Combustion Visualization and Liquid Jet in Crossflow Analysis of H2O2/Kerosene Bipropellant Thruster
AerospaceIn the H2O2/Kerosene bipropellant thruster, a liquid fuel jet is transversely injected into a crossflow of hot oxygen and water vapor, catalytically decomposed from a liquid oxidizer.
Suk Min Choi +3 more
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Conceptual design of single-stage launch vehicle with hybrid rocket engine using design informatics
Nihon Kikai Gakkai ronbunshu, 2014 A single-stage launch vehicle with hybrid rocket engine has been conceptually designed by using design informatics, which has three points of view, i.e., problem definition, optimization, and data mining.
Kazuhisa CHIBA +4 more
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Fiber-reinforced ceramic composites for Earth-to-orbit rocket engine turbines [PDF]
Fiber reinforced ceramic matrix composites (FRCMC) are emerging materials systems that offer potential for use in liquid rocket engines. Advantages of these materials in rocket engine turbomachinery include performance gain due to higher turbine inlet ...
Brockmeyer, Jerry W. +1 more
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Cryogenic gel flow viscometer [PDF]
, 1972 Coiled section of tubing measures viscous properties of gelled cryogenic propellants under conditions closely resembling flow in rocket engine systems. Characteristic flow curve provides data necessary for the design of prototype hardware systems using ...
Globus, R. H., Vanderwall, E. M.
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Trade-off analysis of a new liquid rocket engine
, 2019 When high specific impulse and storability are mission requirements, toxic bi-propellant storable couples are very often used. Typically hydrazine or one of its derivatives are used as fuels and nitrogen tetroxide as oxidizer. Maturity of bi-propellant non-toxic alternatives is still low, even though some monopropellant solutions are coming to the ...
Maggi, F. +5 more
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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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Design criteria monograph for high-load high-speed rolling-contact bearings [PDF]
, 1972 Monograph was published which summarizes and systematically orders large body of successful techniques and practices developed for design of liquid rocket engine turbopump bearings.
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Handbook of Recommended Practices for the Determination of Liquid Monopropellant Rocket Engine Performance, [PDF]
, 1979 R. A. Bjorklund +2 more
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Nondestructive testing of brazed rocket engine components [PDF]
, 1968 Report details study made of nondestructive radiographic, ultrasonic, thermographic, and leak test methods used to inspect and evaluate the quality of the various brazed joints in liquid-propellant rocket engine components and assemblies. Descriptions of
Adams, C. J. +2 more
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PARALLEL UNSTEADY TURBOPUMP SIMULATIONS FOR LIQUID ROCKET ENGINES [PDF]
, 2000 Cetin C. Kiris, Dochan Kwak, W. Chan
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