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Mathematical model of the Space Shuttle Main Engine gaseous oxygen control valveA computer program for modeling transient flow behavior of the GOX control valve (GCV) has been developed which makes it possible to model a variety of operating conditions and changes of physical hardware. The SSME GCV controls the flow of GOX that pressurizes the Pogo accumulator. The model simulates the transient flow behavior of the original, tight stacked, and redesigned valve configurations during start and shutdown. The model reads a user-prepared input file that defines the valve configurations and thus provides maximum flexibility.
Document ID
19920066434
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Langer, Susan L.
(Sverdrup Technology, Inc. Huntsville, AL, United States)
Tygielski, Philip
(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 92-3538
Accession Number
92A49058
Distribution Limits
Public
Copyright
Other

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