推进技术 ›› 1993, Vol. 14 ›› Issue (5): 17-20.
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王宁飞,陆殿林,王新华
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摘要： 提出了催化燃烧双基推进剂在固体火箭发动机中可能出现几个平衡压力的看法。实验证实了此观点的正确性,并讨论了产生非唯一平衡压力的内在条件及外在原因。
关键词: 固体推进剂火箭发动机;固体推进剂;燃烧;压力;气动平衡
Abstract: A new concept that there could be more than one equivalent pressures in a solid rocket motor using double-base propellant has been put forward. This hypothesis has been confirmed by a few experiments. The authors have also discussed the conditions of existence of non-unique equivalent pressures.
Key words: Solid propellant rocket engine;Solid Propellant;Combustion;Pressure;Aerodynamic balance
王宁飞,陆殿林,王新华. 固体火箭发动机平衡压力唯一性探讨[J]. 推进技术, 1993, 14(5): 17-20.
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