Books on the topic 'Solid propellant'

Xristin, Schad, and United States. National Aeronautics and Space Administration., eds. Propellant variability assessment. [Huntsville, Ala.]: Quality Engineering Research Laboratory, University of Alabama in Huntsville, 1991.

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

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Performance of rocket motors with metallized propellants: Report of the Propulsion and Energetics Panel Working Group 17. Neuilly sur Seine, France: AGARD, 1986.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Performance of Rocket Motors with Metallized Propellants: Report of the Propulsion and Energetics Panel : Working Group 17. S.l: s.n, 1986.

L, Boggs Thomas, Derr Ronald L, and Advisory Group for Aerospace Research and Development. Propulsion and Energetics Panel., eds. Hazard studies for solid propellant motors. Neuilly sur Seine: Agard, 1990.

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

G, Schirk P., and United States. National Aeronautics and Space Administration., eds. Facility design consideration for continuous mix production of class 1.3 propellant. [Washington, DC: National Aeronautics and Space Administration, 1994.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Design methods in solid rocket motors. Neuilly sur Seine, France: AGARD, 1988.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Design Methods in Solid Rocket Motors. S.l: s.n, 1987.

United States. National Aeronautics and Space Administration., ed. NASA's advanced solid rocket motor. [Washington, DC: National Aeronautics and Space Administration, 1993.

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.

Moore, Carleton J. SRM propellant and polymer materials structural modeling. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1988.

Langhenry, M. T. Acceleration effects in solid propellant rocket motors. New York: AIAA, 1986.

L, Derr Ronald, and North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development., eds. Hazard studies for solid propellant rocket motors. Neuilly-sur-Seine, France: AGARD, 1990.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Hazard studies for solid propellant rocket motors. Neuilly-sur-Seine: AGARD, 1990.

Roberts, F. E. Optical measurements on solid specimens of solid rocket motor exhaust and solid rocket motor slag. Huntsville, Ala: George C. Marshall Space Flight Center, 1991.

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

1885-1954, Jenkins Billy, and United States. National Aeronautics and Space Administration., eds. Complex burn region module (BRM) update: Final technical report for the period November 01 1989 through September 30, 1990. [Washington, DC: National Aeronautics and Space Administration, 1991.

United States. National Aeronautics and Space Administration., ed. Atomic hydrogen as a launch vehicle propellant. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.

T, Godai, and United States. National Aeronautics and Space Administration., eds. Studies of solid propellant combustion with pulsed radiography. Washington, DC: National Aeronautics and Space Administration, 1987.

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.

Hohmann, Carl. Propellant for the NASA standard initiator. Houston, Tex: National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, 2000.

Caroline, Richards Mary, Thiokol Corporation Space Operations, and George C. Marshall Space Flight Center., eds. RSRM-13 (360Q013) final report: Ballistics mass properties flight designation STS-41 / prepared for National Aeronautics and Space Administration, George C. Marshall Space Flight Center ; [prepared by Brian A. Laubacker, M.C. Richards. Brigham City, UT: Thiokol Corporation Space Operations, 1990.

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

Sabnis, J. S. Navier-Stokes analysis of two- and three-dimensional flow field in solid rocket motors with segment joints. New York: American Institute of Aeronautics and Astronautics, 1987.

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

McCrorie, J. David. Particle behavior in solid propellant rocket motors and plumes. Monterey, Calif: Naval Postgraduate School, 1992.

C, Richards M., Thiokol Corporation Space Operations, and George C. Marshall Space Flight Center., eds. RSRM-9 (360L009) final report: Ballistics mass properties. Brigham City, UT: Thiokol Corp., Space Operations, 1990.

C, Richards M., Thiokol Corporation Space Operations, and George C. Marshall Space Flight Center., eds. RSRM-9 (360L009) final report: Ballistics mass properties. Brigham City, UT: Thiokol Corp., Space Operations, 1990.

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

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

Hohmann, Carl. Viton's impact on NASA standard initiator propellant properties. Houston, Tex: National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, 2000.

Zurawski, Robert L. Analysis of quasi-hybrid solid rocket booster concepts for advanced earth-to-orbit vehicles. Cleveland, Ohio: Lewis Research Center, 1987.

C, Rapp Douglas, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., eds. Analysis of quasi-hybrid solid rocket booster concepts for advanced earth-to-orbit vehicles. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

C, Rapp Douglas, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., eds. Analysis of quasi-hybrid solid rocket booster concepts for advanced earth-to-orbit vehicles. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

C, Rapp Douglas, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., eds. Analysis of quasi-hybrid solid rocket booster concepts for advanced earth-to-orbit vehicles. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

M, Lipanov A., Milekhin I︠U︡ M, and Aliev A. V, eds. Vnutrenni︠a︡i︠a︡ ballistika RDTT. Moskva: Mashinostroenie, 2007.

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

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.

A, Stalnaker Winifred, and Langley Research Center, eds. Structural analysis of a bolted joint concept for the space shuttle's solid rocket motor casing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

Greatrix, D. R. Quasi-steady analysis of the internal ballistics of solid-propellant rocket motors. [S.l.]: [s.n.], 1987.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Terminology and assessment methods of solid propellant rocket exhaust signatures. Neuilly-sur-Seine, France: AGARD, 1993.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Propulsion and Energetics Panel. and North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Consultant and Exchange Programme., eds. Design methods in solid rocket motors. Neuilly sur Seine, France: North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Development, 1987.

Solanki, Niraj. Effect of external pulse on solid propellant rocket internal ballistics. Ottawa: National Library of Canada, 2000.

United States. National Aeronautics and Space Administration., ed. Plume particle collection and sizing from static firing of solid rocket motors. [Washington, D.C: National Aeronautics and Space Administration, 1995.

United States. National Aeronautics and Space Administration., ed. Plume particle collection and sizing from static firing of solid rocket motors. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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.

Greatrix, D. R. Erosive burning model for composite-propellant rocket motors with large length-to-diameter ratios. [S.l.]: [s.n.], 1987.