Eurasian Chemico-Technological Journal, 2017 The choice is discussed of solid gas generating compositions for venting by hot combustion products a fuel tank of the spent orbital stage of a space launch vehicle with a main liquid rocket engine.
V. I. Trushlyakov +2 more
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On possibility to use flow control units of electromagnetic type for liquid propellant rocket engines [PDF]
, 2001 С. А. Шевченко
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Use of cryogenic components of propellants for liquid-propellant rocket engines and in life support systems of manned space vehicles [PDF]
, 2020 S. A. Orlin
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Refractory thrust chambers for spacecraft engines Final report [PDF]
Structural reliability tests on pyrolytic graphite and pyrolytic graphite alloys for use in liquid propellant rocket engine thrust chambers and ...
Campbell, J. G., Coulbert, C. D.
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The alleged contributions of Pedro E. Paulet to liquid-propellant rocketry [PDF]
The first practical working liquid propellant rocket motor was claimed by Pedro E. Paulet, a South American engineer from Peru (1895). He operated a conical motor, 10 centimeters in diameter, using nitrogen peroxide and gasoline as propellants and ...
Ordway, F. I., III
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Method for continuous variation of propellant flow and thrust in propulsive devices Patent [PDF]
, 1962 Continuous variation of propellant flow and thrust by application of liquid foam flow theory to injection ...
Morrell, G.
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Erratum to: “Numerical and experimental investigations of the effect of repeated cyclic thermal loads on the strength of materials of recoverable liquid-propellant rocket engines” [PDF]
, 2009 V. I. Bubnov +3 more
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Review of Combustion Stability Characteristics of Swirl Coaxial Element Injectors [PDF]
Liquid propellant rocket engine injectors using coaxial elements where the center liquid is swirled have become more common in the United States over the past several decades, although primarily for technology or advanced development programs. Currently,
Casiano, M. J., Hulka, J. R.
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Chemistry: Space resources for teachers including suggestions for classroom activities and laboratory experiments [PDF]
, 1971 Curriculum supplement to assist general chemistry teachers in updating instruction materials with aerospace ...
Bowman, W. H., Lawrence, R. M.
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Application of the substructure method for thermal stress-strain assessment of a liquid-propellant rocket engine combustion chamber [PDF]
, 2013 С.С. Гаврюшин +4 more
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