Libri sul tema "Solid propellant"

Xristin, Schad, e United States. National Aeronautics and Space Administration., a cura di. 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 e Advisory Group for Aerospace Research and Development. Propulsion and Energetics Panel., a cura di. 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., e United States. National Aeronautics and Space Administration., a cura di. 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., a cura di. 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, e North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development., a cura di. 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, e United States. National Aeronautics and Space Administration., a cura di. 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., a cura di. Atomic hydrogen as a launch vehicle propellant. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.

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

Vigor, Yang, Brill Thomas B, Ren Wu-Zhen e Zarchan Paul, a cura di. 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 e George C. Marshall Space Flight Center., a cura di. 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 e George C. Marshall Space Flight Center., a cura di. RSRM-9 (360L009) final report: Ballistics mass properties. Brigham City, UT: Thiokol Corp., Space Operations, 1990.

C, Richards M., Thiokol Corporation Space Operations e George C. Marshall Space Flight Center., a cura di. 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, e United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., a cura di. 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, e United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., a cura di. 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, e United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., a cura di. 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 e Aliev A. V, a cura di. 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., a cura di. 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., a cura di. 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, e Langley Research Center, a cura di. 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. e North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Consultant and Exchange Programme., a cura di. 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., a cura di. 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., a cura di. 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.