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Development of isothermal rigsThe results of the Resonant Infrasonic Gauging System (RIGS) development program are reported. The RIGS is a gauging system that is capable of measuring propellant quantity under zero-G as well as under accelerated (one-G) conditions. With the exception of liquid hydrogen, it can be used to gauge virtually any propellant in liquid form including cryogenics. The gauge consists of a sensor unit which is attached to the propellant tank and electronic control unit which may be positioned separately from the sensor. The control unit receives the signals from the sensor as well as the ullage gas pressure and propellant temperature measurements, and computes the propellant quantity remaining in the tank. During the course of this program two prototype RIGS sensors were designed and constructed. The sensors were tested first in the laboratory using water as the simulated propellant and, later, using LN2 in a 100-gallon tank. The system tests proved that the gauge operates virtually as predicted by theory and yielded an accuracy better than 1%.
Document ID
19730019768
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kaminskas, R. A.
(TRW Systems Group Redondo Beach, CA, United States)
Malone, D. J.
(TRW Systems Group Redondo Beach, CA, United States)
Date Acquired
September 2, 2013
Publication Date
April 9, 1973
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-CR-124314
Report Number: NASA-CR-124314
Accession Number
73N28500
Funding Number(s)
CONTRACT_GRANT: NAS8-28574
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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