| 未来大推力液体火箭发动机的方案研讨 |
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| 引用本文： | 契尔瓦考夫ВВ,藏家亮,梅舍劳夫ЕП.未来大推力液体火箭发动机的方案研讨[J].导弹与航天运载技术,1996(2). |
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| 作者姓名： | 契尔瓦考夫ВВ 藏家亮 梅舍劳夫ЕП |
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| 作者单位： | 莫斯科航空学院(契尔瓦考夫ВВ，梅舍劳夫ЕП)，上海动力机械研究所(藏家亮) |
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| 摘 要： | 根据未来航天运载系统需求，提出采用液化天然气（甲烷、丙烷）作为大推力液体火箭发动机燃料的问题。重点对若干个三组元液体火箭发动机的系统方案进行分析比较。结论是：采用液氧－碳氢燃料－液氢的三组元、两工况液体火箭发动机是大推力液体火箭发展的新方向，为研制单级入轨的新型运载火箭提供新的系统方案
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| 关 键 词： | 液体推进剂火箭发动机，碳氢化合物，三元推进剂，系统总体方案 |
Conceptual Discussion about Future High Thrust Liquid Propellant Rocket Engine |
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| Valeviy V. Chervakov.Conceptual Discussion about Future High Thrust Liquid Propellant Rocket Engine[J].Missiles and Space Vehicles,1996(2). |
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| Authors: | Valeviy V Chervakov |
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| Affiliation: | Valeviy V. Chervakov(Moscow Aviation Institute) Zang Jialiang(Shanghai Power Machinery Research Institute) Eugeny P. Myshelov(Moscow Aviation Institute) |
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| Abstract: | The paper raises the question of using liquid natural gas(methane,propane) as the fuel of high thrust liquid propellant rocket engine on the requirement of future space vehicle system. The paper places emphasis on analyzing and comparing several system concepts of tripropellant liquid rocket engine. The conclusion is: the tripropellant (liquid oxygen/hydrocarbon/liquid hydrogen) and dual mode liquid rocket engine is the developing trend of high thrust liquid propellant rocket engine and may be used on single-stage-to-orbit launch vehicle. |
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| Keywords: | Liquid propellant rocket engine Hydrocarbon Tripropellant General system proposal |
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