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Performance effects resulting from plugged liquid oxygen posts of the Space Shuttle Main Engine InjectorThe paper discusses the performance effects resulting from plugged LOX posts of the Space Shuttle Main Engine Injector. The simulation was performed with the REFLEQS 2-D code. Analysis was performed axisymmetrically and injector surface was divided into several regions to account for the mixture ratio variation on the injector surface. The reduction of vaccum specific impulse was approximately 0.01 second per plugged LOX post. This reduction is an order of magnitude higher than the result of Space Shuttle flight reconstruction data. It is presumed that this overprediction is due to the axisymmetric simulation that smears local effects.
Document ID
19920066323
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kim, S.
(Sverdrup Technology, Inc. Huntsville, AL, United States)
Trinh, H. P.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 15, 2013
Publication Date
July 1, 1992
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 92-3376
Accession Number
92A48947
Distribution Limits
Public
Copyright
Other

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