NASA NTRS ยท 19810000189
Multipressure and Temperature Probe
Abstract
Aerodynamic probe is a small cylinder tube holding a network of tiny tubes leading to various ports. Six parameters are recorded simultaneously with little interference with aerodynamic flow. Two tubes connected by a hot-wire tungsten probe sense steady and fluctuating components of total and static pressures; the feedbacks from these tubes are input into differential-pressure sensors to measure fluctuating components of the pressures. Data are recorded by instruments at the back end of the probe.
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Raman, K. R.. 1982-11-01. Multipressure and Temperature Probe. https://ntrs.nasa.gov/citations/19810000189
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