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