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Task 12 data dump (phase 2) OME integrated thrust chamber test reportThe characteristics and performance of the orbit maneuvering engine for the space shuttle are discussed. Emphasis is placed on the regeneratively cooled thrust chamber of the engine. Tests were conducted to determine engine operating parameters during the start, shutdown, and restart. Characteristics of the integrated thrust chamber and the performance and thermal conditions for blowdown operation without supplementary boundary layer cooling were investigated. The results of the test program are presented.
Document ID
19740025118
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Tobin, R. D. (Rockwell International Corp. Canoga Park, CA, United States)
Pauckert, R. P. (Rockwell International Corp. Canoga Park, CA, United States)
Date Acquired
September 3, 2013
Publication Date
August 9, 1974
Subject Category
Propulsion Systems
Report/Patent Number
ASR74-229
NASA-CR-140250
Accession Number
74N33231
Funding Number(s)
CONTRACT_GRANT: NAS9-12802
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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