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High-temperature hydraulic system actuator seals for use in advanced supersonic aircraft Summary reportHigh temperature hydraulic system actuator seals for advanced supersonic aircraft - graphs
Document ID
19690012860
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lee, J. (Fairchild Hiller Corp. Farmingdale, NY, United States)
Date Acquired
August 4, 2013
Publication Date
September 15, 1967
Subject Category
Machine Elements And Processes
Report/Patent Number
NASA-CR-72354
FHR-2704-4
Accession Number
69N22222
Funding Number(s)
CONTRACT_GRANT: NAS3-7264
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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