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A semiconductor combustion pressure transducer for rocket-motor instability studies.Silicon semiconductor combustion pressure transducer for high temperature HF pressure measurements within liquid rocket motor chambers
Document ID
19670046091
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Delmonte, J.
Date Acquired
August 3, 2013
Publication Date
January 1, 1967
Publication Information
Publication: /INSTRUMENT SOCIETY OF AMERICA
Subject Category
Instrumentation And Photography
Accession Number
67A24820
Distribution Limits
Public
Copyright
Other
Keywords
SEMICONDUCTOR DEVICE
PRESSURE TRANSDUCER
PRESSURE MEASUREMENT
COMBUSTION STABILITY
LIQUID PROPELLANT ROCKET ENGINE

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