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| 摘要: |
| 本文叙述了热压碳/碳复合材料和石墨在含铝固体推进剂发动机中由于表面化学反应所产生的化学烧蚀的计算方法.通过试验,证明该方法是符合实际的. |
| 关键词: 喷管烧蚀计算 碳-碳烧蚀计算 碳-碳复合材料 固体火箭发动机 |
| DOI： |
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| Ablation Calculation of Carbon/Carbon Composite Throat Liner in Aluminumized Solid Propellant Engine |
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Lui Shuwei
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| Abstract: |
| In this paper, a method for calculating the ablation, caused by surface chemical reaction, of heatpressing carbon/carbon composite and graphite in aluminu-mized solid propellant rocket engine is proposed. The correctness of the method was confirmed by experimental data. |
| Key words: Nozzle ablation calculation Carbor/carbon ablation calculation Carbon/carbon composite Solid rocket engine |
