NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Value contamination avoidance devicesMechanical redesign methods were used to minimize contamination damage of conventional fluid components and a contamination separator device was developed for long term reusable space vehicles. These were incorporated into an existing 50.8 mm poppet valve and tested for damage tolerance in a full size open loop flow system with gaseous and liquid nitrogen. Cyclic and steady flow conditions were tested with particles of 125 to 420 micrometers aluminum oxide dispersed in the test fluids. Nonflow life tests (100,000 cycles) were made with two valve configurations in gaseous hydrogen. The redesigned valve had an acceptable cycle life and improved tolerance to contamination damage when the primary sealing surfaces were coated with thin coatings of hard plastic (Teflon S and Kynar). Analytical studies and flow testing were completed of four different versions of the separator. overall separation efficiencies in the 55-90% range were measured with these non-optimum configurations.
Document ID
19760006114
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Endicott, D. L.
(McDonnell-Douglas Astronautics Co. Huntington Beach, CA, United States)
Date Acquired
September 3, 2013
Publication Date
November 1, 1975
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-134877
MDC-G6029
Report Number: NASA-CR-134877
Report Number: MDC-G6029
Accession Number
76N13202
Funding Number(s)
CONTRACT_GRANT: NAS3-17812
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available