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Determination of processing and test facility requirements for large solid rocket motors. Volume 1 - Task 1 - Facility modification for full-length 260 inch diameter motor processing and test Final reportFacility modification plan for testing 260-inch diameter solid rocket engine
Document ID
19700027475
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lambert, W. L. (Aerojet Solid Propulsion Co. Sacramento, CA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1970
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-72729
Report Number: NASA-CR-72729
Accession Number
70N36791
Funding Number(s)
CONTRACT_GRANT: NAS3-12041
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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