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ASTM Selected Technical Papers
Flammability and Sensitivity of Materials in Oxygen-Enriched Atmospheres: Fifth Volume
By
J Stoltzfus
J Stoltzfus
1
NASA Johnson Space Center White Sands Test Facility
?
Las Cruces, New Mexico 88004
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K McIlroy
K McIlroy
2
Union Carbide Industrial Gases, Inc.
Linde Division
Tonawanda, New York 14151
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ISBN-10:
0-8031-1461-3
ISBN:
978-0-8031-1461-6
No. of Pages:
588
Publisher:
ASTM International
Publication date:
1991

High strength lithium bearing aluminum alloys offer a significant cost saving potential for application to advanced launch and space vehicles. Three well developed alloys, Al-Li 2090, Al-Li 8090, and Weldalite 049, were evaluated for potential application to the large liquid oxygen and hydrogen tanks for the Advanced Launch System. A series of oxygen compatibility tests evaluation was conducted which included the mechanical impact test in liquid and gaseous oxygen, as per NASA 8060.1B, and the promoted combustion test in pressurized gaseous oxygen. Test results indicated that these alloys were in the same fire hazard category as the Aluminum 2219 currently being used in the external propellant tank of the US Space Shuttles. The test results also highlighted a need for changing the current mechanical impact test standards.

1.
Reed
R. P.
,
Simon
N.
. “
Aluminum Alloys for Cryogenic Tanks: Oxygen Compatibility Interim Report
”,
National Institute of Standards and Technology
,
Boulder, CO
,
05
1990
.
2.
Taguchi Methods
— Orthogonal Arrays and Linear Graphs,
American Supplier Institute, Inc.
,
Schmidt
,
1987
.
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