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Chilldown study of the single stage inducer test rigOf the six chilldown tests, data from only one could be used for evaluation. During the rest of the chilldown tests, there was leakage hydrogen flow into the pump cavity prior to the initiation of the chilldown test. In all of the tests the hydrogen condition into the pump was probably 100% vapor. The data from this one test, therefore, can be used to compare only the single phase fluid correlation in the analytical pump chilldown model. In general, the actual pump chilled down much faster than predicted by the analytical pump model. There were insufficient data from the test to measure the pump flow rate and pump inlet fluid condition; therefore, these parameters were extrapolated based on related data which were available. However, even with the highest probable flow rate, the pump chilled faster than predicted.
Document ID
19730015551
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kimura, L. A.
(Aerojet Nuclear Systems Co. Azusa, CA, United States)
Date Acquired
September 2, 2013
Publication Date
June 2, 1972
Subject Category
Facilities, Research, And Support
Report/Patent Number
N8110R:72-033
NASA-CR-132212
Report Number: N8110R:72-033
Report Number: NASA-CR-132212
Accession Number
73N24278
Funding Number(s)
PROJECT: PROJ. 110
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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