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Design, fabrication, and test of omnidirectional flexible seals for thrust vector control of large solid rocket motors Final reportOmnidirectional flexible, rubber-steel seal design, fabrication, and performance testing for solid propellant rocket engine thrust vector control
Document ID
19710018242
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wong, E. Y. (Aerojet Solid Propulsion Co. Sacramento, CA, United States)
Date Acquired
September 2, 2013
Publication Date
June 10, 1971
Subject Category
Machine Elements And Processes
Report/Patent Number
NASA-CR-72889
Report Number: NASA-CR-72889
Accession Number
71N27718
Funding Number(s)
CONTRACT_GRANT: NAS3-12049
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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