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Multipressure and Temperature ProbeAerodynamic 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.
Document ID
19810000189
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Raman, K. R.
(Raman Aeronautics Research)
Date Acquired
August 11, 2013
Publication Date
November 1, 1982
Publication Information
Publication: NASA Tech Briefs
Volume: 6
Issue: 2
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
ARC-11166
Accession Number
81B10189
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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