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Guide for Oxygen Component Qualification TestsAlthough oxygen is a chemically stable element, it is not shock sensitive, will not decompose, and is not flammable. Oxygen use therefore carries a risk that should never be overlooked, because oxygen is a strong oxidizer that vigorously supports combustion. Safety is of primary concern in oxygen service. To promote safety in oxygen systems, the flammability of materials used in them should be analyzed. At the NASA White Sands Test Facility (WSTF), we have performed configurational tests of components specifically engineered for oxygen service. These tests follow a detailed WSTF oxygen hazards analysis. The stated objective of the tests was to provide performance test data for customer use as part of a qualification plan for a particular component in a particular configuration, and under worst-case conditions. In this document - the 'Guide for Oxygen Component Qualification Tests' - we outline recommended test systems, and cleaning, handling, and test procedures that address worst-case conditions. It should be noted that test results apply specifically to: manual valves, remotely operated valves, check valves, relief valves, filters, regulators, flexible hoses, and intensifiers. Component systems are not covered.
Document ID
19970010451
Acquisition Source
Johnson Space Center
Document Type
Technical Memorandum (TM)
Authors
Bamford, Larry J.
(Lockheed Martin Engineering and Sciences Co. Houston, TX United States)
Rucker, Michelle A.
(NASA Johnson Space Center Houston, TX United States)
Dobbin, Douglas
(Lockheed Martin Engineering and Sciences Co. Houston, TX United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1996
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-TM-104821
S-816
NAS 1.15:104821
Report Number: NASA-TM-104821
Report Number: S-816
Report Number: NAS 1.15:104821
Accession Number
97N15662
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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