Books on the topic 'Rocket combustion'
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Dranovsky, Mark L. Combustion Instabilities in Liquid Rocket Engines. American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/4.866906.
Full textQuentmeyer, Richard J. Rocket combustion chamber life-enhancing design concepts. National Aeronautics and Space Administration, Lewis Research Center, 1990.
Find full textWang, Zhen-Guo. Internal Combustion Processes of Liquid Rocket Engines. John Wiley & Sons Singapore Pte Ltd, 2016. http://dx.doi.org/10.1002/9781118890035.
Full textNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Combustion of solid propellants. AGARD, 1991.
Find full textNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Combustion of solid propellants. AGARD, 1991.
Find full textGreen, James M. A premixed hydrogen/oxygen catalytic igniter. National Aeronautics and Space Administration, 1989.
Find full textDranovsky, Mark L. Combustion instabilities in liquid rocket engines: Testing and development practices in Russia. American Institute of Aeronautics and Astronautics, 2007.
Find full textEtele, Jason. Computational study of variable area ejector rocket flowfields. University of Toronto, Institute for Aerospace Studies], 2004.
Find full textArbib, H. A. Heavy hydrocarbon main injector technology program: Final report. Rocketdyne Division of Rockwell International Corporation, 1991.
Find full textGreatrix, David R. A study of combustion and flow behaviour in solid-propellant rocket motors. [Institute for Aerospace Studies], 1987.
Find full textGreatrix, D. R. A study of combustion and flow behaviour in solid-propellant rocket motors. Institute for Aerospace Studies, 1987.
Find full textJankowsky, Robert S. Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.
Find full textRocker, M. Modeling on nonacoustic combustion instability in simulations of hybrid motor tests. National Aeronautics and Space Administration, Marshall Space Flight Center, 2000.
Find full textMasters, Philip A. High-pressure calorimeter chamber tests for liquid oxygen/kerosene (LOX/RP-1) rocket combustion. Lewis Research Center, 1988.
Find full textWilliam, Brown. Orbit transfer rocket engine technology program: Enhanced heat transfer combustor technology : final report. NASA-Lewis Research Center, 1991.
Find full textQuentmeyer, Richard J. Hot-gas-side heat transfer characteristics of subscale, plug-nozzle rocket calorimeter chamber. Lewis Research Center, 1993.
Find full textJankovsky, Robert S. High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation. National Aeronautics and Space Administration, Glenn Research Center, 1999.
Find full textMeeting, JANNAF Combustion Subcommittee. 31st JANNAF Combustion Subcommittee meeting: Lockheed Missiles and Space Company, Sunnyvale, CA, 17-21 October 1994. Johns Hopkins University, Chemical Propulsion Information Agency, 1994.
Find full textYe ti huo jian fa dong ji ran shao guo cheng jian mo yu shu zhi fang zhen: Modeling and numerical simulations of internal combustion process of liquid rocket engines. Guo fang gong ye chu ban she, 2012.
Find full textCost, Thomas L. Engine data interpretation system (EDIS) (Phase II). National Aeronautics and Space Administration, 1991.
Find full textYe ti huo jian fa dong ji ran shao dong li xue mo xing yu shu zhi ji suan. Guo fang gong ye chu ban she, 2011.
Find full textArmstrong, Elizabeth S. Cooling of rocket thrust chambers with liquid oxygen. NASA, 1990.
Find full textArmstrong, Elizabeth S. Cooling of rocket thrust chambers with liquid oxygen. NASA, 1990.
Find full textMuss, J. A. User's manual for Rocket Combustor Interactive Design (ROCCID) and analysis computer program. The Center, 1991.
Find full textUnited States. National Aeronautics and Space Administration., ed. Combustion-wave ignition for rocket engines. National Aeronautics and Space Administration, 1992.
Find full textUnited States. National Aeronautics and Space Administration., ed. Combustion-wave ignition for rocket engines. National Aeronautics and Space Administration, 1992.
Find full textUnited States. National Aeronautics and Space Administration., ed. Combustion-wave ignition for rocket engines. National Aeronautics and Space Administration, 1992.
Find full textUnited States. National Aeronautics and Space Administration., ed. Solid rocket combustion simulator technology (using the hybrid rocket for simulation): Final report. University of Arizona, Engineering Experiment Station, College of Engineering and Mines, 1994.
Find full textP, Mercer Stewart, and United States. National Aeronautics and Space Administration., eds. ALS rocket engine combustion devices: Design and demonstration. Aerojet TechSystems, 1989.
Find full textUnited States. National Aeronautics and Space Administration., ed. Characteristics of vaporizing cryogenic sprays for rocket combustion modeling. National Aeronautics and Space Administration, 1994.
Find full textUnited States. National Aeronautics and Space Administration., ed. Powdered aluminum and oxygen rocket propellants: Subscale combustion experiments. National Aeronautics and Space Administration, 1993.
Find full textUnited States. National Aeronautics and Space Administration., ed. Characteristics of vaporizing cryogenic sprays for rocket combustion modeling. National Aeronautics and Space Administration, 1994.
Find full textEvaluation and improvement of liquid propellant rocket chugging analysis techniques, final report. National Aeronautics and Space Administration, 1988.
Find full textKratt, Aaron T. Numerical simulation of the ejector flowfield in a ram rocket engine with multiple rockets. 2004.
Find full textWang, Zhen-Guo. Internal Combustion Processes of Liquid Rocket Engines: Modeling and Numerical Simulations. Wiley & Sons, Incorporated, John, 2016.
Find full text(Editor), Martin J. Chiaverini, and Kenneth K. Kuo (Editor), eds. Fundamentals of Hybrid Rocket Combustion and Propulsion (Progress in Astronautics and Aeronautics). AIAA (American Institute of Aeronautics & Ast, 2007.
Find full textS, Zakany James, and United States. National Aeronautics and Space Administration., eds. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket combustion experiments. National Aeronautics and Space Administration, 1995.
Find full textS, Jankovsky Robert, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Structurally compliant rocket engine combustion chamber: Experimental and analytical validation. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.
Find full textYang, V. Liquid Rocket Engine Combustion Instability (Progress in Astronautics and Aeronautics). AIAA (American Institute of Aeronautics & Ast, 1995.
Find full textS, Zakany James, and United States. National Aeronautics and Space Administration., eds. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket combustion experiments. National Aeronautics and Space Administration, 1995.
Find full textEffect of model selection on combustor performance and stability predictions using ROCCID. National Aeronautics and Space Administration, 1992.
Find full textJ, Schneider Steven, and United States. National Aeronautics and Space Administration., eds. Testing of wrought iridium/chemical vapor deposition rhenium rocket. National Aeronautics and Space Administration, 1997.
Find full textJ, Schneider Steven, and United States. National Aeronautics and Space Administration., eds. Testing of wrought iridium/chemical vapor deposition rhenium rocket. National Aeronautics and Space Administration, 1997.
Find full text1926-, Rosenberg S. D., and Lewis Research Center, eds. Hydrocarbon-fuel/combustion-chamber-liner materials compatibility: Final report. GenCorp, Aerojet, 1991.
Find full textMixing fuel particles for space combustion research using acoustics. National Aeronautics and Space Administration, 1988.
Find full textHydrocarbon-fuel/combustion-chamber-liner materials compatibility: Final report. GenCorp, Aerojet, 1991.
Find full textEtele, Jason. Computational study of variable area ejector rocket flowfields. 2004.
Find full textHeat transfer in rocket engine combustion chambers and regeneratively cooled nozzles. SECA, Inc., 1993.
Find full textHeat transfer in rocket engine combustion chambers and regeneratively cooled nozzles. SECA, Inc., 1993.
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