Books on the topic 'Liquid Propellant Rocket'

Sutton, George Paul. History of liquid propellant rocket engines. Reston, Va: American Institute of Aeronautics and Astronautics, 2006.

de Iaco Veris, Alessandro. Fundamental Concepts of Liquid-Propellant Rocket Engines. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-54704-2.

Turbopumps for liquid rocket engines. [Warrendale, PA: Society of Automotive Engineers, 1992.

D, Cruit W., Smith A. W, George C. Marshall Space Flight Center., and AIAA/ASME/SAE/ASEE Joint Propulsion Conference (32nd : 1996 : Lake Buena Vista, Fla.), eds. Cold-flow study of hybrid rocket motor flow dynamics. [Huntsville, AL]: NASA Marshall Space Flight Center, 1996.

United States. National Aeronautics and Space Administration., ed. Propellant injection systems and processes. [Washington, DC: National Aeronautics and Space Administration, 1995.

Bian tui li ye ti huo jian fa dong ji ji qi kong zhi ji shu: Variable thrust liquid propellant rocket engine and its control techniques. Beijing: Guo fang gong ye chu ban she, 2001.

1965-, Liu Kun, and Cheng Mousen 1971-, eds. Ye ti huo jian fa dong ji dong li xue li lun yu ying yong. Beijing: Ke xue chu ban she, 2005.

Bian tui li ye ti huo jian fa dong ji ji qi kong zhi ji shu: Variable thrust liquid propellant rocket engine and its control techniques. Beijing: Guo fang gong ye chu ban she, 2001.

1965-, Liu Kun, and Cheng Mousen 1971-, eds. Ye ti huo jian fa dong ji dong li xue li lun yu ying yong. Beijing: Ke xue chu ban she, 2005.

Ye ti huo jian tui jin zeng ya shu song xi tong: Liquid rocket propellant and pressurization feed systems. Beijing: Guo fang gong ye chu ban she, 2007.

1920-, Huang David H., and Arbit Harry, eds. Modern engineering for design of liquid-propellant rocket engines. Washington, D.C: American Institute of Aeronautics and Astronautics, 1992.

Oldrich, Machacek, North Atlantic Treaty Organization. Scientific Affairs Division., and NATO Advanced Research Workshop on Application of Demilitarized Gun and Rocket Propellants in Commercial Explosives (1999 : Krasnoarmeĭsk, Saratovskai͡a oblastʹ, Russia), eds. Application of demilitarized gun and rocket propellants in commercial explosives. Dordrecht: Kluwer Academic Publishers, 2000.

L, Bickford R., Duncan David B, and United States. National Aeronautics and Space Administration., eds. An overview of in-flight plume diagnostics for rocket engines. [Washington, DC]: National Aeronautics and Space Administration, 1992.

L, Bickford R., Duncan D. B, and United States. National Aeronautics and Space Administration., eds. An overview of in-flight plume diagnostics for rocket engines. [Washington, DC]: National Aeronautics and Space Administration, 1992.

L, Bickford R., Duncan David B, and United States. National Aeronautics and Space Administration., eds. An overview of in-flight plume diagnostics for rocket engines. [Washington, DC]: National Aeronautics and Space Administration, 1992.

Ronald, De Hoff, and Lewis Research Center, eds. Development of life prediction capabilities for liquid propellant rocket engines: Diagnostic system architecture study : final report. Sacramento, Calif: GenCorp, Aerojet Propulsion Division, 1991.

United States. National Aeronautics and Space Administration., ed. Carbon monoxide and oxygen combustion experiments: A demonstration of Mars in situ propellants. [Washington, D.C.]: National Aeronautics and Space Administration, 1991.

Kanda, Takeshi. Effect of regenerative cooling on rocket engine specific impulse. Tokyo: National Aerospace Laboratory, 1993.

D, Cruit W., Smith A. W, and George C. Marshall Space Flight Center., eds. Cold-flow study of hybrid rocket motor flow dynamics: 32nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, July 1-3, 1996, Lake Buena Vista, FL. [Huntsville, Ala: NASA Marshall Space Flight Center, 1996.

D, Cruit W., Smith A. W, and George C. Marshall Space Flight Center., eds. Cold-flow study of hybrid rocket motor flow dynamics: 32nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, July 1-3, 1996, Lake Buena Vista, FL. [Huntsville, Ala: NASA Marshall Space Flight Center, 1996.

NATO Advanced Research Workshop on the Conversion of Liquid Rocket Fuels (2003 Baku, Azerbaijan). The conversion of liquid rocket fuels: Risk assessment, technology and treatment options for the conversion of abandoned liquid ballistic missile propellants (fuels and oxidizers) in Azerbaijan / edited by Wolfgang P.W. Spyra and Kay Winkelmann. Dordrecht: Kluwer Academic Publishers, 2004.

Ye ti huo jian fa dong ji ke kao xing. Beijing: Zhongguo yu hang chu ban she, 2014.

Grigorʹevich, Barʹi͡a︡khtar Viktor, Rosendorfer Theo, and NATO Advanced Research Workshop on Demilitarisation of Conventional Munitions and Rocket Propellants and Reuse and Recycling Concepts (1995 : Kiev, Ukraine), eds. Demilitarisation of munitions: Reuse and recycling concepts for conventional munitions and rocket propellants. Dordrecht: Kluwer Academic Publishers, 1997.

Chato, David J. Ground testing on the nonvented fill method of orbital propellant transfer: Results of initial test series. [Washington, D.C.]: National Aeronautics and Space Administration, 1991.

Dawson, Virginia P. Taming liquid hydrogen: The Centaur upper stage rocket, 1958-2002. Washington, D.C: National Aeronautics and Space Administration, Office of External Relations, 2004.

Lim, Kair Chuan. Evaluation and improvement of liquid propellant rocket chugging analysis techniques.: Final report. [Washington, DC: National Aeronautics and Space Administration, 1988.

Williams, R. W. Tenth Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion: Proceedings of a workshop held at NASA George C. Marshall Space Flight Center, Huntsville, Alabama, April 28-30, 1992. Marshall Space Flight Center, Alabama: George C. Marshall Space Flight Center, 1992.

Zhen tian jing lei: Qing ting ye ti huo jian fa dong ji de hong ming = Zhentian jinglei. Beijing Shi: Zhongguo yu hang chu ban she, 2007.

George C. Marshall Space Flight Center., ed. STS propellant densification feasibility study data book. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1994.

Ye ti huo jian fa dong ji te zhong zhi zao ji shu. Beijing: Zhongguo yu hang chu ban she, 2014.

Ye ti huo jian fa dong ji xian dai gong cheng she ji. Beijing shi: Zhongguo yu hang chu ban she, 2004.

Ke chong fu shi yong ye ti huo jian fa dong ji jian sun kong zhi li lun yu fang fa. Beijing: Ke xue chu ban she, 2013.

Ye ti huo jian fa dong ji xian dai gong cheng she ji. Beijing shi: Zhongguo yu hang chu ban she, 2004.

author, Tian Gan, Xu Zhigao author, and Yang Zhengwei author, eds. Ye ti dao dan fa dong ji gu zhang te xing fen xi yu zhen duan: Failure Characteristics Analysis and Fault diagnosis for Liquid Missile Engine. Beijing Shi: Guo fang gong ye chu ban she, 2014.

Dranovsky, Mark L. Combustion instabilities in liquid rocket engines: Testing and development practices in Russia. Reston, Va: American Institute of Aeronautics and Astronautics, 2007.

W, Armstrong, and United States. National Aeronautics and Space Administration., eds. PC programs for the prediction of the linear stability behavior of liquid propellant propulsion systems and application to current MSFC rocket engine test progams. [Huntsville, Ala.]: Research Institute, The University of Alabama in Huntsville, 1990.

Armstrong, Elizabeth S. Cooling of rocket thrust chambers with liquid oxygen. [Washington, D.C.]: NASA, 1990.

Armstrong, Elizabeth S. Cooling of rocket thrust chambers with liquid oxygen. [Washington, D.C.]: NASA, 1990.

United States. National Aeronautics and Space Administration., ed. Advanced small rocket chambers option II: Fundamental processes and material evaluation : final report. [Washington, DC]: National Aeronautics and Space Administration, 1993.

Liquid Rocket Propulsion History Colloquium (1989 Los Angeles, Calif.). History of liquid rocket engine development in the United States, 1955-1980: Liquid Rocket Propulsion History Colloquium, AAS Annual Meeting, Los Angeles, 1989 : proceedings of an AAS history colloquium. Edited by Doyle Stephen E, American Astronautical Society, and AAS Meeting (1989 : Los Angeles, Calif.). San Diego, Calif: Published for the American Astronautical Society by Univelt, 1992.

Goddard, Robert Hutchings. Rockets. Reston, Va: American Institute of Aeronautics and Astronautics, 2002.

Ye ti huo jian fa dong ji tui li shi she ji: Design for Thrust Chamber of Liquid Propellant Rocket Engines. Beijing Shi: Guo fang gong ye chu ban she, 2014.

Ye ti huo jian fa dong ji ran shao guo cheng jian mo yu shu zhi fang zhen: Modeling and numerical simulations of internal combustion process of liquid rocket engines. Beijing: Guo fang gong ye chu ban she, 2012.

Bryan, Palaszewski, O'Leary Robert, and Lewis Research Center, eds. Preliminary assessment of using gelled and hybrid propellant propulsion for VTOL/SSTO launch systems. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

S, Zakany James, and United States. National Aeronautics and Space Administration., eds. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket combustion experiments. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

J, Breisacher Kevin, and United States. National Aeronautics and Space Administration., eds. A comparison of analytical results for 20 K LOX/hydrogen instabilities. [Washington, D.C.]: NASA, 1990.

J, Breisacher Kevin, and United States. National Aeronautics and Space Administration., eds. A comparison of analytical results for 20 K LOX/hydrogen instabilities. [Washington, D.C.]: NASA, 1990.

P, Skowronski Raymund, and United States. National Aeronautics and Space Administration., eds. Investigation of cleanliness verification techniques for rocket engine hardware. [Washington, DC: National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration., ed. Developments in REDES: The rocket engine design expert system. [Washington, DC]: National Aeronautics and Space Administration, 1990.

P, Skowronski Raymund, and United States. National Aeronautics and Space Administration., eds. Investigation of cleanliness verification techniques for rocket engine hardware. [Washington, DC: National Aeronautics and Space Administration, 1994.