NASA NTRS · 19900048568
SHOOT flowmeter and pressure transducers
Abstract
A venturi flowmeter has been designed and constructed for the Superfluid Helium On-Orbit Transfer (SHOOT) experiment. The calibration results obtained from the SHOOT venturi demonstrate the ability of the flowmeter to meet the requirements of the SHOOT experiment. Flow rates as low as 20 cu dm/h and as high as 800 cu dm/h have been measured. Performances of the SHOOT differential and absolute pressure transducers, which have undergone calibration and vibration tests, are also included. Throughout the tests, the responses of the transducers remained linear and repeatable to within + or - 1 percent of the full scales of the transducers.
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Kashani, A., Wilcox, R. A., Spivak, A. L., Daney, D. E., Woodhouse, C. E.. 1990-03-01. SHOOT flowmeter and pressure transducers. https://ntrs.nasa.gov/citations/19900048568
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