Books on the topic 'Composite propellant'
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Greatrix, D. R. Normal acceleration model for composite-propellant combustion. [S.l.]: [s.n.], 1988.
Find full textGreatrix, D. R. A model for normal acceleration effects on composite propellant combustion. [S.l.]: [s.n.], 1989.
Find full textDrendel, Albert S. RSRM-9 (360L009) final report: Ballistics mass properties. Brigham City, UT: Thiokol Corp., Space Operations, 1990.
Find full textGreatrix, D. R. Erosive burning model for composite-propellant rocket motors with large length-to-diameter ratios. [S.l.]: [s.n.], 1987.
Find full textAhmed, Rafiq. Loads analysis and testing of flight configuration solid rocket motor outer boot ring segments. Huntsville, Ala: George C. Marshall Space Flight Center, 1990.
Find full textGill, M. TP-H1148 knitline integrity evaluation: Final report. Brigham City, UT: Thiokol Corp., Space Operations, 1990.
Find full textGill, M. TP-H1148 knitline integrity evaluation: Final report. Brigham City, UT: Thiokol Corp., Space Operations, 1990.
Find full textComposite propellant technology research: Mechanical property characterization : semi-annual report. Huntsville, Ala: Dept. of Mechanical Engineering, College of Engineering, University of Alabama in Huntsville, 1991.
Find full textC, 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.
Find full textC, 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.
Find full textKumar, Ramohalli, and United States. National Aeronautics and Space Administration., eds. Composite solid propellant predictability and quality assurance: Meeting report, April 21, 1989. Tucson, Ariz: University of Arizona, 1989.
Find full textUnited States. National Aeronautics and Space Administration., ed. Trade study plan for reusable hydrogen composite tank system (RHCTS). [Downey, Calif.]: Rockwell Aerospace, Space Systems Division, 1994.
Find full textMilestone 4: Test plan for reusable hydrogen composite tank system (RHCTS) : task 3, composite tank materials. [Downey, Calif.]: Rockwell Aerospace, Space Systems Division, 1994.
Find full textUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Pocketing mechanics of SRM nozzle liner. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Find full textUnited States. National Aeronautics and Space Administration., ed. Milestone 4: Thrust structure concepts & IHM screening graphite composite primary structure (GCPS). [Downey, Calif.]: Rockwell Aerospace, Space Systems Division, 1994.
Find full textUnited States. National Aeronautics and Space Administration., ed. Milestone 4: Thrust structure concepts & IHM screening graphite composite primary structure (GCPS). [Downey, Calif.]: Rockwell Aerospace, Space Systems Division, 1994.
Find full textA, Talay Theodore, Austin R. Eugene, and United States. National Aeronautics and Space Administration., eds. Reusable Launch Vehicle Technology Program. Paris, France: American International Astronautical Federation, 1996.
Find full textBerner, Milko K. Composite Solid Rocket Propellants: Composition, Chemistry and Technology. Wiley & Sons, Limited, John, 2014.
Find full textBerner, Milko K. Composite Solid Rocket Propellants: Composition, Chemistry and Technology. Wiley & Sons, Incorporated, John, 2021.
Find full textS, Gant Frederick, and United States. National Aeronautics and Space Administration., eds. Stress relaxation functions: Methods of approximation:final report. Huntsville, Ala: Dept. of Mechanical and Aerospace Engineering, The University of Alabama in Huntsville, 1994.
Find full textUnited States. National Aeronautics and Space Administration., ed. A rocket engine for Mars sample return using in situ propellants. [Washington, DC]: National Aeronautics and Space Administration, 1997.
Find full textUnited States. National Aeronautics and Space Administration., ed. A rocket engine for Mars sample return using in situ propellants. [Washington, DC]: National Aeronautics and Space Administration, 1997.
Find full textUnited States. National Aeronautics and Space Administration., ed. A rocket engine for Mars sample return using in situ propellants. [Washington, DC]: National Aeronautics and Space Administration, 1997.
Find full textTP-H1148 knitline integrity evaluation: Final report. Brigham City, UT: Thiokol Corp., Space Operations, 1990.
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