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Guide for Oxygen Compatibility Assessments on Oxygen Components and SystemsUnderstanding and preventing fire hazards is necessary when designing, maintaining, and operating oxygen systems. Ignition risks can be minimized by controlling heat sources and using materials that will not ignite or will not support burning in the end-use environment. Because certain materials are more susceptible to ignition in oxygen-enriched environments, a compatibility assessment should be performed before the component is introduced into an oxygen system. This document provides an overview of oxygen fire hazards and procedures that are consistent with the latest versions of American Society for Testing and Materials (ASTM) Standards G63 (1999) and G94 (2005) to address fire hazards associated with oxygen systems. This document supersedes the previous edition, NASA Technical Memorandum 104823, Guide for Oxygen Hazards Analyses on Components and Systems (1996). The step-by-step oxygen compatibility assessment method described herein (see Section 4) enables oxygen-system designers, system engineers, and facility managers to determine areas of concern with respect to oxygen compatibility and, ultimately, prevent damage to a system or injury to personnel.
Document ID
20070016582
Acquisition Source
Johnson Space Center
Document Type
Technical Memorandum (TM)
Authors
Rosales, Keisa R.
(NASA White Sands Test Facility NM, United States)
Shoffstall, Michael S.
(NASA White Sands Test Facility NM, United States)
Stoltzfus, Joel M.
(NASA White Sands Test Facility NM, United States)
Date Acquired
August 23, 2013
Publication Date
March 1, 2007
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA/TM-2007-213740
S-998
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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