columbus · Investigation Of The Feasibility Of Utilizing Available Heat Resistant Materials For Hypersonic Leading Edge Applications, Volume IV. Thermal Properties Of Molybdenum Alloy And Graphite

Investigation Of The Feasibility Of Utilizing Available Heat Resistant Materials For Hypersonic Leading Edge Applications, Volume IV. Thermal Properties Of Molybdenum Alloy And Graphite

Title: Investigation Of The Feasibility Of Utilizing Available Heat Resistant Materials For Hypersonic Leading Edge Applications, Volume IV. Thermal Properties Of Molybdenum Alloy And Graphite
Date: 1960
Index Abstract: Not Available
Photo Quality: Undetermined
Report Number: WADC TR 59-744 Volume 4
Creator: Fieldhouse, I. B.; Lang, J. I.; Blau, H. H.
Corporate Author: Armour Research Foundation; Arthur D. Little
Extent: 86
PB Number: PB171390
Access Rights: Unknown
DTIC Record Exists: No
Report Availability: Not available via Contrails
Identifier: ADA278180
Distribution Classification: 1
Laboratory: Materials Laboratory; Aircraft Laboratory
Contract: AF 33(616)-6034
DoD Project: 7350; 1368
Distribution Conflict: No
Index In: Materials Research Abstracts: A Review of the Air Force Materials Research and Development (1962) p. 24; U.S. Government Research Reports
Index Price: Order from OTS $2.25
Date Issued: 1960-07
Abstract: The abstract for this report is either unavailable or has yet to be entered
Type: report