| 剩余推进剂排放系统研究 |
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| 引用本文： | 廖少英.剩余推进剂排放系统研究[J].中国空间科学技术,2001,21(1):45-51. |
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| 作者姓名： | 廖少英 |
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| 作者单位： | 上海航天局机电设备研究所!上海200245 |
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| 摘 要： | 论述中国首枚上面级火箭剩余推进剂排放方案论证 ,排放系统方案选择 ;提出中国专用排放系统方案 ,排放系统设计、研制与试验研究的全过程 ,为解决中国长征型号上面级火箭高空爆炸解体问题提供了技术基础
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| 关 键 词： | 推进剂剩余量 排放系统 研究 航天器 |
Research of the Residual Propellant Dumping System |
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| Liao Shaoying.Research of the Residual Propellant Dumping System[J].Chinese Space Science and Technology,2001,21(1):45-51. |
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| Authors: | Liao Shaoying |
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| Abstract: | The dumping scheme demonstration and option of the residual propellant of first upper stages rocket of China are discussed.The scheme of dumping system for special use is put forward.The design,development and experiment of all process is introduced.Based on the technology,the problem of explosive disintegrate in the high altitude of upper stage rocket of Long March Model Vehicles is expected to be solved. |
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| Keywords: | Propellant residual Effluent system Research Spacecraft |
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