| 燃烧室新材料在卫星双组元低推力发动机上的应用 |
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| 引用本文： | 陈健.燃烧室新材料在卫星双组元低推力发动机上的应用[J].航天控制,2001,19(4):8-14. |
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| 作者姓名： | 陈健 |
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| 作者单位： | 北京控制工程研究所,北京,100080 |
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| 摘 要： | 对有代表性、有发展前途的几种新材料进行比较 ,并根据应用新材料的低推力发动机燃烧室的结构特点 ,分析了不同冷却方式对双组元低推力发动机性能损失的影响 ,为双组元低推力发动机燃烧室的材料选择、加工工艺、设计优化提供参考。
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| 关 键 词： | 低推力双组元发动机 燃烧室 铼/铱 碳-碳复合材料 |
| 修稿时间： | 2001年7月13日 |
Application of New Chamber Materials in Low Thrust Bipropellant Thruster for Spacecrafts |
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| Chen Jian Beijing Institute of Control Engineering,Beijing.Application of New Chamber Materials in Low Thrust Bipropellant Thruster for Spacecrafts[J].Aerospace Control,2001,19(4):8-14. |
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| Authors: | Chen Jian Beijing Institute of Control Engineering Beijing |
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| Institution: | Chen Jian Beijing Institute of Control Engineering,Beijing 100080 |
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| Abstract: | This paper makes research on several representative and promising materials, analyzes the performance loss of thruster with different cooling, based on the configuration characteristics of low thrust bipropellant thruster chamber made of new materials, and provides a reference for material choice, manufacturing process and optimal design of low thrust bipropellant thruster chamber. |
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| Keywords: | Low thrust bipropellant thruster Chamber Rhenium/iridium Carbon/carbon composite |
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