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HNBR with organic fiber 2 and carbon fiber powders has little impact on mechanical properties but unsatisfactory ablation performance.
添加有机纤维2和碳纤维粉的hnbr力学性能变化不大，但烧蚀性能不理想。
The ablation mechanism and the performance of carbon-phenolic material of solid propellant rocket nozzles are studied.
本文研究了碳-酚醛材料在固体火箭发动机喷管中的烧蚀机理及性能。
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