| 用一台实验发动机测试发动机性能参数的方法 |
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| 引用本文： | 陈广南,焦少球,张为华,方丁酉,王虎干.用一台实验发动机测试发动机性能参数的方法[J].固体火箭技术,2000,23(4):61-63. |
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| 作者姓名： | 陈广南 焦少球 张为华 方丁酉 王虎干 |
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| 作者单位： | 1. 国防科技大学航天与材料工程学院,长沙,410073
2. 中国航空工业总公司第014中心,洛阳,471009 |
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| 摘 要： | 通过设计一台专用实验发动机进行试验，并应用参数辩识技术，商量确定发动机动态燃速、平均燃速、比冲等参数。通过理论分析和试验结果表明，该方法能准确测量性能参数，并能有效降低试验费用和缩短试验周期。
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| 关 键 词： | 固体推进剂火箭发动机 实验发动机 性能参数 |
Meassurement Method of Solid Motor Parameters by Using One Test Motor |
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| CHEN Guang-nan,JIAO Shao-qiu,ZHANG Wei-hua,FANG Ding-you,WANG Hu-gan.Meassurement Method of Solid Motor Parameters by Using One Test Motor[J].Journal of Solid Rocket Technology,2000,23(4):61-63. |
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| Authors: | CHEN Guang-nan JIAO Shao-qiu ZHANG Wei-hua FANG Ding-you WANG Hu-gan |
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| Institution: | CHEN Guang nan 1,JIAO Shao qiu 1,ZHANG Wei hua 1,FANG Ding you 1 |
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| Abstract: | By using one test motor along with technique of parameter identification, multiple parameters, such as dynamic burning rate, average buring rate and specific impulse were measured. Through theoretical analysis and experimental results, this method is proved to be accurate and also has the advantages of low test cost and short experimental period. |
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| Keywords: | solid propellant rocket engine experimental engine + parameter identification |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
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