| 双基推进剂压力响应函数的实验研究 |
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| 引用本文： | 王宁飞,赵崇信,张暹,王秀维,孙维申.双基推进剂压力响应函数的实验研究[J].推进技术,1992,13(6):81-84,80. |
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| 作者姓名： | 王宁飞 赵崇信 张暹 王秀维 孙维申 |
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| 作者单位： | 西安近代化学研究所
(王宁飞，赵崇信，张暹，王秀维)，西安近代化学研究所(孙维申) |
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| 摘 要： | 讨论了可控式T型燃烧器测量推进剂压力耦合响应函数的原理及方法,列出三种双基推进剂在各种温度、频率和压力下的测量结果。
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| 关 键 词： | 火箭发动机 双基推进剂 燃烧振动 |
EXPERIMENTAL RESEARCH ON THE PRESSURE-COUPLING RESPONSE OF DOUBLE-BASE PROPELLANT |
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| Wang Ningfei,Zhao Chongxin,Zhang Wang,Wang Xiu wei and Sun Weishen.EXPERIMENTAL RESEARCH ON THE PRESSURE-COUPLING RESPONSE OF DOUBLE-BASE PROPELLANT[J].Journal of Propulsion Technology,1992,13(6):81-84,80. |
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| Authors: | Wang Ningfei Zhao Chongxin Zhang Wang Wang Xiu wei and Sun Weishen |
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| Institution: | Xian Modern Chemistry Research Institute |
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| Abstract: | The authors have discussed the principle and method of determining pressure-coupling response function of propellants with the controllable T-burner, and presented the results of three double-base propellants in high initial temperature, normal initial temperature and low initial temperature at various frequences and various pressures. |
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| Keywords: | Solid rocket engine Double-base propellant Combustion vibration Combustion stability |
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