| 对俄出口GVU-600空间环境模拟器研制 |
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| 引用本文： | 茹晓勤,刘波涛,刘劲松,詹海洋,韩 潇,童 华. 对俄出口GVU-600空间环境模拟器研制[J]. 航天器环境工程, 2012, 29(6): 667-670 |
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| 作者姓名： | 茹晓勤 刘波涛 刘劲松 詹海洋 韩 潇 童 华 |
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| 作者单位： | 1.北京卫星环境工程研究所，北京100094 |
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| 摘 要： | GVU-600空间环境模拟器是我国首次为俄罗斯研制的一台航天专用设备，它可以模拟真空、冷黑和太阳辐射3项空间基本参数，主要用于进行卫星热平衡、热真空试验。该设备为卧式圆柱结构，容器内径8 m，总长13.5 m，容积600 m3，极限真空1.4×10-5 Pa，热沉温度-190 ℃。文章主要对该设备的技术指标、系统组成及功能进行了介绍，并给出了研制结果。
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| 关 键 词： | 空间环境模拟器；热沉；真空；地面试验设备 |
| 收稿时间： | 2012-06-29 |
| 修稿时间： | 2012-11-14 |
Development of space environmental simulator GVU-600 |
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| Ru Xiaoqin,Liu Botao,Liu Jinsong,Zhan Haiyang,Han Xiao and Tong Hua. Development of space environmental simulator GVU-600[J]. Spacecraft Environment Engineering, 2012, 29(6): 667-670 |
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| Authors: | Ru Xiaoqin Liu Botao Liu Jinsong Zhan Haiyang Han Xiao Tong Hua |
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| Affiliation: | 1.Beijing Institute of Spacecraft Environment Engineering, Beijing 100094, China |
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| Abstract: | The space environment simulator is used to simulate the vacuum, the cold and black and the solar irradiation. GVU-600 is the first aerospace facility developed by China for Russia. It is mainly used for the thermal vacuum test and the thermal balance test. GVU-600 is horizontal and cylindrical with a dimension of 8 m（inner diameter）×13.5 m（total length）, an ultimate pressure of 1.4×10^-5 Pa, and an average temperature of-190 ℃ in the thermal shroud. This paper discusses the facility＇s specifications, configuration, and functions, with test results. |
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| Keywords: | space environmental simulator thermal shroud vacuum ground test facility |
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