D. S.
Mikhatulin Yu. V.
Polezhaev ABSTRACT We consider the possibilities for modeling heat-erosion impact of a dusty atmosphere on the elements of the frontal surfaces of rockets on ground-based gasdynamic test benches, which should be reproduced in experimental investigations. A model of heat-erosion destruction of coating materials, in which the total entrainment of mass is divided into thermal, erosion, and gas-mechanical, is proposed. The conditions, when these components are independent of each other and when this dependence can be ignored, are analyzed. The determining parameters are formulated.
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