NASA NTRS · 19840024709
Research pressure instrumentation for NASA Space Shuttle main engine, modification no. 6
Abstract
Research concerning the utilization of silicon piezoresistive strain sensing technology for space shuttle main engine applications is reported. The following specific topics were addressed: (1) transducer design and materials, (2) silicon piezoresistor characterization at cryogenic temperatures, (3) chip mounting characterization, and (4) frequency response optimization.
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Anderson, P. J., Johnson, R. L.. 1984-03-01. Research pressure instrumentation for NASA Space Shuttle main engine, modification no. 6. https://ntrs.nasa.gov/citations/19840024709
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