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Guide for Oxygen Hazards Analyses on Components and SystemsBecause most materials, including metals, will burn in an oxygen-enriched environment, hazards are always present when using oxygen. Most materials will ignite at lower temperatures in an oxygen-enriched environment than in air, and once ignited, combustion rates are greater in the oxygen-enriched environment. Many metals burn violently in an oxygen-enriched environment when ignited. Lubricants, tapes, gaskets, fuels, and solvents can increase the possibility of ignition in oxygen systems. However, these hazards do not preclude the use of oxygen. Oxygen may be safely used if all the materials in a system are not flammable in the end-use environment or if ignition sources are identified and controlled. These ignition and combustion hazards necessitate a proper oxygen hazards analysis before introducing a material or component into oxygen service.

The objective of this test plan is to describe the White Sands Test Facility oxygen hazards analysis to be performed on components and systems before oxygen is introduced and is recommended before implementing the oxygen component qualification procedure. The plan describes the NASA Johnson Space Center White Sands Test Facility method consistent with the ASTM documents for analyzing the hazards of components and systems exposed to an oxygen-enriched environment. The oxygen hazards analysis is a useful tool for oxygen-system designers, system engineers, and facility managers. Problem areas can be pinpointed before oxygen is introduced into the system, preventing damage to hardware and possible injury or loss of life.
Document ID
19970001787
Acquisition Source
Johnson Space Center
Document Type
Technical Memorandum (TM)
Authors
Joel M Stoltzfus
(Johnson Space Center Houston, United States)
Jesse Dees
(Lockheed Martin (United States) Bethesda, United States)
Robert F Poe
(Lockheed Martin (United States) Bethesda, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1996
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Spacecraft Design, Testing and Performance
Report/Patent Number
JSC-CN-18456
NAS 1.15:104823
NASA-TM-104823
S-819
Accession Number
97N11558
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Technical Management
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