NASA NTRS · 19670046091
A semiconductor combustion pressure transducer for rocket-motor instability studies.
Abstract
Silicon semiconductor combustion pressure transducer for high temperature HF pressure measurements within liquid rocket motor chambers
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Delmonte, J.. 1967-01-01. A semiconductor combustion pressure transducer for rocket-motor instability studies.. https://ntrs.nasa.gov/citations/19670046091
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