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Study of solid rocket motors for a space shuttle booster. Volume 4: Mass properties reportMass properties data for the 156 inch diameter, parallel burn, solid propellant rocket engine for the space shuttle booster are presented. Design ground rules and assumptions applicable to generation of the mass properties data are described, together with pertinent data sources.
Document ID
19720015130
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Vonderesch, A. H. (Lockheed Propulsion Co. Redlands, CA, United States)
Date Acquired
September 2, 2013
Publication Date
March 15, 1972
Subject Category
Propulsion Systems
Report/Patent Number
LPC-629-6-VOL-4
NASA-CR-123616
Report Number: LPC-629-6-VOL-4
Report Number: NASA-CR-123616
Accession Number
72N22780
Funding Number(s)
CONTRACT_GRANT: NAS8-28429
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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