Results 81 to 90 of about 39,486 (297)
, 2017 Focusing on Liquid Propellant Rocket Engine (LPRE) major components, a steady state modular simulation software has been established in MATLAB Simulink. For integrated system analysis, a new algorithm dependant on engine inlet mass flow rate and pressure
M. Naderi, Guozhu Liang, H. Karimi
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Liquid-hydrogen rocket engine development at Aerojet, 1944 - 1950 [PDF]
This program demonstrated the feasibility of virtually all the components in present-day, high-energy, liquid-rocket engines. Transpiration and film-cooled thrust chambers were successfully operated.
Coplen, H. L. +3 more
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Liquid rocket performance computer model with distributed energy release Interim final report, 15 Aug. 1969 - 15 Aug. 1970 [PDF]
Liquid propellant rocket engine performance computer program with distributed energy ...
Campell, D. T. +2 more
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Eurasian Chemico-Technological Journal, 2017 Technogeneous impact of rocket and space activities on the environment is one of the most actual problems of practical cosmonautics. This technogeneous impact is not only the pollution of near Earth space with space debris (worked-off stages of space ...
V. Trushlyakov +2 more
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Nonlinear combustion instability in liquid-propellant rocket motors Final report [PDF]
Mathematical models of nonlinear combustion instabilities in liquid propellant rocket ...
Burstein, S. Z. +2 more
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Two-axis winch installer for heavy ducts in confined space [PDF]
, 1969 Two-axis winching and traversing device is used for installing liquid-propellant rocket-engine fuel and liquid oxygen suction ducts between the valves and the rocket engine on a test stand.
Cox, E. F.
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ADN – The new oxidizer around the corner for an environmentally friendly smokeless propellant [PDF]
Journal of Aerospace Technology and Management, 2009 The search for a smokeless propellant has encouraged scientists and engineers to look for a chlorine-free oxidizer as a substitute for AP (ammonium perchlorate).
Márcio Y. Nagamachi +3 more
doaj
The prediction of the nonlinear behavior of unstable liquid rockets [PDF]
Analytical technique for solving nonlinear combustion problems associated with liquid propellant rocket ...
Powell, E. A., Zinn, B. T.
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Mathematical model for heat transfer in variable thickness fins for rocket engines
Challenges and Issues of Modern SciencePurpose. This article aims to develop a mathematical model for a fin in the cooling system of liquid propellant rocket engines. The objective is to enable calculations for fins with arbitrary thickness variation. The developed mathematical model will be
Volodymyr Sliusariev, Valerii Bucharskyi
doaj
Discussion: “Liquid-Propellant Rocket Power Plants” (Zucrow, M. J., 1947, Trans. ASME, 69, pp. 847–856) [PDF]
, 1947 J. H. Wyld
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