Extensive research and development efforts have been expended toward development of thermal control and environmental protection coatings for NASP and generic hypersonic vehicle applications. The objective of the coatings development activities summarized here was to develop light-weight coatings for protecting advanced titanium alloys from oxidation in hypersonic vehicle applications. A number of new coating concepts have been evaluated. Coated samples were exposed to static oxidation tests at temperatures up to 1000 C using a thermogravimetric apparatus. Samples were also exposed to simulated hypersonic flight conditions for up to 10 hr to determine their thermal and chemical stability and catalytic efficiency. The emittance of samples was determined before and after exposure to simulated hypersonic flight conditions.
Thermal Control/Oxidation Resistant Coatings for Titanium-Based Alloys
1992
20 pages
Report
No indication
English
Manned Spacecraft , Nonferrous Metals & Alloys , Coatings, Colorants, & Finishes , Engineering Materials , Hypersonic vehicles , Oxidation resistance , Temperature control , Thermal control coatings , Titanium alloys , Aerospace planes , Oxidation , Thermal stability , Thermogravimetry , Flight conditions , Hypersonic flight , National aerospace plane program , Static tests
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