| 某目标飞行器真空热试验操作平台设计 |
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| 引用本文： | 张立建,张立伟,张文杰,等.某目标飞行器真空热试验操作平台设计[J].航天器环境工程,2009,26(4):350-353. |
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| 作者姓名： | 张立建 张立伟 张文杰 等 |
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| 作者单位： | 北京卫星环境工程研究所,北京,100094 |
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| 摘 要： | 为了保证某目标飞行器在真空模拟设备顺利进行各种附件的装配、线路的连接以及吊装等操作,需要设计操作平台.文章详细介绍了该操作平台的设计.与技术要求的对比结果表明,该平台的主体结构合理,满足某目标飞行器热平衡试验要求.
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| 关 键 词： | 目标飞行器 真空热试验 操作平台 |
| 收稿时间： | 2008/12/26 0:00:00 |
Platform design for vacuum thermal test of the a target spacecraft |
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| Zhang Lijian,Zhang Liwei,Zhang Wenjie and et al.Platform design for vacuum thermal test of the a target spacecraft[J].Spacecraft Environment Engineering,2009,26(4):350-353. |
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| Authors: | Zhang Lijian Zhang Liwei Zhang Wenjie and |
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| Institution: | Beijing Institute of Spacecraft Environment Engineering;Beijing Institute of Spacecraft Environment Engineering;Beijing Institute of Spacecraft Environment Engineering |
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| Abstract: | The operating platform for vacuum thermal tests of the a target spacecraft should be carefully designed to guarantee the successful assembly of various accesories in the target height, the connection of the monitoring lines with the power supply lines, as well as other operation in the KM6. This paper presents the detailed design scheme. |
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| Keywords: | target spacecraft vacuum thermal tests platform |
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