Libros sobre el tema "Solid Rocket Motors"

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.

Hovland, Douglas Lyle. Particle sizing in solid rocket motors. Monterey, California: Naval Postgraduate School, 1989.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Propulsion and Energetics Panel. y 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.

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

Xie, Kan, Xinmin Chen, Junwei Li y Yu Liu. Fluidic Nozzle Throats in Solid Rocket Motors. Singapore: Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-6439-6.

L, Derr Ronald y 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.

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

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

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.

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

A, Alvarado, Mathias E. C y United States. National Aeronautics and Space Administration., eds. Correlation of slag explusion with ballistic anomalies in shuttle solid rocket motors. [Washington, D.C: National Aeronautics and Space Administration, 1997.

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.

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

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.

Office, General Accounting. Space shuttle: NASA's procurement of solid rocket booster motors : report to the Administrator, National Aeronautics and Space Administration and the Secretary of the Air Force. Washington, D.C: The Office, 1986.

Office, General Accounting. Space shuttle: NASA's procurement of solid rocket booster motors : report to the Administrator, National Aeronautics and Space Administration and the Secretary of the Air Force. Washington, D.C: The Office, 1986.

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.

United States. General Accounting Office. National Security and International Affairs Division, ed. Advanced solid rocket motor status. Washington, D.C: The Office, 1993.

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

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Solid Rocket Motor Witness Test. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

Turner, J. E. A summary of laboratory testing performed to characterize an elastomeric O-ring material to be used in the redesigned solid rocket motors of the space transportation system. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1993.

Library of Congress. Congressional Research Service, ed. Proposed termination of the Advanced Solid Rocket Motor (ASRM) program. [Washington, D.C.]: Congressional Research Service, Library of Congress, 1992.

D, Smith S., Myruski Brian L y United States. National Aeronautics and Space Administration., eds. Radiation from advanced solid rocket motor plumes. Huntsville, AL: SECA, Inc., 1994.

D, Smith S., Myruski Brian L y United States. National Aeronautics and Space Administration., eds. Radiation from advanced solid rocket motor plumes. Huntsville, AL: SECA, Inc., 1994.

Card, Michael F. Structural behavior of solid rocket motor field joints. New York: American Institute of Aeronautics and Astronautics, 1987.

Powers, John P. Automatic particle sizing from rocket motor holograms. Monterey, Calif: Naval Postgraduate School, 1990.

Harold, Whitesides R. y United States. National Aeronautics and Space Administration., eds. Effects of slag ejection on solid rocket motor performance. Washington, D.C: American Institute of Aeronautics and Astronautics, 1995.

George C. Marshall Space Flight Center., ed. Determination of Solid Rocket Motor (SRM) case segment growth. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1986.

Racine, John A. Subscale solid rocket motor infrared signature and particle behavior. Monterey, Calif: Naval Postgraduate School, 1991.

H, Dunlap Patrick y NASA Glenn Research Center, eds. Development of thermal barriers for solid rocket motor nozzle joints. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Ice nucleus activity measurements of solid rocket motor exhaust particles. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, ed. Star 48 solid rocket motor nozzle analyses and instrumented firings. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

H, Dunlap Patrick y NASA Glenn Research Center, eds. Development of thermal barriers for solid rocket motor nozzle joints. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

United States. National Aeronautics and Space Administration, ed. Block II solid rocket motor (SRM) conceptual design study: Final report. Gainesville, Va: The Division, 1986.

United States. National Aeronautics and Space Administration., ed. The space shuttle advanced solid rocket motor: Quality control and testing. Washington, D.C: National Academy Press, 1991.

J, Gibeling H., McDonald Henry y United States. National Aeronautics and Space Administration., eds. Solid rocket motor aft field joint flow field analysis: Final ... report. Glastonbury, Conn: Scientific Research Associates, inc., 1988.

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.

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

John C. Stennis Space Center. y George C. Marshall Space Flight Center., eds. Supplemental final environmental impact statement: Space shuttle advanced solid rocket motor program. [Stennis Space Center, Miss.]: National Aeronautics and Space Administration, John C. Stennis Space Center, 1990.

A, Stalnaker Winifred y 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.

Ahmed, Rafiq. Cyclic loads tests of carbon involute solid rocket motor outer boot ring segments. Huntsville, Ala: Marshall Space Flight Center, 1988.

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.

B, Maxfield, Boucher C y United States. National Aeronautics and Space Administration., eds. 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.

G, Schirk P. y 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.