Space shuttle orbit maneuvering engine reusable thrust chamber program [PDF]
Tests were conducted on the regenerative cooled thrust chamber of the space shuttle orbit maneuvering engine. The conditions for the tests and the durations obtained are presented.
Pauckert, R. P. +2 more
core +1 more source
Hydrogen/oxygen auxiliary propulsion technology [PDF]
A survey is provided of hydrogen/oxygen (H/O) auxiliary propulsion system (APS) concepts and low thrust H/O rocket technology. A review of H/O APS studies performed for the Space Shuttle, Space Tug, Space Station Freedom, and Advanced Manned Launch ...
Reed, Brian D., Schneider, Steven J.
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Performance Assessment of the Dual-Throat Nozzle Thrust Vector Control in a 3D Rectangular Nozzle
Journal of the Korean Society of Propulsion Engineers, 2020 Kexin Wu, Tae Ho Kim, Heuy Dong Kim
openaire +1 more source
UEG Week 2025 Moderated Posters
United European Gastroenterology Journal, Volume 13, Issue S8, Page S189-S802, October 2025.
wiley +1 more source
Process for Operating a Dual-Mode Combustor [PDF]
A new dual-mode ramjet combustor used for operation over a wide flight Mach number range is described. Subsonic combustion mode is usable to lower flight Mach numbers than current dual-mode scramjets.
Dippold, Vance F., Trefny, Charles J.
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Computational method to predict thermodynamic, transport, and flow properties for the modified Langley 8-foot high-temperature tunnel [PDF]
The Langley 8 foot high temperature tunnel (8 ft HTT) is used to test components of hypersonic vehicles for aerothermal loads definition and structural component verification.
Hunt, L. Roane +2 more
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Free-jet investigation of mechanically suppressed, high radius ratio coannular plug model nozzles [PDF]
The experimental and analytical acoustic results of a scale-model investigation or unsuppressed and mechanically suppressed high-radius ratio coannular plug nozzles with inverted velocity and temperature profiles are summarized.
Brausch, J. F. +3 more
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The 6670-Newton attitude-control thruster using hydrogen-oxygen propellant [PDF]
The development of a reusable, attitude-control propulsion system for the space transportation system is discussed. A flight weight, gaseous oxygen attitude control thruster assembly was tested to obtain data on cyclic life, thermal and hydraulic ...
Gordon, L. H.
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Prediction of the Thrust Performance and the Flowfield of Liquid Rocket Engines [PDF]
In an effort to improve the current solutions in the design and analysis of liquid propulsive engines, a computational fluid dynamics (CFD) model capable of calculating the reacting flows from the combustion chamber, through the nozzle to the external ...
Wang, T.-S.
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Design considerations for the airframe-integrated scramjet [PDF]
Research programs at the NASA Langley Research Center on the development of airframe-integrated scramjet concepts (supersonic combustion ramjet) are reviewed briefly.
Anderson, G. Y., Henry, J. R.
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