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Space Shuttle Solid Rocket Motor (SRM) development and qualificationThe configuration of reusable solid propellant motors for the space shuttle vehicle is delineated and traces their design evolution. Also presented are the summary results of the first two of the three qualification motor firings designated QM-1 and QM-2.
Document ID
19800021888
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lund, R. K. (Thiokol Corp. Brigham City, UT, United States)
Brinton, B. C. (Thiokol Corp. Brigham City, UT, United States)
Date Acquired
August 10, 2013
Publication Date
March 1, 1980
Publication Information
Publication: APL The 1980 JANNAF Propulsion Meeting, Vol. 5
Subject Category
Spacecraft Propulsion And Power
Accession Number
80N30389
Funding Number(s)
CONTRACT_GRANT: NAS8-30490
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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