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High temperature measuring deviceUltrasonic pulse technique for measuring average gas temperature in nuclear rocket engine - sound propagation and environmental studies
Document ID
19650014967
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Carnevale, E. H.
Larson, G. S.
Lynnworth, L. C.
Date Acquired
August 2, 2013
Publication Date
February 1, 1965
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-CR-54339
Report Number: NASA-CR-54339
Accession Number
65N24568
Funding Number(s)
CONTRACT_GRANT: NAS3-5201
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
NUCLEAR ROCKET
ROCKET ENGINE
GAS HEATING
TEMPERATURE MEASUREMENT
SOUND PROPAGATION
PULSE

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