| 引用本文: | 黄奕勇,张育林.三组元推进系统热力性能研究.[J].国防科技大学学报,1998,20(4):20-23.[点击复制] |
| Huang Yiyong,Zhang Yulin.On the Thermal-Dynamic Performance of Tripropellent Propulsion System[J].Journal of National University of Defense Technology,1998,20(4):20-23[点击复制] |
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| 三组元推进系统热力性能研究 |
| 黄奕勇, 张育林 |
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(国防科技大学 航天技术系 湖南 长沙 410073)
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| 摘要: |
| 随着下一代可重复使用飞行器, 特别是单级入轨飞行器的研究, 很多新技术都得到发展, 三组元混合燃烧技术就是其中之一。本文中通过进行热力计算来对比、讨论三组元发动机与两组元发动机在理论比冲上的差异, 分析三组元发动机的可行性。 |
| 关键词: 三组元发动机, 热力计算, 飞行器 |
| DOI： |
| 投稿日期：1997-11-15 |
| 基金项目: |
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| On the Thermal-Dynamic Performance of Tripropellent Propulsion System |
| Huang Yiyong, Zhang Yulin |
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(Department of Astronautics, NUDT, Changsha, 410073)
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| Abstract: |
| With the research on the next generation reusable launching vehicle, especially with the consideration of SSTO, more and more new technology ies under development. The tripropellant combustion is one of them. In this paper a thermal-dynamic model is developed and the theoretic performance of the tripropellant propulsion system is calculated and analyzed. The difference between performance of tripropellant and dual propellant system is discussed, and possibility of tripropellant system is valued. |
| Keywords: tripropellant engine, thermal-dynamic calculation, vehicle |
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