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High temperature hydraulic system actuator seals for use in advanced supersonic aircraft Semiannual reportMaterials evaluation, design and fabrication work, and low pressure testing to develop high temperature hydraulic system actuator seals for use in advanced supersonic aircraft
Document ID
19680003185
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
October 14, 1966
Subject Category
Machine Elements And Processes
Report/Patent Number
SAR-3
NASA-CR-91054
FHR-2702-3
Accession Number
68N12654
Funding Number(s)
CONTRACT_GRANT: NAS3-7264
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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