| 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。 |
| 关键词: 固体火箭发动机 双基推进剂 燃烧振动 燃烧稳定性 |
| DOI： |
| 分类号: |
| 基金项目: |
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| EXPERIMENTAL RESEARCH ON THE PRESSURE-COUPLING RESPONSE OF DOUBLE-BASE PROPELLANT |
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Wang Ningfei, Zhao Chongxin, Zhang Wang, Wang Xiu wei, Sun Weishen
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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. |
| Key words: Solid rocket engine Double-base propellant Combustion vibration Combustion stability |
