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Space Shuttle Main Engine development /May 1980/The Space Shuttle Main Engine is the most advanced liquid propellant rocket engine ever developed. During the last year, significant progess has been made toward the identification and solution of several design weaknesses. The initial two test series to certify the engine's readiness for manned flight have been completed, and additional test series are in progress. Operation of the total propulsion system has been demonstrated by a successful series of flight-simulation tests using the three-engine cluster Main Propulsion Test Article. The first set of flight engines has been acceptance tested for use in Shuttle Orbiter 102 (Columbia) for the first manned orbital flight in late 1980 or early 1981. Engine development is continuing with initial demonstrations of full-power level (109%) operation capability.
Document ID
19800057016
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sanchini, D. J.
(Rockwell International Corp. Canoga Park, CA, United States)
Colbo, H. I.
(Rockwell International Corp. Rocketdyne Div., Canoga Park, Calif., United States)
Date Acquired
August 10, 2013
Publication Date
June 1, 1980
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 80-1129
Report Number: AIAA PAPER 80-1129
Meeting Information
Meeting: Joint Propulsion Conference
Location: Hartford, CT
Start Date: June 30, 1980
End Date: July 2, 1980
Sponsors: AIAA, SAE, and ASME,
Accession Number
80A41186
Funding Number(s)
CONTRACT_GRANT: NAS8-27980
Distribution Limits
Public
Copyright
Other

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