摘要
Through DSC and film curing method as well as theoretical analysis, it is found that the pore problem during curing process of GAP low-oxygen propellant is due to the structure of GAP and existence of ammonium perchlorate (AP). The problem can be resolved by choosing proper curing catalysts, or adding 3‰-5‰ (mass content) resorcin, or coating AP and so on.
源语言 | 英语 |
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页(从-至) | 72-74 |
页数 | 3 |
期刊 | Guti Huojian Jishu/Journal of Solid Rocket Technology |
卷 | 31 |
期 | 1 |
出版状态 | 已出版 - 2月 2008 |