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Dust Erosion Performance of Candidate Motorcase Thermal Protection Materials

机译：候选电机箱热保护材料的粉尘侵蚀性能

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A study was conducted to evaluate the erosion performance of candidate motor-case thermal protection materials for advanced missiles. Available data were compiled and evaluated and empirical expressions were developed to describe the erosion performance of two of the leading candidate materials (VAMAC 15J and Kevlar-epoxy). These expressions then were applied to predict the flight response of these two materials for two design flight trajectories and a simulated freestream dust environment. Finally, a number of available ground test facilities were evaluated for use in performing erosion tests of materials for ascent flight. Recommendations were made for the optimum facilities to accomplish different types of test objectives. (Author)

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作者
Smith, D. H.;
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年度 1980
页码 p.1-150
总页数 150
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Rocket engine cases; Erosion; Heat resistant materials; Heat resistant plastics; Guided missiles; Thermal resistance; Dust; Particles; Flight; Predictions; Impact tests; Impact; Flight testing;

机译：火箭发动机箱;侵蚀;耐热材料;耐热塑料;导弹;热阻;灰尘;颗粒;飞行;预测;冲击试验;冲击;飞行试验;

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2. MICROSTRUCTURE AND SOLID PARTICLE EROSION OF CARBON-BASED MATERIALS USED FOR THE PROTECTION OF HIGHLY POROUS CARBON-CARBON COMPOSITE THERMAL INSULATION [J] . Baxter RI., Rawlings RD. Journal of Materials Science . 1997,第17期

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5. Effects of climate, physical erosion, parent mineralogy, and dust on chemical erosion rates in mountainous terrain. [D] . Ferrier, Kenneth Leslie. 2009

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Dust Erosion Performance of Candidate Motorcase Thermal Protection Materials

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