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High-temperature capacitive pressure transducerCapacitive pressure transducer operates continuously at temperatures as high 1,2000 F, and has been evaluated over full-scale differential pressure range of + or - 10 psi (69 x 1000 N/sq m).
Document ID
19780000398
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Egger, R. L. (Boeing Aerospace Co.)
Mickelsen, R. A. (Boeing Aerospace Co.)
Nelson, D. W. (Boeing Aerospace Co.)
Nelson, E. J. (Boeing Aerospace Co.)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Publication Information
Publication: NASA Tech Briefs
Volume: 3
Issue: 3
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LEW-13078
Report Number: LEW-13078
ISSN: 0145-319X
Accession Number
78B10398
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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