NASA NTRS ยท 19770026539
Development of a high temperature capacitive pressure transducer
Abstract
High 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%.
Keep this discovery
Explore connections, maps & timelines
Egger, R. L.. 1977-10-01. Development of a high temperature capacitive pressure transducer. https://ntrs.nasa.gov/citations/19770026539
Cite the original work for its findings. Save a collection to share your selection of sources.