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Comparative study of thrust-vector-control systems for large, solid-fueled launch vehicles. Volume 1 - SummaryComparative analysis of several advanced thrust vector control system designs applied to large, solid propellant launch vehicles
Document ID
19680002712
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Budris, G. D. (Douglas Aircraft Co., Inc. Huntington Beach, CA, United States)
Date Acquired
August 4, 2013
Publication Date
November 1, 1967
Subject Category
Propulsion Systems
Report/Patent Number
DAC-58065
NASA-CR-66504
Report Number: DAC-58065
Report Number: NASA-CR-66504
Accession Number
68N12180
Funding Number(s)
CONTRACT_GRANT: NAS1-7109
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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