Books on the topic 'Hybrid propellant rockets – Testing'

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

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.

Sati︠u︡kov, V. A. Tekhnologicheskai︠a︡ mekhanika toplivnykh magistraleĭ zhidkostnykh raketnykh dvigateleĭ. Moskva: Fizmatlit, 2009.

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, Space, and Technology. Subcommittee on Space Science and Applications. Tests of the redesigned solid rocket motor program: Hearing before the Subcommittee on Space Science and Applications of the Committee on Science, Space, and Technology, U.S. House of Representatives, One Hundredth Congress, second session, January 27, 1988. Washington: U.S. G.P.O., 1988.

United States. Congress. House. Committee on Science, Space, and Technology. Subcommittee on Space Science and Applications. Tests of the redesigned solid rocket motor program: Hearing before the Subcommittee on Space Science and Applications of the Committee on Science, Space, and Technology, U.S. House of Representatives, One Hundredth Congress, second session, January 27, 1988. Washington: U.S. G.P.O., 1988.

United States. Congress. House. Committee on Science, Space, and Technology. Subcommittee on Space Science and Applications. Tests of the redesigned solid rocket motor program: Hearing before the Subcommittee on Space Science and Applications of the Committee on Science, Space, and Technology, U.S. House of Representatives, One Hundredth Congress, second session, January 27, 1988. Washington: U.S. G.P.O., 1988.

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.

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.

Hybrid thermal control testing of a cryogenic propellant tank. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

(Editor), Martin J. Chiaverini, and Kenneth K. Kuo (Editor), eds. Fundamentals of Hybrid Rocket Combustion and Propulsion (Progress in Astronautics and Aeronautics). AIAA (American Institute of Aeronautics & Ast, 2007.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Space shuttle solid rocket booster main parachute damage reduction team report. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Space shuttle solid rocket booster main parachute damage reduction team report. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

Qualification motor no. 8 (QM-8) final test report. Brigham City, Utah: Morton Thiokol, Inc., Aerospace Group, Space Operations, 1989.

United States. National Aeronautics and Space Administration., ed. Long life testing of oxide-coated iridium/rhenium rockets. [Washington, DC]: National Aeronautics and Space Administration, 1995.