Results 101 to 110 of about 29,759 (245)
International Journal of Aerospace Engineering, 2012 Pressure and temperature of the liquid rocket thrust chambers into which propellants are injected have been in an ascending trajectory to gain higher specific impulse.
Bruce Chehroudi
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Demonstrated survivability of a high temperature optical fiber cable on a 1500 pound thrust rocket chamber [PDF]
A demonstration of the ability of an existing optical fiber cable to survive the harsh environment of a rocket engine was performed at the NASA Lewis Research Center.
Sovie, Amy L.
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Ablative response of a silica phenolic to simulated liquid propellant rocket engine operating conditions [PDF]
Ablative response of silica phenolic to simulated liquid propellant rocket engine operating ...
Moyer, C. B. +3 more
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Design criteria monograph on turbopump systems [PDF]
, 1975 Turbopump assembly for modern liquid propellant rocket engine is complete system in itself. It consists of many components, some of which are themselves subsystems.
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The Formation and Properties of Liquid Sheets Suitable for Use in Rocket Engine Injectors [PDF]
Formation and properties of liquid sheets suitable for use in rocket engine ...
Riebling, R. W.
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A Historical Systems Study of Liquid Rocket Engine Throttling Capabilities [PDF]
, 2010 This is a comprehensive systems study to examine and evaluate throttling capabilities of liquid rocket engines. The focus of this study is on engine components, and how the interactions of these components are considered for throttling applications ...
Betts, Erin M. +1 more
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Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроениеIn this paper, various configurations of jet nozzles are analyzed, as well as their design. The effects of the inlet chamfer of jet nozzles on their flow rate and range are considered.
Yu. I. Ageenko, A. S. Bubnova
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Extended temperature range ACPS thruster investigation [PDF]
The successful hot fire demonstration of a pulsing liquid hydrogen/liquid oxygen and gaseous hydrogen/liquid oxygen attitude control propulsion system thruster is described.
Blubaugh, A. L., Schoenman, L.
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Journal of Aerospace Technology and Management, 2011 This study presents the results of the investigation of a cooling method widely used in the combustion chambers, which is called cooling film, and it is applied to a liquid rocket engine that uses as propellants liquid oxygen and kerosene.
Luís Antonio Silva
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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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