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Space shuttle orbit maneuvering engine reusable thrust chamber programTests 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. The tests demonstrated thrust chamber operation over the nominal ranges of chamber pressure mixture ratio. Variations in auxiliary film coolant flowrate were also demonstrated. High pressure tests were conducted to demonstrate the thrust chamber operation at conditions approaching the design chamber pressure for the derivative space tug application.
Document ID
19750002095
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Pauckert, R. P. (Rockwell International Corp. Canoga Park, CA, United States)
Yost, M. C. (Rockwell International Corp. Canoga Park, CA, United States)
Tobin, R. D. (Rockwell International Corp. Canoga Park, CA, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1973
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-140321
ASR-73-349
Accession Number
75N10167
Funding Number(s)
CONTRACT_GRANT: NAS9-12802
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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