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

This report has yet to be scanned by Contrails staff

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

The abstract for this report is either unavailable or has yet to be entered

Provenance: Lockheed Martin Missiles & Fire Control

Other options for obtaining this report:

Via the Defense Technical Information Center (DTIC):
A record for this report, and possibly a pdf download of the report, exists at DTIC

Via National Technical Report Library:
This report may be available for download from NTRL. Use the Title from this record to locate the item in DTIC Online

Indications of Public Availability
No digital image of an index entry indicating public availability is currently available
The inside cover of this report indicates that it was released for public sale