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A technique for dynamically calibrating pressure transducers at cryogenic temperaturesA technique was developed for the calibration of dynamic pressure transducers at cryogenic temperatures. The calibration system utilizes an 8.9 Newton peak thrust shaker which oscillates a helium-filled bellows to generate a sinusoidal dynamic pressure to calibrate transducers immersed in a cryogenic environment. The system has a dynamic pressure measurement uncertainty of approximately 11% and is capable of producing peak-to-peak dynamic pressure amplitudes of 1.4 kPa over a frequency range of 40 to 100 hertz and a temperature range of 100 to 300 K. It provides an unprecedented capability of both static and dynamic calibration of pressure transducers from ambient to cryogenic temperature.
Document ID
19840003390
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Gibbens, B. V.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
October 1, 1983
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-TM-85695
NAS 1.15:85695
Report Number: NASA-TM-85695
Report Number: NAS 1.15:85695
Accession Number
84N11458
Funding Number(s)
PROJECT: RTOP 505-31-53-09
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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