Investigation Of Feasability Of Utilizing Available Heat Resistant Materials For Hypersonic Leading Edge Applications. Vol.7. Oxidation Resistance Of Bare And Coated Molybdenum Alloy And Graphite

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Report Number: WADC TR 59-744 Volume 7
Author(s): Powers, Donald J., Dickson, John A.
Corporate Author(s): Bell Aerosystems Company
Laboratory: Materials Central
Date of Publication: 1960-12
Pages: 192
Contract: AF 33(616)-6034
DoD Project: 7350
DoD Task: 73500
Identifier: AD0257732

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Provenance: Lockheed Martin Missiles & Fire Control

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