| 水冲压发动机原理性试验技术研究 |
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| 引用本文： | 甘晓松,何国强,王建儒,任全彬.水冲压发动机原理性试验技术研究[J].固体火箭技术,2008,31(1):4-7. |
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| 作者姓名： | 甘晓松 何国强 王建儒 任全彬 |
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| 作者单位： | 1. 西北工业大学,航天学院,西安,710072
2. 中国航天科技集团公司四院四十一所,西安,710025 |
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| 摘 要： | 从水冲压发动机的工作机理出发,提出了适合开展发动机原理性研究的燃气发生器式水冲压发动机的工作原理。结合铝镁贫氧推进剂、水冲压发动机试验测试系统设计等研究,完成了燃气发生器式水冲压原理性试验研究工作,获得了该工作形式下铝镁推进剂的燃烧性能,成功验证了水冲压发动机的工作原理可行性,为后续开展水冲压发动机的性能研究提供了丰富的试验数据。
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| 关 键 词： | 水冲压发动机 试验 贫氧推进剂 |
| 文章编号： | 1006-2793（2008）01-0004-04 |
| 收稿时间： | 2007-08-16 |
| 修稿时间： | 2007-11-15 |
Experimental investigation on concept of water ramjet |
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| GAN Xiao-song,HE Guo-qiang,WANG Jian-ru,REN Quan-bin.Experimental investigation on concept of water ramjet[J].Journal of Solid Rocket Technology,2008,31(1):4-7. |
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| Authors: | GAN Xiao-song HE Guo-qiang WANG Jian-ru REN Quan-bin |
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| Abstract: | According to working mechanism of water ramjet,operation principle of the gas generator water ramjet was put forward.In combination with measurement system design of low-oxygen aluminum and magnesium propellant and water ramjet,experimental investigation on the gas generator water ramjet was finished,and combustion properties of aluminum and magnesium propellant were obtained.Feasibility of operation principle of water ramjet was successfully verified,which can provide sufficient test data for further performance investigation of water ramjet. |
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| Keywords: | water ramjet test fuel-rich propellant |
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