THE HIGH TEMPERATURE EVALUATION OF AEROSPACE MATERIALS.
Summary rept. Jan 65-Jan 66,
DAYTON UNIV OH RESEARCH INST
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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 BTUsq 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.
- Coatings, Colorants and Finishes
- Metallurgy and Metallography