| 固体火箭发动机平衡压力唯一性探讨 |
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| 引用本文： | 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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| 作者姓名： | 王宁飞 陆殿林 王新华 |
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| 作者单位： | 西安近代化学研究所
(王宁飞，陆殿林)，西安近代化学研究所(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。
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| 关 键 词： | 固体推进剂 火箭发动机 燃烧 |
RESEARCH ON THE NON-UNIQUENESS OF EQUIVALENT PRESSURE IN A SOLID ROCKET MOTOR |
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| Wang Ningfei,Lu Dianling and Wang Xinghua.RESEARCH ON THE NON-UNIQUENESS OF EQUIVALENT PRESSURE IN A SOLID ROCKET MOTOR[J].Journal of Propulsion Technology,1993,14(5):17-20. |
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| Authors: | Wang Ningfei Lu Dianling and Wang Xinghua |
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| Institution: | Xian Modern Chemistry Research Institute |
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| 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. |
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| Keywords: | Solid propellant rocket engine Solid Propellant Combustion Pressure Aerodynamic balance |
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