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Combined effects of hydrazine exposure and endurance testing on solenoid-actuated valve performanceResults are presented from a test program which was conducted to assess the capability of various solenoid-actuated valve design concepts to provide performance characteristics commensurate with long-duration (ten-year) missions to explore the outer planets. The valves were installed in a hydrazine flow test setup and periodically cycled during a nine-month test period under test conditions comparable to anticipated mission operating conditions. In situ valve performance was periodically determined, and leakage was continuously monitored.
Document ID
19740021770
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hagler, R., Jr.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1974
Subject Category
Machine Elements And Processes
Report/Patent Number
NASA-CR-139360
JPL-TM-33-691
Report Number: NASA-CR-139360
Report Number: JPL-TM-33-691
Accession Number
74N29883
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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