| 三组元推进剂燃烧试验分析 |
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| 引用本文： | 宋连忠.三组元推进剂燃烧试验分析[J].推进技术,1989,10(6):33-37,71,72. |
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| 作者姓名： | 宋连忠 |
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| 作者单位： | 航空航天部11所 |
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| 摘 要： | 三组元火箭发动机是近几年提出的新概念.本文介绍了三组元推进剂燃烧试验及其结果分析.试验用液氧/丙烷/氢做推进剂在9.78MPa燃烧室压力下完成.试验结果表明,三组元推进剂和三组元发动机概念可行.
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| 关 键 词： | 液体推进剂火箭发动机 多元推进剂 燃烧试验分析 |
TEST AND ANALYSIS ON COMBUSTION OF TRI-PROPELLANT |
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| Song Lianzhong.TEST AND ANALYSIS ON COMBUSTION OF TRI-PROPELLANT[J].Journal of Propulsion Technology,1989,10(6):33-37,71,72. |
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| Authors: | Song Lianzhong |
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| Institution: | The 11st Research Institute |
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| Abstract: | Tri-propellant rocket engine is a new concept developed in recent years.The combustion tests of LOX/propane/gas hydrogen tri-propellant are conducted with subscale hardware at chamber pressure of 6.78MPa and the results are analyzed in this paper.It is shown that the concept is feasible. |
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| Keywords: | Multipropellant combustion test Liquid propellant rocket engine Analyzing |
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