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Development of a high temperature capacitive pressure transducerHigh temperature pressure transducers capable of continuous operation while exposed to 650 C were developed and evaluated over a full-scale differential pressure range of + or - 69 kPa. The design of the pressure transducers was based on the use of a diaphragm to respond to pressure, variable capacitive elements arranged to operate as a differential capacitor to measure diaphragm response and on the use of fused silica for the diaphragm and its supporting assembly. The uncertainty associated with measuring + or - 69 kPa pressures between 20C and 650C was less than + or - 6%.
Document ID
19770026539
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Egger, R. L.
(Boeing Aerospace Co. Seattle, WA, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1977
Subject Category
Instrumentation And Photography
Report/Patent Number
D180-20746-1
NASA-CR-135282
Report Number: D180-20746-1
Report Number: NASA-CR-135282
Accession Number
77N33483
Funding Number(s)
CONTRACT_GRANT: NAS3-19556
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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