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Photographic Study of Liquid-Oxygen Boiling and Gas Injection in the Injector of a Chugging Rocket EngineHigh-speed motion pictures were taken of conditions in the injector liquid-oxygen cavity of an RL-10 rocket engine during throttled engine operation. Photographs were taken during operation of the engine in the chugging region as the helium gas was injected to stabilize combustion, during operation at rated thrust, and during transition into chugging conditions as the gas injection was discontinued. Results of the investigation indicate that, during chugging rocket operation of the RL-10 engine, a high population of fairly large bubbles formed and collapsed within the liquid-oxygen cavity at the same frequency as the chamber pressure oscillations. When gaseous helium was injected into the liquid-oxygen cavity, a fog rapidly spread over the entire field of view, and the system immediately became stable. The injection of gaseous helium at rated conditions produced a very slight increase in engine performance but not enough to produce a net gain in a typical mission payload with the extra equipment needed. The inherent low-frequency system instability associated with the fuel system at low thrust levels was reduced by injecting either gaseous helium or hydrogen. Complete stabilization was achieved in some cases, and a reduction in the severity of the oscillations in others. This was apparently due to the ·anchoring of the phase change front to the location of the gas injection.
Document ID
19710069673
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Conrad, E. William (NASA Lewis Research Center Cleveland, OH, United States)
Hannum, Ned P. (NASA Lewis Research Center Cleveland, OH, United States)
Bloomer, Harry E. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 6, 2013
Publication Date
December 1, 1964
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-TM-X-948
GRC-EDAA-TN68700
Accession Number
71N74987
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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