 647, 754 [N 34] 756 [P 35, 36, 37J, 757 [P 53] Nagarajan, G. 333, 754 [N 3] Oberland, C. 505, 757 [P 70J Panosian, J. O. 758 [P 91] Nahmani, G. 754 [N 23] Oberst, F. W. 404, 537, 725 [C 31J, Paribok, W.P. 417, 757 [P71] Napier & Son 592,754 [N 12] 755 [0 7] Pari don, L. J. 757 [P 66J NASA 310,328,383,414,479,480, Oberstone, J. 478, 681, 755 [0 30J Park, R. P. 505, 733 [F 52J 504, 533, 572, 754 [N 32, 36J Oberth, H. 5 Parker, W. G. 461, 597, 654, 674, Nash, L. K. 301, 754 [N 14J Odinzow, W. A. 705, 755 [027] 685, 717 [A 61], 756 [P 24, 44, Nasiak, 1.. D. 681, 754 [N 5] O'Donnell, P.1\1. 301, 303, 478, 45], 757 [P 54J National Bureau of Standards 76, 755 [09] Parlange, J.-Y. 98 326,511,754 [N 2, 10J Oer, C. 267, 285 Parr, R. G. 161, 164, 177 NATO Vorschriften 146 Offenbach, J. A. 153, 177 Parry 500, 757 [P 63J Neal, A. E. 490, 754 [N 30] Ogimachi, N. 755 [0 25] Parsons, J. W. 686, 751 [M 89J Neat, W. 670, 754 [N 11J O'Hanlon, T. W. 472, 755 [018] Partel 674, 758 [P 94J Neat, W. N. 593. 740 [H 119] Ohrdahl, D. D. 182, 187, 191 Pass,1. 659, 757 [P 58J Neehaev, Yu. 1. 754 [N 21J Oikenus, A. H. 506, 537, 725 Pastuhov, A. 756 [P 251 Needham, D. P. 609, 740 [H 112J, [C 30, 38J Pattison, J. N. 528, 738 [H 33] 754 [N 24] Oja, P. D. 567, 601, 743 [J 52J, Patton. F.::\L 417, 450, 734 [G 26, Neff, J. 332, 774 [W 109] 758 [P 89J 31,32] Nein, M. E. 360, 487, 754 [N 19, OIah, G. A. 327, 403, 755 [0 4, Pavlath, A. E. 327, 341, 460, 724 38J, 770 [T 78] 24] [C 7], 727 [C 1481, 737 [G1501 Nekrasov, 1.. 1. 385, 763 [S 99J Olin ::\Iathieson 503, 568, 569, 572, Pearce, D. G. 494, 773 [W 59] Nelsen, :b'.:\1. 397, 754 [N 33J 755 [05, 22J Pearl, C. E. 589, 727 l C' 109J Nerad, A. J. 500, 655, 754 [N 25] Oliver, G. 325, 326, 733 [G 3J Pearson, J. B. 495. 771 lV 34] Nespital, W. 717 [A 26J Olivier, J. R. 483, 729 [D 63J, 755 Pease, R. N. 65, 98. 654, 662, 721 Netheler& Hintz 272,286 [08J [B 86], i73 [W 56J Neugebauer, C. 346, 753 [N 4] Olsen, R. E. 460, 755 [0 28] Peck, i\L V. 178, 181, 185, 186, Neumann, W. 347, 758 [R 8] Olsen. W. A. 491. 75.5 [0 19] 190. 706, 709, 740 [H 105 J, 757 Neumark. H. R. 291, 293, 310, 324, Obon, E. C. 529, 570, 755 [P 52J 754 [N 1, 13, 15J [02J Peckham, H. M. 357, 756 [P 22] Neville, R. G. 338, 339, 348, 737 Olson, W. T. 617, 654, 655, 657, Pedersen, C. ,J. 609, 756 [P 50J [H 1], 741 [H 150] 755 [0 11, 16J Pedler, A. E. 757 [P 60J Nevins, C. D. 477, 486, 489, 728 O'Malley, R. F. 340, 764 [S 144J Peenemiinde (Archiv) 757 [P 59] [C 163J, 767 [S 244J ONERA 186, 254 Penfold, A. S. 17,31 Nevitt, T. D. 331, 730 [D 64J O'Neal, C. 409, 724 [C 12] Penneman, R. A. 528, 756 [P 11]

Dadieu-Damm-Schmidt, Raketentreibstoffe 52 790 Namenverzeichnis

Penner, S. S. 65, 73, 97, 117, 160, Plurien, R. 724 [B 205] Purgalis, P. 638 ,768 [S 281] 164, 177, 185, 191, 196, 198, Poensgen, R. 286 Putt, J. W. 592, 758 [P 90J 217, 241, 245, 284, 594, 717 Poiseuille 279 [A 62] Pokatilo, N. A. 551, 688, 747 Rabideau, S. W. 497, 741 [H 145] Pennsalt 345, 346, 347, 755 [P 2, 3], [L 46J Radell, J. 760 [R 88] 757 [P 51] Polak, R. J. 505, 757 [P 70] Rae, W. N. 275, 286 Penzias, G. J. 681, 758 [P 88] Poling, E. L. 654, 756 [P 43], 766 Ragozin, N. A. 542, 543, 760 Peregud, E. A. 333, 756 [P 5] [S 213] [R 64] Pergiel, F. Y.757 [P 64] Pollard, F. H. 757 [P 60J Rains, W. A. 187, 191, 706, 755 Perkins, C. K. 491, 757 [P 82] Pollond, R. T. 657, 728 [C 152] [029] Perkins, H. 335, 338, 665,666,758 Pondy, P. R. 502, 504, 757 [P 65] Raleigh, C. W. 402, 578, 744 [P 98, R 10] Poole, D. R. 327, 675, 756 [P 47], [K 38J, 760 [R 98] Perkins, P. J. 479, 486, 757 [P 80, 758 [P 96] Randall, R. 359, 489, 761 [R 105] 85] Pope, A. H. 755 [020, 26] Randolph, C. L. 573, 758 [R 16] Perkins, W. E. 486, 756 [P 38] Pope, D. H. 490, 756 [P 39] Randolph, W. O. 362, 770 [T 73] Perl, A. R. 494, 775 [Y 11] Poplin, G. 707, 740 [H 104, 106J Rannie, W. D. 178, 185, 190, 706, Periee, H. E. 492 678, 756 [P 9], Porter, R. N. 412, 531, 679, 741 722 [B 120J 757 [P 74], 758 [P 100] [H 157J, 758 [P 99J, 770 [T 81] Rao, E. V. 348, 756 [P 16J Perrin, J. R. 395, 767 [S 241] Porter, R. W. 324, 756 [P 10J Rao, G. V. R. 202, 203, 204, 217 Perroud, P. 472, 757 [P 83] Potter 76 Rapp, L. R. 222, 238, 248, 284, Perry, D. D. 339, 749 [M 1], 758 Potter, J. A. 358, 757 [P 81J 560, 567, 635, 636, 678, 690, [P 87] Potter, R. L. 513, 613, 683, 686, 691, 700, 701, 703, 743 [K 2], Pesante, R. E. 366, 758 [P 97] 687, 731 [E 26J, 751 [M 83, 84J, 760 [R 80, 81], 765 [S 188] Peschka, W. 7, 8, 9, 25, 30, 31 756 [P 48J, 757 [P 78J, 759 Rastogi, R. P. 689, 699, 702, 760, Pestalozzi, W. G. 491, 723 [B 173] [R 43J, 773 [W 61J [R 82], 761 [R 119, 120, 121] Peters, M. 415, 756 [P 7] Pound, G. M. 74, 97 Rausch, A. 358, 761 [R 104] Peters, R. L. 315, 487, 757 [P 75] Poustian, J. E. 588, 757 [P 68] Raymond, A. J. 459, 760 [R 88] Peters, Th. 15, 17, 18,30,31 Powell, R. W. 284, 286 Reamer, H. H. 419, 428, 437, 440, Peterseim, F. D. 532, 756 [P12] Powell, W. B. 354, 475, 636, 756 725 [C 28], 758 [R 13, 14], Peterson, J. A. 235, 238 [P 23J, 757 [P 77J 759 [R 31, 33, 34, 35, 36], 762 Petker, 1. 429, 436, 749 [M 26] Powers, J. C. 497, 757 [P 86] [820] Petrowski, J. A. 491, 757 [P 82] Powers, J. V. 359, 489, 757 [P 69] Reardon, F. H. 652, 761 [R 113] Petrozzi, P. J. 475, 729 [D 62] Powling, J. 609, 610, 718 [A 73J, Rebiere, J. 472, 757 [P 83] Petschek, H. E. 17,31 754 [N 24J, 757 [P 61, 62J Redding, P. E. 553, 554, 689, 697, Petters, W. J. 367,756 [P 18] Pratt, R. 602, 605, 757 [P 55J 760 [R 78] Pettey, T. M. 661, 756 [P 41] Pratt & Whitney 652, 758 [P 93] Redmond 537, 760 [R 96] Pfiirtner 271, 286 Prescott, B. 537, 756 [P 13] Reed, R. P. 357, 477, 761 [R 102] Philipsen 44 Priapi, J. J. 714, 756 [P 4] Reese, B. A. 438, 759 [R 37, 38], Phillips, T. R. 300, 741 [H 134] Price, C. F. 184, 191, 706, 707, 772 [W 19] Phillipson, J. 44, 65 767 [S 260J, 768 [S 274] Reid, R. C. 360, 487, 720 [B, 63, Pierce, L. 339, 340, 341, 755 [P 1], Price, D. 273, 286 69] 756 [P 14] Price, E. W. 209, 214, 218 Reid, T. J., 726 [C 98] Pilipovich, D. 329, 758 [P 95] Price, F. P. 504, 654, 655, 756 Reilly, J. 275, 286 Pilz, W. 230, 238, 449, 680, 757 [P 42J, 757 [P 67] Reinhardt, T. F. 513, 759 [R 43] [P 73] Price, H. G. 301, 307, 308, 320, Remaly, R. F. 368, 768 [T 11] Pimentel, G. C. 345, 769 [T 24] 615, 616, 651, 659, 726 [C 78J, Renich, W. 654, 655, 657, 721 Pinkerton, M. K. 581, 756 [P 8] 730 [D 83], 756 [P 28, 29], 757 [B 92], 722 [B 143] Pinkston, J. T. 291, 324, 331, 719 [P 92] Reuel, N. C. 316, 759 [R 54] [B 3], 756 [P 26] Priem, R.J. 196, 197, 198,217, Reynales, C. H. 357, 759 [R 50] Pinns, 1\1. L. 528, 550, 577, 714, 298, 355, 513, 527, 663, 756 Reynolds, J. M. 761 [R 128] 716 [A 6], 748 [L 112J, 756 [P 27], 757 [P 57J Reynolds, T. W. 461, 486, 760 [P 32J, 757 [P 56J Priest, H. F. 310, 471, 614, 756 [R 95] Pino, M. A. 253, 257, 285, 705, [P 30, 34J Reynolds, W. D. 356, 760 [R 94] 756 [P 49], 757 [P 79J Probert, W. H. 361, 717 [A 56] Ribaud,76 Pitskhelauri, E. W. 381, 756 [P 19] Prok, G. M. 550, 773 [W 43] Ribovich, J. 594, 606, 752 [M 118] Pizzolato, P. J. 413, 593, 594, 757 Prosad, S. 352, 756 [P 20J Ricca, P. M. 321, 761 [R 122] [P 72J, 766 [S 195J Prosen 501, 587, 757 [P 64], 773 Rice, E. J. 475, 652, 741 [H 162] Place, E. R. 98 [W 80] Rice, M. J. 507, 761 [R 110, 111J Plank, C. J. 509, 756 [P 15] Prout, W. E. 601, 756 [P 31] Rice, O. K. 162, 163, 164, 177 Plate, J. B. 417, 719 [B 40J Pshezhetskiy, S. Ya. 762 [S 36J Rice, S. A. 345, 742 [J 30] Platt, G. K. 362, 756 [P 40] Psyras, G. H. 450, 723 [B 159] Rice, T. K. 592, 758 [P 90] Platz, G. M. 366, 368, 370, 373, Pugibet, M. 229, 238, 713, 752 Rice, W. E. 673, 684, 760 [R 75] 739 [H 98J, 756 [P 17J [M 122] Richards, R. J. 491, 723 [B 173], Plauson, R. A. 606, 753 [M 157] Punte, C. L. 404, 756 [P 21] 760 [R 69] Plescia, O. J. 598, 757 [P 76] Puranik, P. G. 348, 756 [P 16] Richter, G. N. 758 [R 13] N amenverzeichnis 791

Ricketson, B. W. A. 353,461,720 Rose 579, 758 [R 17] Ryker, 762 [S 34] [B 67], 759 [R 44] Rose, C. M. 98 Ryker, D. W. 541, 718 [A 68], 759 Rickey, R. P. 318, 320, 771 [V 9] Rose, L. C. 595, 601, 723 [B 169], [R 25] Riebling, R. W. 646, 775 [Z 15] 760 [R 86] Ryker, O. W. 522, 759 [R 27], 760 Riechmann, G. 743 [K 6] Rose, W. B. 333, 752 [M 137] [R 97] Riede, P. M. 479, 760 [R 70] Rosemary, J. K. 614,631,653,678, Ryschkewitsch, G. F. 588, 760 Riehl, W. A. 335, 357, 397, 665, 723 [B 170] [R 91] 666, 758 [R 10], 759 [R 46],761 Rosen, R. 296, 317, 746 [L 40, 42, [R 106] 43] Sanger, E. 25, 31, 230, 238, 366, Rinehart, W. T. 546, 759 [R 59, 60] Rosenbaum 471,759 [R 61] 550, 660, 764 [S 145], 765 Ring, E. 710, 760 [R 84] Rosendaal 502, 505, 760 [R 931 [S 162], 767 [S 247] Rittenhouse 759 [R 39, 40] Rosenthal, L. 593, 731 [E 20] Saenger, H. H. 426, 719 [B 36] Ritter, J. A. 489, 761 [R 115] Rosolovsky, V. J. 460, 761 [R 112] Sanger-Bredt, J. 16, 30, 366, 461, Rivard, J. G. 681, 761 [R 114] Ross, D. H. 406, 414, 758 [R 15], 471,660,764 [S 109],767 [8 247] Roaldi, A. 374, 748 [L 90] 760 [R 77] Sage, B. H. 419, 428, 429, 430, Robell, J. 521, 759 [R 26] Ross, D. S. 610, 761 [R 126] 431,432,436,437,442,444,509, Robbins, J. H. 483, 761 [R 108] Ross, P. S. 592, 679, 772 [W 9, 523, 553, 561, 725 [C 28], 728 Robbins, R. F. 359, 761 [R 103] 28] [D 18], 746 [L 8J, 750 [M 60], Roberts, E. R. 139, 156, 157, Rossano, A. T. 417, 759 [R 41] 758 [R 13], 759 [R 31, 32, 35], 176 Rosser, A. 597, 760 [R 85] 762 [S 20, 44] Roberts, O. P. 461, 479, 480, 750 Rosser, W. A. 195,217,676,677, Saggiomo, A. J. 557, 766 [S 235, [M 50], 757 [P 84] 758 [R 19, 20, 21, 22] 236] Roberts, R. W. 654, 761 [R 117] Rossini, F. D. 275. 286 Saint Robert 142 Robertson, G. D. 429, 434, 440, Rossmann, T. G. 760 [R 76J Salomon, A. 751 [M 88J 441,442,444,758 [R 23, 24], 759 Roth, E. M. 388, 394, 397, 759 Salser, G. E. 427, 730 [D 76J [R 32] [R 45] Salt, D. L. 177 Robertson, W. W. 601, 759 [R 58] Roth, J. F. 608, 760 [R 87] Salters, L. B. 592, 759 [R 47] Robillard, G. 144, 176 Roth, W. 674, 760 [R 74] Saltzman, B. E. 412, 417, 720 Robin, C. D. 480, 491, 759 [R 49] Rothberg, S. 572. 581, 758 [R 18], [B 41], 767 [S 249] Robinson, P. L. 347, 348, 741 759 [R 42], 760 [R 92] Salvatore, R. 760 [R 92] [H 151, 152] Rothe, K. 360, 488, 490, 761 Samanich, N. E. 759, 747 [L 53, 54] Robinson, W. C. 526, 539, 602, 603, [R 125] Samoilovich, V. G. 368, 762 [S 53] 759 [R 51], 760 [R 68] Rothenberg, E. A. 200, 217, 301, Sample, P. E. 654, 765 [S 168] Robotti, A. 651, 652, 760 [R 71] 307,309,315,320,538,616,618, Samuelson, L. E. 504, 766 [S 201] Rock, E. J. 569, 575, 585, 717 623, 624, 627, 629, 653, 755 Sandell, D. J. 492, 764 [S 117] [A 34] [0 10], 760 [R 65, 66], 764 Sandri, R. 378, 653, 762 [S 57], 763 Rocket Research Corp., 524, 525, [S 123, 147], 769 [T 26J, 770 [S 58], 767 [S 271] 532, 533, 596, 599, 600, 761 [T 90] Sands, G. A. 450, 762 [S 46] [R 1161 Roush, J. 505, 760 [R 89] Sanghvi, M. D. 439, 440, 441, 744 Rocketdyne 63, 76, 103, 104, 106, Rowe, W. H. 538, 616, 617, 629, [K 29],762 [S 51] 107,109,116,202,409,410,414, 654, 671, 755 [0 10, 14], 760 Sanz, S. 597, 751 [M 112] 445, 499, 504, 531, 532, 533, [R 73,83] Sarli, V. J. 98, 617, 724 [B 197] 563, 611, 612, 634, 639, 641, Rowinskij, A. E. 368, 732 [F 19] Sarner, S. 293,321, 343, 350, 408, 642, 647, 648, 669, 681, 682, 758 Rowley, R. W. 680, 761 [R 99, 428, 430, 432, 435, 444, 503, [R 9, 9a], 759 [R 28, R 29, 30], 118] 504,508,514,569,573,641,708, 760 [R 90], 761 [R 100, 109] Roy, .1\1. 198, 217 762 [S 14, 42] Roder, H. M. 464, 735 [G 90] Rozanov, D. K. 606, 729 [D 60J Sarner, S. F. 454, 457, 460, 497, Rodzitis, E. 292, 764 [S 136] Ruccia, F. E. 364,477,759 [R 48], 638, 768 [S 280] R6hm & Haas 559, 760 [R 79] 761 [R 124J Sarrat, P. 285 Roesky, H. W. 340, 344, 760 [R 67] Rudge, A. J. 291, 293, 325, 719 Sarten, P. 553, 563, 767 [S 253] Roger, 768 [T 8] [B 4],759 [R 53J, 761 [R 101] Sartori, P. 339, 344, 762 [S 48], 766 Rogers, A. C. 483, 761 [R 108] Rudyj, O. N. 686, 769 [T 40] [S 221] Rogers, G. T. 609, 736 [G 111] Ruff, O. 291, 299, 331, 333, 334, Satterfield, C. N. 385, 394, 395, Rogers, H. H. 341, 347, 640, 758 339, 341, 342, 347,758 [R 1, 2, 396, 397, 591, 592, 763 [S 87, [R 4, 11], 759 [R 62] 3,5,6,8], 759 [R 52] 88, 89, 90, 91, 92, 93, 96], 766 Rogers, J. D. 475, 476, 490, 759 Rumpel, W. F. 357, 739 [H 87] [S 225], 772 [W 24] [R 57], 761 [R 107], 770 [T 86] Runckel, J. :1<'. 592, 759 [R 47] Saunders, L. Z. 404, 756 [P 21] Rohrback, G. H. 331, 345, 758 Rundle, R. E. 345, 760 [R 63] Sawyer, A. E. 327, 761 [S 7] [R 7] Rupert, R. C. 419, 681, 767 [S 257, Sawyer, R. F. 638, 679, 767 Rollbuhler, R. J. 316, 318, 319, S 261] [S 272], 768 [S 281, 282, 289] 320, 636, 651, 652, 665, 758 Russel, K. C. 74, 97 Sawyer, W. A. 480, 492, 493, 725 [R 12], 759 [R 55, R 56], 760 Russel, L. M. 320, 321, 761 [R 123] [C 47, 48], 726 [C 70] [R 72], 761 [R 127], 770 [T 80] Rust, P. M. 609, 773 [W 75] Sax, J. 417, 536, 762 [S 19] Rom, F. E. 11, 30 Ruston, G. 461, 756 [P 24] Scanlon, J. J. 681, 765 [S 175] Romero, J. B. 31 Ryan, N. W. 156, 177 Scatchard, C. S. 387, 763 [S 102]

52* 792 Namenverzeichnis

Schaaf, V. P. 609, 766 [S 196, 198] Schreib, R. R. 333, 728 [D 4], 730 Semel, G. 444, 767 [S 262] Schafer, K. 326, 761 [S 5] [D 66] Semenov, 241, 284 Schafer, L. 489, 725 [049] SchrOder, J. 282, 286 Senior, D. A. 763 [S 62] Schaffner, J. G. 301, 764 [S 121] Schubert, F. 589, 748 [L 86] Settle, J. L. 292, 764 [S 136] Schalla, O. A. 489, 765 [S 177] Schubert, H. 153, 176, 177, 263, Setze, P. O. 654, 655, 657, 724 Schalla, R. L. 256, 259, 260, 285, 285 [B 207], 755 [0 16], 768 504, 655, 691, 700, 701, 735 Schubert, J. 231, 238 [S 287] [G 68], 765 [S 185, 189], 766 Schufflebotham, N. 361, 763 Shanley, E. S. 393, 394, 395, 397, [S 208] [S 79] 402, 403, 759 [R 45], 763 [S 82, Schallus, E. 521, 738 [H 28] Schultz, J. L. 444, 732 [F 12] 83], 767 [S 241] Schapiro, J. B. 551, 602, 765 Schultz, J. W. 356, 365, 366, 763 Shapiro, 1. 729 [D 57] [S 152], 766 [S 234] [S 81] Shapiro, J. 503, 766 [S 200] Scharle, W. J. 349, 462, 463, 478, Schulze, G. 762 [S 32] Sharkley, A. G. 444, 732 [F 12] 480, 486, 764 [S 115], 771 [V 5] Schulze, W. A. 541, 766 [S 232] Sharpe, A. G. 291, 323, 324, 738 Schechter, W. H. 502, 504, 589, Schumacher, H. J. 322, 329, [H 60], 762 [S 30] 766 [S 202] 346, 368, 733 [G 10], 737 Sheard, J. L. 332, 764 [S 143] Scheck, W. G. 357, 728 [0 158], 753 [G 157], 763 [S 66], 764 [S 138, Sheehan, D. F. 329, 343, 724 [M 181] 139] [B 211], 748 [L 110] Scheer, M. D. 326, 761 [S 3] Schumachcr, J. O. 459, 767 [S 250] Sheehan, W. R. 414, 737 [G 156] Scheller, K. 661, 662, 765 [S 165] Schumacher, 'V. 261, 285 Sheft, J. 345, 750 [M 64] Schick siche unter von Schick Schuman, L. H. 417, 743 [K 22] Shelberg, W. E. 528, 562, 570, 577, Schieler, L. 65, 97, 103, 112, 117, Schumb, W. O. 291, 340, 385, 388, 767 [S 254,266,267,268] 149,150,176,150,176,189,191, 394, 397, 763 [S 84, 85, 86], Sherburne, A. E. 720 [B 64] 595, 598, 766 [S 193] 764 [S 118, S 144], 766 [S 225] Sheridan, P. B. 450, 769 [T 59] Schigatsch, A. F. 504, 766 [S 228] Schwartzberg, F. R. 357, 477, 766 Sherley, J. E. 472, 765 [S 170] Schilling, 1\1. 765 [S 166] [S 192] Shieber, H. 419, 681, 767 [S 257, Schlesinger, H. 1. 497, 506, 705, Schwarz, E. 521, 742 [J 10], 762 261] 723 [B 188], 733 [F 63], 766 [S 35] Shilov, A. E. 614, 745 [K 101] [S 212, S 229],767 [S 251,252] Scott, O. R. 551, 560, 688, 705, 717 Shinn, A. M. 615, 758 [P 92] Schlesinger, H. J. 705, 766 [S 205] [A 46, 47, 59, 60], 765 [S 182, Shinner, R. 155, 156, 177 Schmeisser, M. 331, 339, 344, 345, 186, 187] Shishkov, Yu, D. 326, 761 [S 6] 762 [S 11, 12, 48], 766 [S 221, Scott, D. W. 525, 526, 762 [S 38] Shomate, O. H. 586, 729 [D 45] 222] Scott, F. F. 762 [S 40] Short, J. N. 765 [S 182] Schmiedlin, R. F. 203, 217 Scott, H. E. 652, 741 [H 155] Sib bitt, W. L. 428, 762 [S 45] Schmidt, A. F. 481, 483, 484, 487, Scott, H. F. 412, 413, 716 [A 11, Sicre, J. E. 322, 346, 733 764 [S 108], 765 [S 154, 171] 15] [G 10] 764, [S 138, 139] Schmidt, E. W. 222, 225, 289, 339, Scott, H. T. 476, 480, 771 [V 6] Siegel, A. R. 30, 191 341,343,344,461,554,556,586, Scott, J. E. 603, 735 [G 69] Siegel, B. 65, 97,103,112, 117, 602,610,636,640,653,655,761 Scott, L. E. 358, 761 [R 104] 149,150, 176, 189, 191, 528, 736 [S 1], 762 [S 17], 763 [S 106], Scott, R. B. 464, 467, 468, 469, 470, [G 120] 765 [S 150, 151, 163, 164, 179] 772 [W 37], 774 [W 98] Siegmund, G. 45, 65 Schmidt, H. W. 301, 302, 305, 306, Scott, R. W. 492, 766 [S 216] Siegmund, J. M. 311, 312, 313, 318, 309,310,314,315,316,317,320, Scully, E. J. 480, 481, 487, 489, 319, 329, 415, 504, 584, 762 321, 730 [D 67], 761 [R 123],764 490, 763 [S 107] [S 23],764 [S 131, 134] [S 123, 127, 129, 130], 768 Scurlock, A. O. 681, 766 [S 220] Sievers, G. K. 650, 651, 765 [S 157] [S 277] Seader, J. D. 391, 471, 503, 513, Sievers, R. F. 455, 763 [S 75] Schmidt·Tintemann, U. 321, 764 527, 548, 741 [H 148], 753 [M Sikes, J. H. 529, 775 [Y 10] [S 137] 166], 767 [S 264] Siler, R. K. 319, 321, 767 [S 265] Schmitt, O. R. 299, 317, 764 [S 132, Seamans, T. F. 657, 681, 768 Silocks, O. G. 602, 769 [T 27] 133] [S 273], 772 [V 38] Silverman, H.-P. 301, 412, 578, Schmitz, B. W. 599, 767 [S 269, Sears, D. R. 345, 750 [M 63] 770 [T 88] 270] Seaver, R. E. 300, 764 [S 122] Silverman, J. 657, 722 [B 142] Schmitz, E. 767 [S 237] Seel, F. 327,764 [S 149] Silverstcin, A. 461, 766 [S 226] Schmueli, K. 360, 491, 764 [S 114] Segel, M. 486, 767 [S 245] Sima, J. J. 338, 768 [S 278] Schneebeli, P. 691, 699, 701, 765 Segel, M. P. 483, 548, 724 [B 210], Simkin, D. J. 389, 391, 763 [S 97] [S 176] 767 [S 246] Simkin, J. 346, 762 [S 15] Schneider, H. 588, 590, 657, 670, Seidel, A. 475, 653, 768 [S 284] Simons, H. P. 654, 756 [P 43],765 763 [S 95], 767 [S 255] Seidel, H. H. 475, 733 [F 68] [S 168], 766 [S 213] Schnitzlein, J. G. 332, 764 [S 143] Seifert, H. S. 48, 65 Simons, J. H. 291, 323, 762 [S 31] Schoenfelder, O. W. 339, 342, 343, Sekleman, H. V. 705, 766 [S 230J Simmons, F. S. 659, 765 [S 159] 762 [S 13, 47] Sekler, ~. 395, 763 [S 88] Simpson, G. E. 366, 763 Schoettlin, O. E. 502, 505, 506,589, Selig, H. 345, 726 [0 62] [S 80] 766 [S 211] Sellars, J. R. 597, 722 [B 117] Simpson, J. O. 490, 744 [K 49] Schram, S. R. 291, 307, 314, 317, Selleck, F. T. 419, 762 [S 20J Singleton, A. H. 301, 305, 306, 321, 764 [S 119] Selzer 165 328, 764 [S 142] Namenverzeichnis 793

Sisler, H. S. 537, 730 [D 65] Snegyreva, T. D. 98 Stephenson, C. C. 511, 762 [S 49] Sivo, J. N. 655, 768 [S 288] Snoek, E. 415, 743 [K 8] Stephenson, M. E. 471, 767 [S 243] Sjoblon, J. J. 593, 594, 766 [S 195] Snyder, A. D. 654, 765 [S 180], 766 Stern, G. 328, 761 [S 8] Skinner, D. A. 327, 761 [S 7] [S 214) Stern, M. D. 153, 176 Skinner, G. B. 654, 765 [S 180],766 Snyder, H. J. 762 [S 371 Stern, S. A. 428, 441, 762 [S 43] [S 214] Sobeniak, M. 681, 754 [N 5] Stettbacher, A. 676, 762 [S 29] Skirrow, G. 635, 762 [S 18] Sobolev, N. N. 692, 767 [S 259] Steunenberg, R. K., 761 [S 2] Skolnik, S., 727 [C 119], 766 [S231] Solomon, 1. J. 336, 765 [S 169], Steward, W. G. 760 [R 69] Skorokhodov, 1. 1. 385, 763 [S 99, 768 [S 276] Stewart, R. B. 470, 765 [S 173] 100] Solomon, W. S. 356, 760 [R 94] Stewart, P. A. E. 764 [S 110] Slabey, V. A. 299, 302, 318, 551, Somogyi, D. 702, 703. 765 [S 181] Stiel, L. J. 501, 763 [S 103] 764 [S 128, 140] Sorokin, Yu. A. 521, 7li2 [S 36] Stockinger, H. E. 383, 762 Slater, V. W. 593, 763 [S 94] Soorovikin, V. F. 98 [S 52] Slavinskaya, N. A. 378, 763 [S 73] Sotak, R. E. 480, 483, 484, 766 Stocks, G. W. 597, 718 [A 65] Slesser, C. 291, 307, 314, 317, 321, [S 227] Stober, "T. 732 [F 18] 764 [S 119] Spakowski, A. E. 301, 303, 478, Stokes, C. S. 322, 374, 379, 384, Slough, C. M., 726 [C 68] 563, 576. 755 [09], 762 [S 27] 640, 662, 763 [S 59, 76], 764 Smelser, P. 360, 492, 765 [S 172] Spalding, D. B. 164, 177, 185, 191, [S 146],767 [S 240, 242, 263] Smetana, J. 774 [W 107] 207,218 Stokinger, H. E. 384, 765 [S 191] Smiley, S. H. 317, 764 [S 132] Spencer. ~I. 576, 597.664, 674, 735 Stonc, F. G. A. 500, 766 [S 204] Smith, A. L. 468, 469, 589, 615. [G 84, 89], 736 [G 122, 135] Stoy, S. T. 356, 479, 732 [F 23], 655, 724 [B 208], 743 [J 54J, Spencer, R. T. 490, 768 [S 286] 765 [S 153] 763 [S 105] Spengler, G. 248. 249, 250, 251, Strahle, W. C. 212, 218 Smith, B. G. 475, 733 [F 68] 252,254,258,259,285,691,696, Straigt, D. M. 616, 635, 651, 653, Smith, C. P. 351, 356, 746 766 lS 215],767 [S 258] 665, 733 [G 5], 760 [R 72], 764 [L 20], 763 [S 78], 765 [S 155] Spialter, L. 563, 751 [M 100] [S 147] Smith, D. D. 618, 764 [S 148] Spicer, D. R. 310, 731 [F. 41] Strakhov, B. V. 350, 369, 378, 731 Smith, D. F. 326, 329, 724 [B 195], SpieB, T. 436, 743 [K 161 [E 19],763 [S 70] 761 [S 4], 762 [S 50] Spohn, E. 270, 286 Strasser, A. 492, 536, 563, 580, Smith, G. C. 502, 504, 752 [M 133J Sprenger, D. J". 176 719 [B 24], 734 [G 18] Smith, H. J. 360, 764 [S 116] Stacey, M. 323 Streetman, J. R. 476, 736 [G 129] Smith, 1. E. 602, 604, 607, 610, Stage, H. 368, 762 [S 54], 763 Streett, W. B. 487, 764 [S 111J 726 [C 69, 76], 765 [S 156] [S 101] Streich, 1\1. 462, 483,765 [S 174] Smith, J. M. 409, 554, 731 [F 4], Stahl, U. 654, 765 [S 167] Streim, H. G. 562, 577, 578, 762 733 [F 57],773 [W 51] Stai, D. F. 409, 767 [S 248J [S 26] Smith, J. R. 490, 530, 562, 570, Staite. I. J. 301, 764 [S 124] Streng, A. G. 299, 317, 331, 577, 578, 725 [C 33], 762 [S 26]. Stake, A. ~l. 414, 768 lS 285] 336,338,345,369,370,371,372, 773 [W 68] Stamper, J. G. 298, 764 [S 120] 374,375,376,377,379,384,662, Smith, K. C. 462, 463, 480, 772 Stanford, H. B. 414, 770 [T 83] 6m, 733 [G 8, 11], 734 [G 30], [W 34] Staple, E. 301, 764 [S 121] 736 [G 124J, 743 [K 5], 744 Smith, L. R. 362, 764 [S 113] Starieco, E. H. 322, 764 [S 138] [K 45], 745 [K 104], 762 [S 16, Smith, L. S. 757 [P 80] Stark, T. M. 551, 766 [S 219J 55, 56J, 763 [S 59, 60, 61, 63, 64, Smith, R. A. 342, 733 [G 1, 2] Staudhammer, P. 680,731 [E 11] 65, 67, 68, 74], 764 [S 135], 765 Smith, R. V. 355, 359, 471, 722 Staverman, A. J. 127, 152, 176 [S 160, 178, 190J. 766[S223,224], [B 146],763 [S 69] Steckly, Z. J. J. 9, 30 768 [S 279] Smith, R. W. 591, 690, 720 [B 59], Steele, A. J. 767 [S 238] Streng, L. A. 379, 763 [S 591 721 [B 107] Steffen, F. \Y. 651, 652, 721 Streng, L. V. 766 [S 223J, 768 Smith, S. H. 501, 503, 766 [S 203, [B 82] [S 279] 209] Steffy, R. J. 730 [D 71J Strickcr, W. 298, 768 lS 275] Smith, T. D. 480, 481, 487, 489, Stehling, K. 193, 217 Strier, M. P. 248, 284, 560, 567, 490, 763 [S 107] Stehling, K. R. 478, 525, 546, 763 690, 691, 700, 701, 703, 760 Smith, T. L. 154, 177 [S 77J, 764 [S 112J [R 80, 81], 765 [S 188J Smith, W. A. W. 610, 757 [P 61, Stein, L. 292, 301, 330, 762 [S 28], Strite, M. K. 475, 741 [H 143] 62] 764 [S 125, 136] Strunk 762 [S 41 J Smith, W. D. 414, 415, 681, 762 Stein, S. 658, 765 [S 161] Stuart, A. P. 521, 762 [S 33J [S 24] Stein, T. W. 394, 763 [S 89] Stukey, J. :\1. 479, 753 [1\1 168J Smith, W, G. 413, 727 [C 126] Steinberger, R. 124, 176, 609, 766 Stuhlinger, E. 17,21,22,23, 25, 30, Smith, W. J. 489, 732 [F 33J [S 196, 197, 198, 199J 31 Smith, W. L. 502, 766 [S 210] Steindler, 1\1. J. 301, 705, 764 Stumpe, A. R. 581, 762[S 25] Smith, W. W. 599, 767 [S 270] [S 126], 766 [S 233] Sturm, B. 275, 286 Smolak, G. R. 479, 765 [S 158] Stellrecht, D. H. 484, 729 [D 46] Suarez-Alfonso, E. 328, 412, 413, Smoot, L. D. 185, 191, 706, 707, Stemmer, J. 764 [S 141] 414, 504, 761 [S 9], 762 [S 10, 767 [S 260], 768 [S 274] Stengel, L. A. 595, 601, 765 [S 183, 21,22],766 [S 206,2071 Smyth, H. F. 321, 334, 417, 572, 184], 766 [S 194], 767 [S 239] Sugden, R. P. 490, 769 [T 47] 581,768 [S 283] Stephanou, S. E. 409, 767 1:S 248] Suhrmann, R. 275, 276, 286 794 N amenverzeichnis

Sukornick, B. 339, 733 [G 7] Thieme, J. O. 658, 731 [E 40], 770 Tower, L. 655, 657, 733 [F 48] Sullivan, A. 359, 489, 761 [R 105] [T 79] Tower, L. K. 461, 655, 660, 768 Sullivan, E. A. 497, 757 [P 86] Thiokol Chem. Corp. 134, 136 [T 20], 769 [T 54, 55] Summerfield, M. 116, 118, 143, 155, Thodos, G. 501, 730 [D 78], 763 Townsend, C. R. 301,412, 578, 770 156,166,168,173,177,263,270, [S 103] [T 88] 594,717 [A 62] Thomas, A. A. 506, 578, 581, 589, Trauzl273 Summers, W. H. 679, 768 [S 290] 719 [B 22], 728 [D 8], 729 [D 58], Travers, M. W. 602, 769 [T 27] Sundaram, T. R. 191 756 [P 8] Traverse, G. 607, 770 [T 63] Sussman, M. 643, 767 [S 256] Thomas, D. D. 549, 595, 596, 607, Trebes, D. M., 753 [M 166] Sutherland, G. S. 176, 177 683, 686, 718 [A 71, 72], 769 Trent, C. H. 688, 769 [T 22, 38] Sutton, G. 30, 46, 62, 65, 97, 117, [T 31, 36, 44] Trofimov, V. S. 606, 729 [D 60] 192, 194, 206, 216 Thomas, M. D. 770 [T 74] Trofimova, E. M. 614, 745 [K 101] Sutton, N. V. 571, 578, 588, 590, Thomas, N. 769 [T 30] Troyan, J. E. 521, 522, 533, 759 657,766 [S 217, 218], 767 [S 255] Thomas, W. H. 349, 768 [T 13] [R 27], 768 [T 9] Sutton, W. K. 746 [L 32] Thompson 694, 769 [T 42] Trucks, H. F. 362, 770 [T 73] Svirbely, J. L. 502, 504, 505, 506, Thompson, C. I. 451, 769 [T 50] Trush, B. A. 676, 717 [A 22] 738 [H 41], 748 [L 85], 763 [S 71, Thompson, J. F. 360, 487, 754 Tschinkel, J. G. 397, 403, 454, 72] [N 38], 770 [T 78] 455,456,543,544,545,591,608, Swalley, F. E. 486, 489,767 [S 244] Thompson, R. J. jr. 65, 208, 217, 686, 704, 768 [T 14, 15, 16], Swart, K. H. 154, 177, 273, 286 218, 504, 614, 615, 689, 769 769 [T 23, 41, 48] Swehla, R. J. 370, 373, 739 [H 98] [T 25, 34, 37, 53] Tschuikow-Roux, E. 348, 768 Swenson 522, 759 [R 25],762 [S 34] Thompson, W. R. 475, 481, 737 [T 2] Szegho, G. C. 6, 30 [G 152], 769 [T 29], 770 [T 87] Tsentsiper, A. B. 385, 768 [T 17] Szetela, E. J. 391, 475, 763 [S 98, Thorp, C. E. 367, 368, 369, 375, Tsien, H. S. 451, 452, 548, 564, 104] 381, 383, 768 [T 11, 12] 770 [T 60] Szwarc, M., 762 [S 39] Thorpe 768 [T 8] Tsitsischwili, L. D. 529, 734 [G 24] Thurston 770 [T 71] Tsuchiya, S. 685, 686, 770 [T 65, Tabala, W. 679, 681, 770 [T 82], Thurston, R.S. 476,770 [T61, 72,86] 77] Tuczek, H. 17, 30 772 [W 8] Thynne, J., 757 [P 61] Tibbels, C. M. 450, 769 [T 59] Turkheimer, P. 360, 768 [T 18] Tait, C. W. 440, 529, 570, 577, 606, Tickner, A. W. 602, 747 [L 49] Turnbull, S. G. 291, 299, 300, 317, 609, 725 [C 15], 740 [H 110], Ticknor, L. B. 387, 763 [S 102] 768 [T 21] 768 [T 7], 769 [T 39] Tillman, R. M. 590, 740 [H 117] Turner, C. F. 117, 265, 266, 285, Tajima, Y. A. 427, 730 [D 76] Tilton, V. V. 555, 556, 739 [H 74] 595, 604, 735 [G 72] Tamas, A. A. 589, 774 [W 82] Timmerhaus, K. D. 471, 490, 729 Turner, J. J. 345, 769 [T 24] Tannenbaum, S. 328, 562, 582, [D 41], 769 [T 47] Tyler, W. E. 610, 770 [T 89] 588, 636, 678, 684, 718 [A 80], Tiner, N. A. 306, 334, 338, 770 Tyler, W. H. 679, 680, 761 [R 118], 736 [G 115, 138], 768 [T 1], 769 [T 85] 770 [T 81] [T 57] Tischler, A. 0.659,757 [P 58] Tyson, G. N. 705, 770 [T 62] Tanner, A. D. 549, 683, 773 [W 57] Tischler, O. 221, 238 Tans, A. M. P. 768 [T 10] Tittle, B. 348, 770 [T 66] Ugine 329, 770 [U 6] Tantam, D. H. 360, 769 [T 28] Tkachenko, E. A. 353, 354, 768 Ulich 241, 284 Tarifa, C. S. 597, 769 [T 45, 46] [T 19] Ulich, H. 717 [A 26] Tarr, I. 330, 737 [H 3] Tlumac, F. N. 343, 728 [D 21] Ulimanns 511, 770 [U 2] Tathow, J. G. 323 Tobolsky, A. V. 127,152,153,176, Union Carbide-Linde Co. 481, 485, Tatom, J. W. 483, 487, 726 [C 74], 177 770 [U 4] 769 [T 32] Toeniskoetter, R. H. 329, 737 Urbanski, T. 456, 770 [U 5] Tavernier, P. 176, 769 [T 43] [G 149] US Bureau of Mines 76 Taylor, C. S. 508, 725 [C 34] Tolberg, W. E. 341, 770 [T 84] Useller, J. W. 655, 722 [B 119] Taylor, F. R. 686, 769 [T 35,40] Tomazic, W. A. 618, 636, 650, 651, US Navy Med. News Letter 549, Taylor, G. D. 768 [T 3] 652, 677, 678, 758 [R 12], 761 770 [U 3] Taylor, J. 156, 176, 769 [T 51] [R 127], 765 [S 157], 768 [T 6], US Office of the Director of Taylor, L. J. 549,753 [M 151] 769 [T 26], 770 [T 80, T 90] Defense Res. and Engineering Taylor, L. L. 442, 445, 749 [M 13, Tomlinson, E. M. 681, 769 [T 33] 310,320,321,328,364,366,401, 24] Tompson, C. I. 769 [T 50] 408,414,444,450,458,459,480, Telle, O. 272, 286 Toole, L. E. 739 [H 96] 511,514,515,533,536,548,553, Tenenbaum, D. M. 414, 415, 416, Toops, E. E. 451, 452, 595, 601, 554,555,564,575,578,579,581, 584, 768 [T 4] 766 [S 194], 769 [T 49], 770 770 [U 1] Tepper, L. B. 231, 238 [T 64] Terpko, D. E. 503, 722 [B 128] Tormey, J. F. 65, 586, 769 [T 56] Van Dael, W. 350, 351, 353, 464, Terpko, S. P. 455, 727 [C 141] Toth, J. M. 357, 486, 770 [T 67, 771 [V 27] Tesner, P. A. 98 68,69,70] Vandenkerckhove, J. 30, 53, 65, Thayer, J. R. 624, 770 [T 76] Toth, L. R. 414, 770 [T 83] 97,101,117,143,144,146,176, Theilacker, W. 573, 768 [T 5] Toulmin, H. A. 500, 550, 769 192,194,198,202,206,207,208, Theile, H. 609, 769 [T 52] [T 58], 770 [T 75] 209,210,212,216,253,254,257, N amenverzeichnis 795

258,284,428,429,430,524,526, Vose, D. W. 497, 757 [P 86] Weber, W. 387, 744 [K 39] 549, 575, 699, 719 [B 30] Vosman, A. 367 Webster, T. J. 463, 480, 772 Van der Ahrend, P. O. 462, 463, Vosper, A. J. 719 [B 13] [W34] 478, 480, 486, 771 [V 5, 10, 32] Vouk, V. B. 455, 771 [V 19] Weeks, J. L. 345, 773 [W 45] Vanderhyde, N. J. 458, 771 [V 20] Voyer, R. 357, 477, 771 [V 33] Weeks, .vI. H. 504, 572, 581, 759, Van Dolah, R. W. 459, 609, 775 [R 42], 772 [W 11], 773 [W 77] [Z 10] Waesche, R. H. W. 604, 773 Wegener, P. P. 72, 74, 97, 98, 234, Vango, S. P. 429, 436, 437, 442, [W 70] 238 541, 549, 749 [M 13, 26], 753 Wagman 501,774 [W 81] Wegener, E. 573, 768 [T 5] [1'1152], 771 [V 25] Wagman, D. D. 353, 772 [W 30] Weil, L. 357, 472, 477, 750 [M 51] Van Gundy, DA 361, 486, 723 Wagner. H. G. 597, 751 [M 113] 757 [P 83], 771 [V 33] [B 163], 771 [V 7] Wagner, W. R. 391, 471, 503, 513, Weilmuenster, E. A. 588, 748 Vanica, D. F. 489, 771 [V 28] 527,767 [S 264] [L 83] Van Itterbcck, A. 350, 351, 353, Wahlquist, A. L. 706, 774 [W 95] Weinberg, F. J. 98 464, 470, 771 [V 14, 15, 16, 27, Walker, O. A. 479, 748 [L 98] Weir, F. W. 504, 537, 573, 773 29,30] Wallack, S. 417, 556, 580, 723 [W 77],774 [W 89] Van Meter, R. A. 481, 772 [B 157] Weir, R. J. 329, 738 [H 35] [V 37] Wallenstein 501, 587, 773 [W 80] Weiss, H. G. 503,705,766, [S 200], Van Nice, L. J. 599, 752 [M 115, Wallner, L. E. 479, 765 [S 158] 773 [W 60],774 [W 86] 116] Walsh 360, 772 [W 22] Weiss, S. 478, 487, 755 [0 15], 773 Vanpee, M. 504, 654, 657, 681, Walter, H. 593, 674, 772 [W 25, [W 52] 705, 768 [S 273], 771 [V 23, 24], 26], 773 [W 65] Weitzel, D. H. 357, 772 [W 36], 772 [V 38], 774 [W 83] Walter, R. J. 774 [W 99] 774 [W 108] Van Paemel, O. 771 [15] Walters, O. J. 554, 773 [W 51] Weleff, W. 477, 774 [W 91] Van Tiggelen, A. 606, 664, 677, Walters, H. H. 471, 773 [W 44] Wellman, H. B. 604, 774 [W 101] 729 [D 43, 49], 771 [V 13] Walters, T. 1\1. 394, 746 [L 26] Welsh, F. E. 333, 752 [M 137] Van Vorst, W. D. 597, 771 [V 22] Walters, W. P. 602, 750 [M 67] Wendt, R. P. 346, 749 [M 4] Vargo, D. J. 495, 771 [V 34] Walton, A. L. 549, 683, 773 Wenger, N. 0.774 [W 107] Vasta, V. M. 749 [M 6] [W 57] Wenograd, J. 155, 156, 177 Vaughan, J. O. 652, 772 [V 36] Wang, D. 1. J.479, 757 [P 84], Wentworth, R. L. 385, 394, 397, VDI218 760 [R 70] 774 [W 85] Veley 428, 771 [V 2] Wang, E. S. J. 355, 750 [M 45] Wernick, J. H. 30 Verbecke, O. 350, 771 [V 14, 16] Wanhainen, J. P. 592, 655, 679, Wesley, B. K. 344, 748 [L 111] Verderame, F. D. 530, 771 [V 26] 768 [S 288], 772 [W 9, 28], 774 WESTFAOO 574, 575, 578, 579, Verdier, H.176 [W 103] 581, 772 [W 6] Verhaegen, L. 350, 350, 771 [V 29] Wannagat, U. 521, 772 [W 14] Westlake, E. F. 589, 774 [W 82] Verschoyle, P. D. 115, 117, 458, Ward, D. L. 494, 773 [W 59] Wetmore, K. R. 489, 732 [F 33] 606,771 [V 18] Warner, O. F. 474, 685, 732 [F 30], Wetmore, W. H. 610, 614, 631, Vetere, A. M. 473, 727 [0124] 775 [Z 5] 653, 774 [W 102] Veubeke siehe Fraeijs de Veubeke Warren, R. H. 490, 754 [N 30] Weyl, T. 275, 283, 284, 286 Vialatte, M. M. 445, 771 [V 3] Warshavosky, 1. 491, 750 [M 72] Weymouth, F. R. 636, 772 [W 3] Vieille 142 Wasko, R. A. 679, 774 [W 105] Whaley, T. P. 550. 774 [W 87] Vigdortschik, N. A. 417,771 [V 4] Wasserbauer, J. F. 679, 772 Wharton, W. W. 709, 728 [0 155] Vincent, D. W. 681, 770 [T 82], [W 8] Whatley, A. T. 654, 773 [W 56] 774 [W 103] Waszeslak 501, 587, 773 [W 79] Whitacker, G. O. 301, 773 [W 41] Vincent, L. A. 453, 771 [V 1] Waterman, T. E. 370, 371, 720 White, B. G. 461, 738 [H 53] Vliet, G. O. 483, 771 [V 31] [B 44], 772 [W 20] White, D. 293, 294, 295, 296, 297, Vogel, R. 301, 764 [S 125] Watson, D. D. 397, 759 [R 46] 298, 305, 465, 738 [H 62], 772 Vogel, R. O. 761 [S 2] Watson, J. F. 357, 727 [0131] [W 29,38] Vogt, J. W. 771 [V 35] Watt, G. W. 521, 772 [W 13] White, E. L. 301, 302, 304, 306, Vogt, P. R. 310, 631, 653, 771 Wayman, D. H. 686, 773 [W 61] 471,773 [W 40] [V 8] Weast, R. O. 564, 774 [W 111] White, L. 442, 443, 445, 723 Volz, H. A. 505, 760 [R 89] Weatherby, J. H. 537, 749 [.vI 34] [B 160], 772 [W 10] von Ardenne, M. 20 Weaver, R. D. 525, 529, 578, 772 White, L. E. 652, 750 [1\1 69] von Brecht, F. L. 607, 747 [L 74] [W 5] White, W. B. 71, 98 von der Heyde, N. J. 318, 320, 771 Webb, A. K. 529, 571, 578, 730 White, W. D. 550, 774 [W 100] [V 9] [D 89] Whitnak, G. O. 525, 529, 576, 578, von Elbe, G. 298, 476, 480, 746 Webb, M. J. 176, 177 772 [W 5, 16] [L 36], 771 [V 6] Weber, A. 326,772 [W 2] Whitney, E. D. 774 [W 97] von Glahn, V. H. 473, 771 [V 12] Weber, A. E. 589, 752 [M 135], 772 Whittaker, A. 419, 772 [W 4] von Karman, Th. 198, 210, 217 [W2] Whittaker, A. G. 394, 609, 728 Vonnegut, B. 726 [075] Weber, O. W. 301, 738 [H 64] [D 22], 769 [T 39], 772 [W 23], von Nieciecki 712, 724 [B 194] Weber, L. A. 464, 465, 735 [G 90], 773 [W 63, 73, 75, 76] von Schick, O. 451, 771 [V 21] 773 [W 58] Whittick, J. S. 332, 774 [W 109] von Zborowski, H. 247, 771 [V 17] Weber, O. A. 455, 771 [V 19] Wiberg, E. 497, 774 [W 94] 796 N amen verzeichnis

Wiberg, K. B. 551, 774 [W 88] Wilson, R. H. 773 [W 46] Yakolewa, T. V. 774 [Y 1] Wiberley, S. E. 504, 654, 655, 721 Wilson, R. Q. 522, 772 [W 15] Yamamura, S. S. 529, 775 [Y 10] [B 90], 722 [B 130, 133] Wilson, W. E. 705, 723 [B 164] Yamauchi, T. 414, 753 [M 179] Wicke, E. 298, 326, 476, 761 [S 5], Wimpress, R. N. 176 Yanyecic, G. A. 610, 773 [F 71] 772 [W 39], 773 [W 42] Winning, W. 1. H. 527, 772 Yard, A. S. 570, 749 [M 33] Wiebenga, E. H. 323, 774 [W 84] [W 17] Yastrebov, V. V. 377,380,381,756 Wiegand, J. H. 153, 176 Winkler, O. 275, 286 [P 19], 774 [Y 2, 3, 4, 5] Wiesbock, R. A. 610,774 [W 110] Winstead, T. W. 483, 723[B 183] Yates, G. B. 494, 775 [Y 11] Wiggin, E. 301, 764 [S 121] Winterberg, F. 17, 31 Yin, P. 411, 727 [C 146] Wilber, P. C. 679, 728 [C 153], 774 Winternitz, P. F. 606, 655, 660, Yoffe, A. D. 609, 736 [G 112] [W 104] 773 [W 53, 54, 69] Young, A. 737 [H 9] Wilcox, K. K. 362, 772 [W 35] Wintersteen 480, 772 [W 32] Young, D. A., 774 [Y 6] Wilcox, O. W. 433, 523, 553, 561, Wintucky 595, 773 [W 66] Young, J. A. 343, 452, 454, 456, 750 [M 60] Wirth, H. E. 773 [W 78] 457,728 [D 21],775 [Y 9] Wilde, K. A. 97, 98, 609, 773 Wise, H. 195, 217, 758 [R 20, 21], Young, R. S. C. 394,395,763 [S 91] [W 71,72] 773 [W 55] Younglove, B. A. 468, 774 [Y 7], Wilfong, R. E. 164, 261, 262, Witkin 572, 573, 581, 772 [W 7] 775 [Y 8] 285 Witkin, L. B. 537, 749 [M 34] Yurczyk, R. :1<'.494,774 [W lJ2] Wilkins, R. G. 478, 772 [W 31] Witte, A. B. 582, 772 [W 12] Wilkins, R. L. 65,71,97,618,620, Witzke, W. R. 550, 773 [W 43] Zabelka, R. J. 664,681,775 [Z 8] 734 [G 58] Woerner 738 [H 31] Zabetakis, :tV!. G. 364, 366, 415, Wilkinson, G. 342,772 [W 1] Wojtowicz, J. A. 385, 750 [M 44] 459,480,492,533,562,576,577, Williams, D. A. 599, 767 [S 270] Wolf, A. A. 327, 719 [B 6] 580, 597, 609, 719 [B 19], 728 Williams, F. A. 164, 170, 177 Wolf, F. K. 359, 480, 748 [L 109] [D 14], 733 [F 47], 737 [H 16], Williams, G. C. 591, 772 [W 24] Wolf, H. 547, 739 [H 69], 750 757 [P 74],775 [Z 3,6,10,11] Williams, H. 609, 769 [T 39], 773 [M 61], 772 [W 19] Zahringer, A. J. 176,436,775 [Z 1] [W 75,76] Wolfe, S. W. 494, 774 [W 92] Zaki, S. A. 394, 750 [M 39] Williams, J. 588, 589, 722 [B 138, Wolff, H. 286, 438, 474 Zborowski siehe unter von Zbo- 139] Wolfhard, H. G. 97, 504, 597, 609, rowski Williams, K. 231, 238 635,654, 674, 685, 717 [A 61], 739 Zeigler, K. 475, 759 [R 57] Williams, R. L. 588, 589, 722 [H 99], 756 [P 44, 45], 762 [S 18], Zeleznik, F. J. 98 [B 138, 139] 771 [V 23, 24], 773 [W 74, 83] Zelman, 1. M. 357, 479, 775 [Z 14] Williams, W. H. 685, 773 [W 62] Wong, A. K. 445, 745 [K 82] Zettle, E. V. 646, 775 [Z. 15] Williamson, F. 684, 773 [W 64] Wong, E. L. 658, 735 [G 79] Ziebland, H. 354, 548, 722 [B 152], Williamson, K. D. 475, 774 Wood, C. C. 362, 756 [P 40] 739 [H 79], 775 [Z 13] [W 93] Wood, J. L. 575, 717 [A 20] Ziegler, W. T. 353,471, 750 [M 38, Willis, C. M. 592, 759 [R 47], 772 Wood, W. S. 593, 763 [S 94] 79,80] [W 27] Woods, H. P. 707, 709, 739 [H 94], Ziemer, R. W. 17,31 Willis, W. L. 490, 773 [W 68] 740 [H 104, 106] Zima, G. E. 301, 314, 775 [Z 4] Wilson, B. F. 709, 728 [C 155] Woolfolk, R. 345, 742 [J 29] Zink, H. 771 [V 15] Wilson, E. G. 345, 742 [J 30] Wooley, H. W. 353, 464, 467, 468, Ziolkowski 5 Wilson. E. J. 672, 721 [B 112] 469, 470, 772 [W 21, 37], 774 ZIetz, A. 331, 590, 705, 726 [C 92, Wilson, E. L. 480, 481, 487, 489, [W 98] 93,94,95],727 [C 110], 730 [D 64] 490, 763 [S 107] Worobjew, N. K. 275,286 775 [Z 12] Wilson, E. M. 573, 605, 618, 743 Wright, C. C. 471, 773 [W 44] Zolki, T. P. 575, 717 [A 20] [K 10], 773 [W 48, 50] Wright, P. G. 524, 734 [G 23] Zuber, N. 473, 775 [Z 2] Wilson, F. M. 357, 773 [W 67] Wrobel, J. R. 681, 774 [W 106] Zucrow, M. J. 685, 686, 688, 769 Wilson, G. L. 437, 772 [W 18] Wiinnenberg, E. 406, 719 [B 27] [T 22, 38], 775 [Z 5, 7] Wilson, J. N. 341, 774 [W 96] Wursthorn, A. M. 652, 774 Zupnik, T. F. 97, 98, 617, 724 Wilson, M. 556, 773 [W 49] [W90] [B 197] Wilson, R. G. 613, 773 [W 47] Wyatt, O. H. 461, 772 [W 33] Zwicky, F. 607, 775 [Z 9] Sachverzeichnis

Abbrand, erosiver 144 N-Aminoathylenimin 568 -, neutraler 119 Ammoniak 105, 225, 507 -, progressiver 119 -, Brennstoffmischungen mit 516 -, quasi-homogener 180 -, Hypergolisierung von 517 -, regressiver 119 -, monergole Treibstoffmischungen mit 594 Abbrandformeln, empirische 142, 173 - in monergolen Treibstoffmischungen 594 Abbrandgeschwindigkeit, Druckabhangigkeit, -, Umgang mit 514 Temperaturabhangigkeit 142, 146 Ammolliumllitrat 126, 129, 150, 170, 172 -, -, -, experimentellc Bestimmung 182 Ammoniumperchlorat 126, 150, 164, 170, 172, 174, -, -, - von Festtreibstoffen 119,142,145,167,261 460 -, -, - bei Lithergoltriebwerken 182, 185 Ammoniumpikrat 125 Abbrandgesetze bei Festtreibstoffen 142f., i 73 Ammonsalpeter, s. Ammoniumnitrat -- Lithergoltriebwerken 185 Anilin 105, 564 Abbrandkurven 146 Antibackmittel 130 Abbrandoberflache 119 Abbrandtheorien 157 Antriebe, elektrische 15 Abbrandtypen lithergoler Systeme 178 -, -, Energiequellen 23 Abschmelzkuhlung 35 -, -, Energiewandler 23 Accel-Decel-System 20 -, elektromagnetische 17 Acetylcn 103, 551 -, elektrostatische 19 Additions- und Kondensationsreaktionen von Mono- -, elektrothermische 15 meren 127 -, lithergole 178 Adiabatengleichung 57 Antriebsdauer 6 Adiabatenkoeffizient 56 Antriebswirkungsgrad 47, 48 Aerozin-50 104, 110, 117, 582 Arbeitsmasse 3 Athanol, s. Athylalkohol Arbeitsplatzkonzentration, maximale, s. MAK Athylalkohol 105, 552 Asphalt 153 Athylen 105 Asphaltcomposite 129 Athylencarbonat 605 ATLAS 37, 361, 624 Athylendiamin 255, 561 ATLAS-AGENA, s. auch AGENA 220 Athylenimin 560 ATLAS CENTAUR, s. auch CENTAUR 220, 472 Athylenoxyd 113, 114, 554 Atomc, metastabile 6 - als monergoler Treibstoff 602 Atomraketen 9 -, Zersetzungsreaktion von 603 Aufheizung, chemische 229 Athylnitrat 457 -, kernchemische 10 - als monergoler Treibstoff 609 -, konvektive 10 Athylpentaboran 588 -, durch Radioisotope 12 AGENA 684 Aushartung 132 Alkyldekaborane 589 Ausstromungsgeschwindigkeit 49, 61 Alkyldiborane 588 -, wirksame 49 Alkylnitrate als monergole Treibstoffe 609 Auswaschanlagen fur HF-Abgase 315 Alkylnitrite als monergole Treibstoffe 609 Alkylpentaborane 588 Ballistit 122 Allseitsbrenner 119 Bergmann-Junk-Probe 154 Allylamin 563 Beryllium 230, 231, 496 Aluminium als Zusatz zu flussigen Treibstoffen 229 -, toxische Eigenschaften von 497 ---- festen Treibstoffen 122, 130, 149, 214, -, Umgang mit 498 232 Berylliumhydrid 234, 235, 497 Aluminiumboranat 103, 506, 656 Beryllium-Verbindungell 231, 497 Aluminiumborhydrid, s. Aluminiumboranat Bildungswarmen von Oxyden und Fluoriden Aluminiumhydrid 507 (Tabelle) 224 798 Sachverzeichnis

Binder, gummielastische 152 Dekaboran 505 -, Herstellung 131 Desmophen 175 -, Leistullgserhohung beim 150, 233 DETA, s. Diiithylentriamin -, physikalische Eigenschaften 152, 174 Detonationsempfindlichkeit 273 -, thixotrope 174 DIAMANT 220 -, viskoelastische 174 Diathylamin 559 Bis-(2.2-dinitropropyl)formal 234 Diathyldekaboran 589 Bleiblock nach TRAUZL 273 Diathylentriamin 561, 695 BLUE STREAK 222 Diathylhydrazin, asymmetrisches 566 BN-Konzept 112, 224 -, symmetrisches 566 Bombe, ballistische (Bombenmethode nach GRIFFIN Diallylamin 563, 693, 696 und ANGELOFF) 114,265 Diboran 103, 105, 500 Bombenmethode nach KILPATRICK und BAKER, s. Di-n-butylhydrazin, asymmetrisches 566 Dreikolbenapparatur Dichte 114 Bor 500 Dichtebestimmung 277 Boran-Hydrazin -Kombinationen 112 Dichtungswerkstoffe 307, 328, 338, 357, 381, 400, Brennkammer (Feuergasgleichgewicht) 67, 79 413,447,479, 531, 579 -, Mischungs- und Verbrennungsvorgange 196 Dicyan 105, 557 Brennkammergeometrie 198 -, Verbrennung in Stickoxyden 674 BrennschluBgeschwindigkeiten (Tabelle) 32 Dicyanacetylen 105, 557 Brennstoffbinder 126 Dicyandiacetylen 557 Brennzeit 6 Diergole 99 -, effektive 146, 147 Diffusionsflamme 180 Brittle point 153 Difluoramino-Radikal (NF2-Radikal) 344 Brompentafluorid 110, 330 Difluordiazin 344 -, Treibstoffkombinationen mit 111, 638 1,2-Dihydrazinoathan 567 Bromtrifluorid 330 Diisopropylhydrazin, asymmetrisches 566 -, symmetrisches 566 Card-Gap-Test 154, 273 Dimazin, s. Dimethylhydrazin, asymmetrisches CENTAUR 472, 487, 488, 652, 653 Dimethylamin 558 Charakteristische Lange, s_ Lange, charakteristische Dimethylaminodiboran 590 Chlormonofluorid 324 N,N-Dimethylanilin 565 Chlorpentafluorid 110, 225, 329 Dimethylberyllium 234 -, Treibstoffkombinationen mit 110, 112, 225, 638, 1,2-Dimethyl-1,2-diazetidin 568 708 Dimethylhydrazin, asymmetrisches 105, 573 Chlortrifluorid 110, 225, 324 -, -, Analyse von 577 -, triergole Kombinationen mit 228 -, -, in monergolen Treibstoffen 595 -, Umgang mit 328 -, -, Treibstoffmischungen mit 581 -, Zweistoffkombinationen mit 633,707 -, -, Umgang mit 579 - zur Ziindung von Sauerstoff/Wasserstoff-Trieb- -, -, Zersetzung von 576 werken 653 -, symmetrisches 585 Chlortrifluorid/Ammoniak 636 -, Verbrennung in Stickstoffmonoxyd 674 Chlortrifluorid/Bor 709 Dipropargylhydrazin 567 Chlortrifluorid/Hydrazin 636 Di-n-propylhydrazin, asymmetrisches 566 Chlortrifluorid/Methan 635 Disauerstoffdifluorid 334 Chlortrifluorid/Pentaboran 635 Distickstoffpentoxyd 424 Chlortrifluorid/Wasserstoff 635 Distickstofftetrafluorid, s. Tetrafluorhydrazin Chlortrioxyfluorid 345 Distickstofftetroxyd 110, 406 -, Kombinationen mit 111, 638 -, Analyse von 411 COLBuRN-j-modulus 438 -, Baumaterialien fiir 412 Composite, s. Festtreibstoffe, heterogene -, lithergole Kombinationen mit 711 Composite-Double-Base-Festtreibstoffe 234 -, toxische Eigenschaften von 417 CORALIE 682 -, Treibstoffmischungen mit 418 CORPORAL 554 -, triergole Kombinationen mit 227 Crawfordbombe 261 -, Umgang mit 414 Cryogenics 100 -, Zweistoffkombinationen mit 675 C-Stoff 539, 673 Distickstofftetroxyd/Aerozin-50 680 Curing 131 Distickstofftetroxyd/Ammoniak 677 Distickstofftetroxyd/asymmetrisches Dimethyl- Dampfdruck (Zahlenwerte s. bei den einzelnen Sub• hydrazin 682 stanzen) 115 Distickstofftetroxyd/Hydrazin 678 Dampfdruckbestimmung 275 Distickstofftetroxyd/Kerosin 676 Dampfdruckkurve (Abbildungen bei den einzelnen Distickstofftetroxyd/Methan- Verbrennung 677 Substanzen) 274 Distickstofftetroxyd/Monomethylhydrazin 681 Dehnung 152 Distickstofftrioxyd 405 Sachverzeichnis 799

Di-tert-butylhydrazin, asymmetrisches 566 Festtreibstoffe, mehrbasige 121 Diverssche Lasung 99, 594 -, Oxydatoren 125, 459 Dreikolbenapparatur nach KILPATRICK und BAKER -, Sicherheit und Handhabung 154 255 -, Ziindung 155 Dreistoffsysteme, lithergole 179 -, Ziindverzug 156 Druckabfall-Periode, s. Abbrandkurve -, Zusatzeinspritzung von Oxydatoren 713 Druckaufbauperiode, s. Abbrandkurve Feuergasgleichgewicht in der Brennkammer 67, 79 Druckexponent, s. Verbrennungsindex Filmkiihlung 35, 208 Druckfarderung 34 Filmsieden 208 Diise, angepaBte 49 Flamme, granulare 168 Diisenauslegung 201 Flammenreaktionszone 158 Diisenformen 201 Flammentemperatur, adiabatische 161 Diisenhals 59 Flammenzone 162 DiisenquersclUlittsverhaltnis 53 -, vorgemischte 181 Diisentheorie 58 FLOX 107, 225, 321 Diisenwirkungsgrad 204 FLox/Cyanwasserstoff 625 DurchfluBmessung 314, 360, 491 FLOx/Kerosin 620 FLOx/Methan 619 E-D-Diise 203 Fliissigfluor, s. Fluor Einspritzsystem 193 Fliissigtreibstoffe 99 Elastizitat 152 -, chemische Eigenschaften 115 Elastizitatsmodul 152 -, einzelne Kombinationen, s. unter dem Substanz- ELDO-A 220 namen des Oxydators ELDo-Drittstufe 680 -, Handhabungssicherheit 115 ELDo-Tragerrakete 110 -, hochenergetische 100 EMERAUDE 688 -, konventionelle 100 Energie, innere, s. thermodynamische Funktionen -, kryogene 99, 100 -, nukleare 9 -, lagerbare 99 Energiesatz 55, 161 -, Leistungsdaten 100 Enthalpie, s. thermodynamische Funktionen -, mittelenergetische 100, 105 -, freie, s. thermodynamische Funktionen -, monergole 113, 590 Entropie, s. thermodynamische Funktionen -, physikalische Eigenschaften 114 Entropiebedingung 72 -, Preis und Beschaffung 117 Entspannung, isotherme 17 Fliissigkeitstriebwerk 34 Entspannungsvorgang in der Diise 71 Fliissigsauerstoff, s. Sauerstoff Ermiidungserscheinungen 153 Fluor 103, 105, 224, 289 Eulersche Gleichung 162 -, Analyse von 299 Expansionsverhaltnis, optimales 49 -, chemische Eigenschaften 298 Explosionsgrenzen 244 -, Herstellung 290 Explosionssicherheit von Festtreibstoffen 154 -, lithergole Kombinationen 706 -, Mischungen mit anderen Oxydatoren 321 F l-Motor 36 -, physikalische Eigenschaften 293 Fallhammermethode 273 -, triergole Kombinationen 227 Feinheitsbestimmung, mikroskopische 273 -, Toxizitat 321 Felder, gekreuzte 17 -, Umgang mit 301, 310 -, Vernichtung von 315,318 Felle 123 -, Zweistoffkombinationen 610 Feststoffabbrand, Theorie des 157 Fluor/Alkalimetalle 617 Feststofftriebwerk 39 Fluor/Ammoniak 626 Festtreibstoffe 118 Fluor/Bor 707 -, Abbrandtheorien 157, 166ff. Fluor/Diboran 617 -, Alterungsbestandigkeit 154 Fluor/Hydrazin 631 -, doppelbasige, s. homogene Fluor/Hydrazin und Ammoniakmischungen 628 -, Explosionssicherheit 154 Fluor/Lithium 617, 707 -, Festigkeitseigenschaften 153 Fluor/Lithiumhydrid 707 -, Handhabung 154 Fluor/Ozon mit Kerosin JP-4 625 -, heterogene 125 Fluor/Pentaboran 617 -, homogene (doppelbasige) 120 Fluor/Wasserstoff 614 -, hypergoles Ziindverfahren 714 Fluorhaltige, monergole Treibstoffe 610 -, Isolierung 156 Fluornitrat, s. Nitroxylfiuorid -, kolloidale, s. homogene -, Kosten von 156 Fluortrager 110, 225 -, Leistungsdaten 148 Fremdziindung 239 -, linear amorphe 129 Fiillstandsmessung 359, 490 -, mechanische Eigenschaften 152 Furfurylalkohol 553 800 Sachverzeichnis

Gaschromatographie 300, 327, 343, 355, 504, 529, Induktion 17 571, 578, 598 Inhibitoren 119 Gas-Core-Reaktoren 14 Inverse Lithergol-Kombinationen, s. Lithergol- Gasgleichung, s_ Zustandsgleichung kombinationen Gas61, s_ Kerosin Ionen-Antriebe 19 Gasstrahlen, Ziindung von 253 Ionenmotor 21 Gehausebindung 119 Ionenquellen 19 Gele, thixotrope 230 Isoketten 127 Geliermittel 230 Isolierung von Festtreibstoffen, s. Festtreibstoffe Geltriebwerke 44 Isopropenylacetylen 114 GEMINI 358 Isoteniskop 276 Geschwindigkeit, charakteristische 52, 64, 192 Geysir-Effekt 362 J 2-Motor 38 GieBpulverprozeB 124 JP -4, s. Kerosin Glas-Ubergangstemperatur 152 JUPITER-C 561 Gleichgewichtsbedingungen 80 Gleichgewichtskonstante 68, 80 KaIiumperchlorat 126 Gleichgewichtsstromung 72, 89 Katalysatoren, EinfIuB auf Ziindverzug 259 Gleichwertigkeitsverhaltnis 101 - in Festtreibstoffen 130 Grasshoff-Zahl471 - zur Hydrazinzersetzung 598 Giitefaktor 193 -- Wasserstoffperoxydzersetzung 592 - fiir o-p-Wasserstoffumwandlung 462 Hi-Motor 35 Kernverschmelzung 9 HeiBwasserrakete 3 Kerosin 541 Hemmstoffe 119 -, Hypergolisierung von 549 , Heterogene Treibstoffe, s. Festtreibstoffe, heterogene - mit Metallbeimischung 550 Heteroketten 127 Kerosole, s. Kerosin mit Metallbeimischung High Energy Fuels (HEF), s. Hochenergietreibstoffe Kettenexplosion 241, 243 Hochenergietreibstoffe, s. auch Fliissigtreibstoffe und KIWI-NERvA-Projekt, s. ROVER-KIWI-NERvA-Projekt Tribride 219, 223, 500, 586 Klemmung 146 Hochfrequenzionenquelle 21 Kornungskennlinie 271 Hochleistungstreibstoffe, s. Hochenergietreibstoffe Kombinationen, lithergole, s. Lithergolkombinationen Hoppler-Viskosimeter 279 -, triergole (tribride), s. Lithergolkombinationen Holland-Test 154 Kontinuitatsgleichung 56, 96, 160, 169 Homogene Treibstoffe, s. Festtreibstoffe, homogene Konvektionskoeffizient 115 Hookesches Gesetz 152 KorngroBenmessungen 267 Husten 143 Korrosion 302, 334, 412, 445 Hybridsysteme 178 Kriechverhalten 153 Hybridtriebwerke 45, 178, 231 Kryptontetrafluorid 345 Hydrazin 105. 107, 108, 110, 113, 114,225,520 Kiihleigenschaften 115 --, Baumaterialien fiir 530 Kiihlsysteme 206 - als monergolcr Treibstoff 595 Kiihlung, ablative 35, 209 -, Umgang mit 532 -, regenerative 34, 208 -, Zersetzung von 527 Hydrazin-Ammoniak-Mischungen 537 Lange, charakteristische 52, 199 Hydrazin-Analyse 528 Laufzeit 210 Hydrazin-AniIin-Mischungen 539 Laufzeitmodell 212 Hydrazin -Hydrazinnitrat-Mischungen 539 Lavaldiise 33, 58, 201 - als monergoler Treibstoff 600 -, konische 201 Hydrazinmononitrat 150 -, parabolische 201 Hydrazinnitrat 460 Laval-Ringdiise 204 Hydrazin/Pentaboran 705 LC-50 (Letalkonzentration) 321 Hydrazinperchlorat 460 LD-50 (Letaldosis) 321 Hydrazin-Triebwerke 598 Leichtmetalle 226 Hydrazinzersetzung, Katalysatoren fiir 598 Leichtmetallhydride 226 HydrazinzersetzungsfIamme 597 LeichtmetalIzusatze zu Festtreibstoffen 149, 234 Hydyne 561 Leistungsberechnung 66, 77 Hypergolisierung von Ammoniak durch Zusatz von -, graphische Losungsmethoden 82 Alkalimetallen 517 -, rechnerische Losungsmethoden 84 - von Brennstoffen durch UDMH 258 Leistungsbereiche verschiedener Festtreibstoff· Hypergolitat 116, 239, 700 Gruppen 148 - der wichtigsten Raumfahrtantriebe 27 Impuls, spezifischer 50, 61, 193 Leistungsdaten von Festtreibstoffen 148 -, volumspezifischer 51 -- Fliissigtreibstoffen 100 Impulsdichte 51 - Iithergoler Kombinationen 188 Sachverzeiehnis 801

Leistungserhohung bei Bindern 233 Monohexylhydrazin 566 --- festen Oxydatoren 233 Monomethylamin 558 -- heterogenen Pulvern 232 Monomethylhydrazin (MMH) 105, 108, 566, 568 - durch hochenergetische Treibstoffe 218 -, Analyse von 570 - bei homogenen Pulvern 232 -, :VIischungen mit 571 -- Weichmaehern 233 -, Umgang mit 571 Leistungsparameter 48 Monopropylhydrazin 566 Lewis-Zahl 164 Morpholin 560 Lithergolkombinationen 178, 706 M-Stoff 539, 552, 673 -, inverse 713 Myrol99 -, Leistungsdaten 188 Myrol-Tricbwerk 113 -, Theorie der Verbrennung 183 -, tribride (triergole) 179, 189,228,230 Lithergoltriebwerke 45 Nachbrennraum 182 Lithium 495 Natriumborhydrid 506 Lithiumaluminiumhydrid 507 ~atriumhydrid 507 Lithium-Ammoniak-System 517 Newton-Raphson-Verfahren 84 Lithiumborhydrid 506 NichtgleichgewichtsprozeB 72, 95, 231 Lithiumhydrid 216, 225, 495 Nitroathan 456 Lithiumperehlorat 126 Kitroalkane, Sauerstoffbilanz der 605 L6sungsmittel-Extrusionsverfahren 124 Nitrocellulose 120, 233 Losungsmittelverfahren 123 -, diehte 125 LOX, s. Sauerstoff -, globulare (spharische) 125,233 LOZ, s. Ozon Nitroglykol 121 Luftstrahlsieb 268 Nitroglyzerin 121 Nitromethan 113, 114,451 --, Anwendung von 607 Maehzahl M 57, 59 -, Explosion von 606 Magnesiumhydrid 507 - als moncrgoler Treibstoff 606 MAK (maximale Arbeitsplatzkonzentration) 321 Nitroniumperchlorat 126, 233 Massendurchsatz 5, 119 :Nitropropan 456 MassenfluBfaktor 52 Nitrosylfluorid 347 Massengesehwindigkeit 144 Nitroweiehmacher 234 Massenverhaltnis 5 Nitroxylfluorid 348 Massenwirkungsgesetz 67, 81 Nitrylfluorid 347 Mehrstufengerat 32 Nitrylperchlorat 460 Mesaabbrand 143 NOMAD 105, 632 Metallzusatzc zu Festtreibstoffen 213, 214, 235 Normbrennkammern 261, 263 Methylacetylen als monergoler Treibstoff 601 Normsiebe 268 Methylamin in monergolen Treibstoffen 595 NovA-Klasse 221 K-Methylanilin 565 N usseltzahl 207 Methylpentaboran 588 ~ utzlastverhaltnis 219, 222 Methylviolett-Probe 154 MHF-l, s. Monomethylhydrazin, Mischungen mit Open-Cup-Methode 248 Mikrobrennkammer 247,253,254 ORION 10 Mikromerograph 272 Oxydatoren fiir Festtreibstoffe, s. Festtreibstoffe Miniatur-Brennkammer, s. lVIikrobrennkammer OxydatoriiberschuBzahl 102 -:\Iinimalvolumen 199 Ozon 108, 225, 366 MnWTEMAN 41 - -, Detonation von fliissigem :n8 MIRAGE 110 -, -- - gasf6rmigem 376 MisehsaUl'e 255, 450 -, Herstellung von 367 Misehungsdauer bei der Compositherstellung 131 -, stationare Zersetzungsflamme von :n5 Misehungsverhaltnis 101 -, Umgang mit 381 -, EinfluB des auf den Ziindverzug 259 -, Zweistoffkombinationen mit (l06 -, st6chiometrisches 101 OzonjDicyan (lOl MMH, s. Monomethylhydrazin OzonjKerosin OOS MO:N, s. Distiekstofftetroxyd-Misehungen OzonjWasserstoff 6U7 Monergole 99, 590 Ozonfluorid 335 -, Leistungsdaten 113 - zlir Hypergolisierung von LOX O(l5 -, Priifungsmethoden 116 Monergol-Triebwerk 39 Monoathylamin 559 PE-Wolle 120 Monoathyldekaboran 589 Pentaboran 103, 503 Monoathylhydrazin 566 als Brennstoff fiir luftatmende Triebwerke 055 Monoallylamin 696 657 802 Sachverzeichnis

Pentaboran/Hydrazin 113, 705 Salpetersaure 110, 257, 427 Pentad-Einspritzsystem 194 -, Analyse von 442 PerchloryIfluorid, s. Chlortrioxyfluorid -, Baumaterialien fiir 444 Phasen, kondensierte in den Feuergasen 73, 74, 93 -, chemische Eigenschaften von 438 PHOEBUS 12 -, lithergole Kombinationen mit 711 Photonenantrieb 24 -, monergole Treibstoffmischungen mit 594 Photosedimentometer 272 -, rotrauchende 427, 443 Piperidin 560 -, rotrauchendejKerosin 683 Planpriifsieb 267 -, Umgang mit 448 Plasma 15 -, weil3rauchende 427, 442 Plastisol-Treibstoffe 129 -, Ziindverziige von TriathylaminjAnilin-Mischun- Plateauabbrand 143 gen mit 691 Plug Nozzle 203 -, Zweistoffkombinationen mit 682 Pockets 166 Salpetersaure/Athylalkohol 689 POL-Pulver 123 SalpetersaurejAthylenimin 695 POLARIS 40, 41 SalpetersaurejAmmoniak 684, 689 Polvora tribasica 122 SalpetersaurejAnilin 696 Polyathylen.Composite 151 Salpetersaure/Cyclopentadien 688 Polybutadien-Acrylesterharze 153 SalpetersaurejDiathylentriamin 695 Polybutadien-Acrylsaure-Polymere 130 Salpeter~aurejDiallylamin 696 Polyisobutylen 129, 153 Salpetersaurejasymmetrisches Dimethylhydrazin Polymere, linear amorphe 128 684,703 -, partiell kristalline 128 SalpetersaurejFurfurylalkohol 689 -, polykristalline 128 SalpetersaurejHydrazin 684, 702 -, vernetzte 128 SalpetersaurejKerosin 685 Polymerisation 127 SalpetersaurejKerosin, Hypergolisierung mit asym· PolysuIfid.(Thiokol)-Treibstoffe 129 metrischem Dimethylhydrazin 683 Polyurethan 129, 153 SalpetersaurejKerosin, Hypergolisierung durch Zu- Polyvinylchlorid 129 satz von Leichtmethylhydriden 687 POODLE 12, 238 SalpetersaurejMonoallylamin 696 Prandtlzahl 206 Salpetersaurejo. Toluidin 698 Propargylhydrazin 567 SalpetersaurejTriathylamin 691 Propinylhydrazin 567 SalpetersaurejVinylather (Visole) 689 n-Propylnitrat 457, 609 SalpetersaurejXylidin 699 Pulse-Motor 44 Salpetersaureanhydrid, s. Distickstoffpentoxyd Pulver, heterogene 125, 232 Sandwichmodell 169 -, homogene 120, 232 SATURN 37, 103,360,361,362,472,659 Pulverwolle 120 SATURN I 37, 220 Pumpenfiirderung 34 SATURN-S IV B-STUFE 472, 482, 652 Pyrrol563 SATURN V 37, 220 Sauerstoff 349 -, Analyse und Reinheitskontrolle von 355 Qualitatsfaktoren 192, 200 -, Baumaterialien fiir 356 Querschwingungen 210 -, Hypergolisierung durch Zusatz von Fluor 665 Querwellen 212 -, ---- Ozonfluorid 665 -, Leistungsdaten von Kombinationen mit 103 -, lithergole Kombinationen mit 709 Radialeinspritzsystem 195 -, Pentaboran 655 Radikale, freie 6 -, physikalische Eigenschaften von 349 Rakete, ideale 54, 192 -, triergole Kombinationen mit 226 Raketengrundgleichung 4 -, Umgang mit fliissigem 357 RANGER·Hydrazin. Triebwerk 598 -, Warmeiibergang an 354 Reaktionsgeschwindigkeit 72, 95 -, Zweistoffkombinationen mit 647 Rechenverfahren zur Bestimmung der Leistungsdaten SauerstoffjAcetylen 660 77 SauerstoffjAthylalkohol 660 Regenerativkiihlung 208 SauerstoffjAmmoniak 662 Reifung 124, 131 SauerstoffjButadiendicarbonsaurenitril 661 Reynoldzahl 207 SauerstoffjDiboran 654 RFNA, s. rotrauchende Salpetersaure SauerstoffjDicyan 661 RIFT 12 SauerstoffjDicyanacetylen 661 Ringhalsdiisen 203 SauerstoffjHydrazin 664 RL-l0 Motor 37 SauerstoffjHydyne 664 ROVER-KIWI-NERVA 10, 238 SauerstoffjKerosin 657 RP-l, s. auch Kerosin 107, 108 SauerstoffjKerosole 660 Sachverzeichnis 803

Sauerstoff/Methylacetylen 660 Stautemperatur 55 Sauerstoff/Plexiglas 709 Steigrohrsichter 269 Sauerstoff/Triathylaluminium 655 Sterninnenbrenner 119 Sauerstoff/Triathylbor 655 Stickstoffoxyde, Kombinationen mit 674 Sauerstoff/Wasserstoff 649 Stickstofftetroxyd, s. Distickstofftetroxyd Sauerstoff/Wasserstoff -Triebwerke, ka talytische Stickstofftrifluorid 110, 112, 225, 339 Ziindung von 654 -, Kombinationen mit 639 Sauerstoffdifluorid 103, 107, 225, 331 Stickstofftrioxyd 427 Sauerstoffdifluorid/Ammoniak und Hydrazin 645 Stirnbrenner 119 Sauerstoffdifluorid/Ammoniak, Zweistoffkombi- Storables 100 nationen mit 642, 644 Sto13empfindlichkeit 273 Sauerstoffdifluorid/Diboran 643 Strahlabliisung 202 Sauerstoffdifiluorid/Hydrazin 645 Strahlleistung, spezifische 6 Sauerstoffdifluorid/Monomethylhydrazin 646 Strahlneutralisierung (bei elektrostatischen Trieb- Sauerstoffdifl uorid/W asserstoff 643 werken) 20 Sauerstofftrager 109 Strangpressen von Festtreibstoffen 123, 130 Schadlichkeitsfaktor 505, 572 Striimung, erstarrte 72, 87 Schallgeschwindigkeit 57, 59, 89, 90, 92 -, Gleichgewichts- 72, 89 Schaumzone 159, 162 Stiitzmasse 3 Schichteneffekt 482 Stufenprinzip 31, 33 Schie13baumwolle 120 SURVEYOR 419, 681 Schleierkiihlung 35 Suspcnsionen von Metallpulvern 230 Schlierenoptik 251 Systeme, lithergole, s. Lithergolkombinationen Schmelzdiagramm 275 Schmelzpunkt 115, 274 Taliani-Test 154 Schmierstoffe 307, 328, 338, 357, 401, 414, 479, 514, Testanlage, geschlossene 232 579 Tetraathyldiboran 588 Schneckenpressenproze13 123 Tetrafluorhydrazin (Distickstofftetrafluorid) 110, 112, Schub 5, 48 225,342 -, effektiver 146 -, Kombinationen mit 640 Schubkoeffizient 52, 64, 193 Tetrafluorhydrazin/Hydrazin 641 Schubunterbrechung 179 N,N,N',N'-Tetramethyl-l,3-diaminobutan 563 Schub-Zeit-Diagramm 146 Tetramethyltetrazen 586 Schutzkleidung 311, 416, 450, 535 Tetranitromethan 113, 453 Schwingungen 210 - als monergoler Treibstoff 607 -, hochfrequente 212 -- Oxydator 705 -, niederfrequente 210, 213 Thermal layer 171 Schwitzkiihlung 208 Thermodynamische Funktionen, Formeln 78 SCOUT 41 -- von Verbrennungsprodukten, Zahlenwerte (Bei• S_D.-Pulver 122 spiele und Literaturangaben) 74 SDMH, s. Dimethylhydrazin, symmetrisches -- von Treibstoffen, s_ unter den Substanz- Sedimentationsanalyse 270 namen Sedimentationswaage 271 THOR 37 Selbstanpassung an den Au13endruck (Ringhals- TITAN-II 110, 413, 582, 584, 680 diisen) 204 TITAN-III C 220 Shell 405- Katalysator 598 TNM, s. Tetranitromethan Shrouded Plug Nozzle 204 TOFLOX, s. Ozonfluorid Siebanalyse 267 o-Toluidin 565 Siebenriihrenladung 119 TONKA 250, 692 Sieden, blasenfiirmiges, Filmsieden 208 Transportbehalter 311, 312, 356, 359, 365, 485 Siedepunkt 115, 224, 274 Treibsatzgeometrie 119 Slurry-Proze13 125 Treibstoffdichte, Einflu13 auf Triebwerksleistung 51, Sonnensegel 26 114,214 Spannungs-Dehnungs-Diagramm 152 Treibstoffe, doppelbasige, s. Festtreibstoffe Spike Nozzle 203 -, heterogene, s. Festtreibstoffe Spritzapparatur nach LUTZ 248 -, hochenergetische, s. Fliissigtreibstoffe und Lither- Spriihzone 162 golkombinationen Stabilisatoren 121 -, homogene, s. Festtreibstoffe Stabilitatspriifung (von Festtreibstoffen) 154 -, kolloidale, s. Festtreibstoffe Standardbedingungen fUr 18 100 -, konventionelle, s. Fliissigtreibstoffe Stanton-Zahl 207 -, kryogene, s. Fliissigtreibstoffe Start-Stop-Eigenschaft (von Lithergoltriebwerken) -, lager bare, s. Fliissigtreibstoffe 179 -, linear amorphe, s. Festtreibstoffe Staubfeuerung 230 -, mittelenergetische, s. Fliissigtreibstoffe Staudruck 55 -, pastiise 174 804 Sachverzeichnis

Treibstoffverbrauch, spezifischcr 51 Wasserstoff, Verfliissigung von 462 TrennkorngroBe 269 -, Warmeiibergang an 471 Triathylaluminium 590 Wasserstoffperoxyd 109, 113, 385 - zur Ziindung von Sauerstoff/Wasserstoff-Trieb- -, Analyse von 397 werken 653 -, Baumaterialien fiir 397 Triathylamin 559 -, Leistung als monergoler Treibstoff 591 Triathylamin-Xylidin-Misehungen 692 -, lithergole Kombinationen mit 709 Triathylbor 586 - als monergoler Treibstoff 590 B-Triathylborazol 589 -, triergoler Kombinationen mit 227 Triathyldekaboran 589 -, Umgang mit 401 Tribride, s_ Lithergolkombinationen, tribride -, Zersetzung von fliissigem 392, 590 Triergole, s. Lithergolkombinationen, tribride -, -- gasformigem 394ff. Trimethylamin 558 -, Zweistoffkombinationen mit 668 Trimethylbor 586 Wasserstoffperoxyd/.Athyldekaboran 671 1,2,3-Trimethyldiaziridin 568 Wasserstoffperoxyd/ Ammoniak 672 Tropfchenverbrennung 198 Wasserstoffperoxyd/Diboran 671 Tropfenmethode 247 Wasserstoffperoxyd/Hydrazin 672 T-Stoff 38;"). 674 Wasserstoffperoxyd/Kerosin 671 Wasserstoffperoxyd/Lithium 670 Wasserstoffperoxyd/Lithinmaluminiumhydrid 70) Uberschalldiisen 60 Wasserstoffperoxyd/Pentaboran 671 UDMH, s. Dimethylhydrazin, asymmetrisches Wasserstoffperoxyd/Polyathylen 710 Uranspaltung 9 Wasserstoffperoxyd/Trimethylbor 671 \Vasserstoffsuperoxyd, s. Wasserstoffperoxyd V 2 552, 593, 660 Weichmacher 121, 130, 234 Velocity, actual 49 -, Leistungserhohung bei 233 -, effective 49 WFNA, s. weiBrauchende Salpetersaure Verbrennungsgeschwindigkeit von Tropfchen 197 Windsichtnng 269 Verbrennungsindex (Druckexponent) 142, 146 Wirkungsgrad 45 Verbrennungsinstabilitaten 209, 239 -, auBerer 47 Verbrennungswirkungsgrad 181, 193 -, idealer 61 Verfahren ohne Losungsmittel 123 -, innerer 47 Vernetzung 128 -, thermischer- 47 Vernetzungsdichte 128 Wurfpriifsieb 267 VERONIQUE 110, 686, 688 Versprodungstemperatur 153 X-15 593, 648, 663 Viskoelastizitat 152 Xenondifluorid 345 Viskosimeter 279 Xenonhexafluorid 345 Viskositat 115, 279 Xenontetrafluorid 345 Yorbereitungszone 163 Xylidin 255, 565 Xylidin-Triathylamin-Mischungen 692, 694 Warme, spezifische, s. thermodynamische Funk- tionen Z-Stoff 385 Warmebilanz 72, 167 Zell nlose 120 Warmeexplosion 241 Zelluloseacetat 129 Warmeleitfiihigkeit (Zahlenwerte, s. unter den ein- Zigarettenabbrand 119 zelnen Substanznamen) 281 Zischzone 158, 162 Warmeleitfahigkeitskoeffizient 115 Ziindpartner, chemische Zusammensetzung der 257 Warmeleitfahigkeitsmessungen 280 Ziindreaktion, Katalysierung einer 259 Warmeleitungsgleichung 161, 162, 167, 169 Ziindtemperatur, spontane 143 Warmeriickfiihrungskoeffizient 206 Ziindung 239 Warmeiibergang 206 'n dcr festen Phase 155 - durch Konvektion 206 von Festtreibstoffen 155 W ALTER-Triebwerke 385, 593, 594, 673 in der Gasphase 155 Wanderwellenbeschleunigung 17 von Gasstrahlen 253 Wandler, thermionische 23 durch heterogene Reaktion 155 Wasserstoff 103, 105, 108, 225, 461 -, Schema des Temperaturverlaufs 245 -, atomarer 7 - bei Unterdruck 260 -, Baumaterialien fiir 476 Ziindverhalten 116 -, Herstellung von 461 Z(indverzug 146, 239 -, physikalische Eigenschaften 463 - von Aminen 700 -, tiefgekiihlter 483 -- - Brennstoffgemischen 258 -, Umgang mit f1iissigem 480 -, EinfluB von Druck, Temperatur und Mischungs- -, o-p-Umwandlung 462,463 verhaltnis 259 Sachverzeichnis 805

Ziindverzug, Einfluf3 von oberflachenaktiven Zusatzen Zugfestigkeit, maximale 152 261 Zugspannung 152 - von Festtreibstoffen 156 Zukunftsantriebe 4 -- - Gasen 253 Zusatze zu Festtreibstoffen, ballistische 121, 130 --. Messung, Dreikolbenapparatur 255 -- -, kalorische 130 -. --. Methode von PINO 247, 253 Zustandsgleichung fiir Festkorper 161 -. - . - der zusammengespritztenStrahlen 247,249 -- ideale Gase 56,77, 161 -, -. Tropfenmethode 247 -- Schaum 161 Ziindverzugsapparaturen 240 Zweiphasenstromung 73,93 Ziindvorgang 245 Zwittertriebwerke 178