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Chemical vapor deposited tungsten with dispersed carbides for Space Shuttle check valvesA chemical vapor deposited tungsten with dispersed carbides was selected as the material for Space Shuttle Orbital Maneuvering and Reaction Control Systems check valve poppets and seats. The selection followed a NASA-sponsored prototype check valve development program utilizing the cutter-seal shell poppet concept. The poppet material is deposited as a coating approximately 0.9 mm thick and fabricated into a shell as a free standing body. The seat material is deposited as a coating 1.1 mm thick on a seat blank, and the cutter seal is machined in the coating. Module tests demonstrated that the material could be ground and lapped to very sharp edges and could cut through typical system contaminants without excessive damage to the sealing surfaces. The material was also determined to be unaffected by exposure to a strongly oxidizing storable propellant.
Document ID
19810028517
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Williams, G. E.
(Rockwell International, Rocketdyne Div., Los Angeles Calif., United States)
Date Acquired
August 11, 2013
Publication Date
October 1, 1980
Publication Information
Publication: SAMPE Quarterly
Volume: 12
Subject Category
Metallic Materials
Accession Number
81A12921
Funding Number(s)
CONTRACT_GRANT: NAS9-14000
CONTRACT_GRANT: NAS9-13882
Distribution Limits
Public
Copyright
Other

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