THE HIGH TEMPERATURE EVALUATION OF AEROSPACE MATERIALS.
Abstract
Section I describes the evaluation of pedigreed TZM molybdenum alloys with several commercially available oxidation resistant coatings. Section II describes the arc-plasma screening of a variety of materials at heat flux levels in the range of 100 to 1000 BTU/sq ft sec. Section III describes linear thermal expansion data from 20 to 2500 C for Carb-I-Tex 100, ATJ graphite, and L-56 graphite.
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 01, 1966
- Accession Number
- AD0804192
Entities
People
- D. A. Gerdeman
- J. A. Cherry
- J. C. Wurst
- N. L. Hecht
Organizations
- University of Dayton