Books on the topic 'Solid propellant rockets Combustion'

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Combustion of solid propellants. Neuilly sur Seine, France: AGARD, 1991.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Combustion of solid propellants. Neuilly sur Seine, France: AGARD, 1991.

Meeting, JANNAF Combustion Subcommittee. 31st JANNAF Combustion Subcommittee meeting: Lockheed Missiles and Space Company, Sunnyvale, CA, 17-21 October 1994. Columbia, MD: Johns Hopkins University, Chemical Propulsion Information Agency, 1994.

Greatrix, David R. A study of combustion and flow behaviour in solid-propellant rocket motors. [Downsview, Ont.]: [Institute for Aerospace Studies], 1987.

Greatrix, D. R. A study of combustion and flow behaviour in solid-propellant rocket motors. [Downsview, Ont.]: Institute for Aerospace Studies, 1987.

Riehl, John. SRM-assisted trajectory for the GTX reference vehicle. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2002.

K, Kuo Kenneth, and Pein Roland, eds. Combustion of Boron-based solid propellants and solid fuels. Boca Raton: Begell House/CRC Press, 1992.

Butler, Albert George. Holographic investigation of solid propellant combustion. Monterey, Calif: Naval Postgraduate School, 1988.

Kalinin, V. V. Nestat͡s︡ionarnye prot͡s︡essy i metody proektirovanii͡a︡ uzlov RDTT. Moskva: "Mashinostroenie", 1986.

Jiao long hou tian: Jie du gu ti huo jian fa dong ji mi wen = Jiaolong houtian. Beijing Shi: Zhongguo yu hang chu ban she, 2007.

Gu ti huo jian fa dong ji yuan li. [Peking]: Guo fang gong ye chu ban she, 1985.

Gu ti huo jian chong ya zu he fa dong ji: Integral solid propellant ramjet rocket motor. Beijing Shi: Zhongguo yu hang chu ban she, 2006.

Kishore, K. Solid propellant chemistry: Condensed phase behaviour of ammonium perchlorate-based solid propellants. New Delhi: Defence Research & Development Organisation, Ministry of Defence, 1999.

Greatrix, D. R. A model for normal acceleration effects on composite propellant combustion. [S.l.]: [s.n.], 1989.

Gu ti huo jian fa dong ji shi yong gong cheng. Beijing Shi: Guo fang gong ye chu ban she, 2010.

Gu ti huo jian fa dong ji yuan li. Beijing Shi: Guo fang gong ye chu ban she, 2013.

Shishkov, Alʹbert Alekseevich. Rabochie prot͡s︡essy v raketnykh dvigateli͡a︡kh tverdogo topliva: Spravochnik. Moskva: "Mashinostroenie", 1989.

Duo guan huo jian fa she dong li xue fang zhen yu shi yan ce shi fang fa: Simulation and test methods of launch dynamics of multiple launch rocket system. Beijing: Guo fang gong ye chu ban she, 2003.

Chung, T. J. Development of a computerized analysis for solid propellant combustion instability with turbulence. [Washington, DC: National Aeronautics and Space Administration, 1988.

Office, General Accounting. Solid rocket motors: Loss of oxidizer production necessitates emergency allocation procedures : report to the Chairman, Committee on Government Operations, House of Representatives. Washington, D.C: The Office, 1988.

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

Berger, F. C. Heat transfer from propellant burning in a constant-volume chamber. [Downsview, Ont.]: Department of Aerospace Science and Engineering, University of Toronto, 1990.

Hockgraver, Valerie Ruth. Implementation of ImageActionplus software for improved image analysis of solid propellant combustion holograms. Monterey, Calif: Naval Postgraduate School, 1989.

Chung, T. J. Development of computerized analysis for solid propellant combustion (ISAP-2): Semi-annual report. Huntsville, Ala: NASA/MSFC, 1987.

Lee, Yeaw-Lip. Particle-sizing system fro scanning electron microscope images of solid-propellant combustion exhaust. Monterey, Calif: Naval Postgraduate School, 1991.

Teori͡ia vnutrikamernykh pro͡tsessov i proektirovanie RDTT. Moskva: Mashinostroenie, 1991.

Gu ti huo jian fa dong ji ji suan ji fu zhu she ji. Beijing: Beijing hang kong hang tian da xue chu ban she, 1996.

Schobert, Detlef. Aluminiunmoxid-Belastung nideriger Erdumlaufbahnen durch feststoffraketengestützte Plazierung geostationärer Satelliten. München: Utz, Wissenschaft, 1996.

Rocker, M. Modeling on nonacoustic combustion instability in simulations of hybrid motor tests. Marshall Space Flight Center, Ala: National Aeronautics and Space Administration, Marshall Space Flight Center, 2000.

Passman, James A. Flight set 360T004 (STS-30). Brigham City, Utah: Morton Thiokol, Inc., Aerospace Group, Space Operations, 1989.

Passman, James A. Flight set 360T004 (STS-30). Brigham City, Utah: Morton Thiokol, Inc., Aerospace Group, Space Operations, 1989.

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.

Xiaosong, Wu, Chen Jun, and Wang Dong, eds. Gu ti huo jian fa dong ji qi ti dong li xue. Beijing Shi: Guo fang gong ye chu ban she, 2005.

Drendel, Albert S. RSRM-9 (360L009) final report: Ballistics mass properties. Brigham City, UT: Thiokol Corp., Space Operations, 1990.

Schulze, N. Flight demonstration of flight termination system and solid rocket motor ignition using semiconductor laser initiated ordnance. Washington, D.C: American Institute of Aeronautics and Astronautics, 1995.

Ye ti huo jian fa dong ji ran shao dong li xue mo xing yu shu zhi ji suan. Beijing Shi: Guo fang gong ye chu ban she, 2011.

United States. Congress. House. Committee on Science and Technology. Subcommittee on Space Science and Applications. Strategy for safely returning space shuttle to flight status: Hearing before the Subcommittee on Space Science and Applications of the Committee on Science and Technology, House of Representatives, Ninety-ninth Congress, second session, May 15, 1986. Washington: U.S. G.P.O., 1986.

United States. Congress. House. Committee on Science and Technology. Subcommittee on Space Science and Applications. Strategy for safely returning space shuttle to flight status: Hearing before the Subcommittee on Space Science and Applications of the Committee on Science and Technology, House of Representatives, Ninety-ninth Congress, second session, May 15, 1986. Washington: U.S. G.P.O., 1986.

Applications, United States Congress House Committee on Science and Technology Subcommittee on Space Science and. Strategy for safely returning space shuttle to flight status: Hearing before the Subcommittee on Space Science and Applications of the Committee on Science and Technology, House of Representatives, Ninety-ninth Congress, second session, May 15, 1986. Washington: U.S. G.P.O., 1986.

United States. Congress. House. Committee on Science, Space, and Technology. Subcommittee on Space Science and Applications. Results of the development motor 8 test firing: Hearing before the Subcommittee on Space Science and Applications of the Committee on Science, Space, and Technology, House of Representatives, One Hundredth Congress, first session, September 16, 1987. Washington: U.S. G.P.O., 1987.

United States. Congress. House. Committee on Science and Technology. Investigation of the Challenger accident: Report of the Committee on Science and Technology, House of Representatives, Ninety-ninth Congress, second session. Washington: U.S. G.P.O., 1986.

Vigor, Yang, Brill Thomas B, Ren Wu-Zhen, and Zarchan Paul, eds. Solid propellant chemistry, combustion, and motor interior ballistics. Reston, Va: American Institute of Aeronautics and Astronautics, 2000.

Brill, Thomas B., and Wu-Zhen Ren. Solid Propellant Chemistry Combustion and Motor Interior Ballistics 1999 (Progress in Astronautics and Aeronautics). AIAA (American Institute of Aeronautics & Ast, 2000.

Plume diagnostics of the RSRM static firings for the pressure perturbation studies. [Washington, D.C: National Aeronautics and Space Administration, 1995.

Greatrix, David Robert. A study of combustion and flow behaviour in solid-propellant rocket motors. 1987.

Roy, Gabriel D. Advances in Chemical Propulsion: Science to Technology. Taylor & Francis Group, 2001.

Roy, Gabriel D. Advances in Chemical Propulsion: Science to Technology (Environmental & Energy Engineering). CRC, 2001.

D, Roy G., ed. Advances in chemical propulsion: Science to technology. Boca Raton, FL: CRC Press, 2002.

Walker, J. D. Holographic investigation of metallized solid propellant combustion in two-dimensional and three-dimensional rocket motors. 1987.

SRM-assisted trajectory for the GTX reference vehicle. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2002.