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Guidelines for the Utilization of Composite Materials in Oxygen Storage TanksSpace travel is inherently dangerous and, currently, quite expensive. NASA has always done everything possible to minimize the risk associated with the materials chosen for space travel applications by requiring that all materials associated with NASA programs meet the strict requirements established by NASA testing standard NASA-STD-600 1 Flammability, Odor, Offgassing, and Compatibility Requirements and Test Procedures for Materials in Environments that Support Combustion. NASA also has the need to develop lighter weight structural materials that will allow more payload weight to be carried into space. NASA is utilizing composite materials inside the orbiter to lighten the overall weight, but has not considered composite materials for oxygen tanks because of the inherent incompatibility of composite materials with atomic oxygen. This presentation will focus on how oxygen tanks can be built from composite materials. Details will be provided for the design and compatibility testing techniques that will be utilized to create a new NASA standard, NASA-HDBK-6018, which will serve as the starting point for the design of oxygen tanks made from composite materials.
Document ID
20060026037
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Davis, Samuel E.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Herald, Stephen
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2006
Subject Category
Composite Materials
Meeting Information
Meeting: 2006 National Space and Missile Materials Symposium
Location: Orlando, FL
Country: United States
Start Date: June 25, 2006
End Date: June 30, 2006
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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