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Development of cost-optimized insulation system for use in large solid rocket motors. Volume 4, task 4 - 260 in. dia motor insulation system design and process plan Final reportDesign, weight, cost, and tooling concepts for cost optimized insulation system for 260 in. dia solid rocket motor
Document ID
19690026619
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Nachbar, D. L. (Aerojet-General Corp. Sacramento, CA, United States)
Simmons, B. A. (Aerojet-General Corp. Sacramento, CA, United States)
Date Acquired
August 5, 2013
Publication Date
August 1, 1969
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-72584
Report Number: NASA-CR-72584
Accession Number
69N35997
Funding Number(s)
CONTRACT_GRANT: NAS3-11224
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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