| 一种新型航天救生系统的设计 |
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| 引用本文： | 赵阳 高劭伦. 一种新型航天救生系统的设计[J]. 哈尔滨工业大学学报, 1995, 27(5): 27-31 |
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| 作者姓名： | 赵阳 高劭伦 |
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| 摘 要： | 对宇航员紧急救生方案进行了概要的讨论，在比较弹射座椅和救生火箭两种方法的基础上，选择适用于多乘员航天器的救生火箭作为主动飞行段救生方案，文中提出的救生火箭方案采用部分整流罩，减了救生系统质量，提高有效载荷，且对航天器稳定性无影响。
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| 关 键 词： | 火箭 救生火箭 部分整流罩 航天 救生系统 |
Research on a New Accidental Life-saving System of the Spacecraft |
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| Zhao Yang,Gao Shaolun,Guo Zhongxiong. Research on a New Accidental Life-saving System of the Spacecraft[J]. Journal of Harbin Institute of Technology, 1995, 27(5): 27-31 |
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| Authors: | Zhao Yang Gao Shaolun Guo Zhongxiong |
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| Affiliation: | Dept.of Astronautics and Mechanics |
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| Abstract: | Methods of accident rescue for pilot are discussed briefly. Compared to eject installation,the life-saving rocket is employed to suit for multi-piloted spacecraft during the active fly stage.A new life-saving rocket is designed for the first time.Compared with the previous structure,the main advantage of the new system is that the local fairing is applied,and hence the payload is enhanced without any influence on the stability of the system. |
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| Keywords: | Life-saving rocket local fairing payload |
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