A research study has been performed to select, through a combined experimental and analytical effort, a refractory metal material and an air vane leading edge configuration capable of surviving the high-performance advanced ballistic missile defense (HMD) interceptor environments. Five candidate tungsten alloy materials and a tungsten-copper material have been screened for use on the basis of mechanical properties, thermal performance, and resistance to particle impact damage. Only those material fabrication processes which had potential to yield full-scale air vane leading edge hardware were considered. Tensile and coefficient of thermal expansion data were obtained for each material from room temperature to 5000°F. Tests conducted in 5-MW and 50-MW plasma arc facilities evaluated surface recession characteristics over a wide range of pressures and enthalpies. Particle impact damage tests on heated and unheated specimens were conducted in a light gas gun facility using /g-in. glass spheres traveling at 10,000 fps. Using the properties obtained, a leading edge design study and thermal stress analysis of several configurations yielded an acceptable design concept which exhibited significantly lower thermal stresses than others considered. The tungsten-hafnium carbide (arc cast) material was the superior candidate in every category.
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