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Comparative study of thrust vector control systems for large, solid-fueled launch vehicles. Volume 3 - Appendix materialSystems design and guidance and control analyses of thrust vector control systems for large, solid propellant launch vehicles
Document ID
19680003683
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
NASA-CR-66506
DAC-58067, V. 3
Report Number: NASA-CR-66506
Report Number: DAC-58067, V. 3
Accession Number
68N13152
Funding Number(s)
CONTRACT_GRANT: NAS1-7109
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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