| 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. |
| 关键词: 液体推进剂火箭发动机 多元推进剂 燃烧试验分析 |
| DOI： |
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| TEST AND ANALYSIS ON COMBUSTION OF TRI-PROPELLANT |
|
Song Lianzhong
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|
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. |
| Key words: Multipropellant combustion test Liquid propellant rocket engine Analyzing |
