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High temperature hydraulic system actuator seals for use in advanced supersonic aircraft First semiannual reportHigh temperature hydraulic system actuator seals for use in advanced supersonic aircraft
Document ID
19660006256
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lee, J.
(Republic Aviation Corp. Farmingdale, NY, United States)
Date Acquired
August 3, 2013
Publication Date
October 14, 1965
Subject Category
Machine Elements And Processes
Report/Patent Number
NASA-CR-54496
FHR-2702-1
Report Number: NASA-CR-54496
Report Number: FHR-2702-1
Accession Number
66N15545
Funding Number(s)
CONTRACT_GRANT: NAS3-7264
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HIGH TEMPERATURE MATERIAL
HYDRAULIC ACTUATOR
SEALANT
SUPERSONIC AIRCRAFT
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