| 航天飞机系统两体分离问题的探讨 |
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| 引用本文： | 张鲁民,柳森.航天飞机系统两体分离问题的探讨[J].空气动力学学报,1990,8(2):174-180. |
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| 作者姓名： | 张鲁民 柳森 |
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| 作者单位： | 中国空气动力研究与发展中心
(张鲁民)，中国空气动力研究与发展中心(柳森) |
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| 摘 要： | 本文简要地叙述了美国研究轨道器与外挂贮油箱,轨道器与载机分离问题的概况。对垂直起飞两级入轨的并联两机的分离问题,提出了研究模型并作了具体分析,着重提出了实现两机安全分离需要解决的技术难点。 二级航天飞机的两机分离问题,是未来航天高技术领域的关键技术之一,本文阐述了解决两体并联分离问题我国现有的技术水平,并提出了解决该问题的技术方案。
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| 关 键 词： | 航天飞机 载机分离 分离动力学 |
INVESTIGATION OF SEPARATION ABOUT THE PARALLEL SPACE SHUTTLE SYSTEM |
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| Zhang Lumin Liu Sen.INVESTIGATION OF SEPARATION ABOUT THE PARALLEL SPACE SHUTTLE SYSTEM[J].Acta Aerodynamica Sinica,1990,8(2):174-180. |
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| Authors: | Zhang Lumin Liu Sen |
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| Institution: | China Aerodynamic Research and Development Center |
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| Abstract: | The separation research of the Orbiter/External Tank or Orbiter/Carrier in the United States is described in this paper. The analytical model of separation is presented for the parallel Space Shuttle system with the perpendicular launch. Meanwhile, the important problems of the secure separation are presented. The separation of the parallel Space shuttle system is a key technique in the future space technical fields. Our capability of resolving separation is discribed and the method of resolving separation is provided in this paper. |
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| Keywords: | space shuttle carrier separation separation dynamics |
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