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High total temperature sensing probe for the X-15 hypersonic aircraftHigh total temperature sensing probe using fluid oscillator concept for X-15 hypersonic aircraft
Document ID
19710013774
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bailey, R. G. (Honeywell, Inc. Minneapolis, MN, United States)
Date Acquired
August 6, 2013
Publication Date
September 1, 1968
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-CR-116772
REPT-12080-FR1
Report Number: NASA-CR-116772
Report Number: REPT-12080-FR1
Accession Number
71N23250
Funding Number(s)
CONTRACT_GRANT: NAS4-1211
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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