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Development of the Space Shuttle main engineThe history of the development, certification, and launch operations of the Space Shuttle Main Engine is described. Development problems and their solutions are discussed. Ground testing at both rated and full power levels involving four engines and eight certification test cycles totalling more than 40,000 seconds of hot-fire testing, which qualified both Columbia's and Challenger's engines for flight, are discussed. Ground checkout and flight performance of Columbia's and Challenger's engines are revealed. Future plans for the Space Shuttle Main Engine are outlined including flight certification testing to verify a life of 40 flights and 20,000 seconds operation before overhaul.
Document ID
19840029017
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Klatt, F. P.
(Rockwell International Corp. Rocketdyne Div., Canoga Park, CA, United States)
Date Acquired
August 12, 2013
Publication Date
October 1, 1983
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
IAF PAPER 83-386
Report Number: IAF PAPER 83-386
Accession Number
84A11804
Funding Number(s)
CONTRACT_GRANT: NAS8-27980
Distribution Limits
Public
Copyright
Other

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