| DQ—1气球卫星热设计 |
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| 引用本文： | 徐济万,江经善.DQ—1气球卫星热设计[J].中国空间科学技术,1993,13(2):31-35. |
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| 作者姓名： | 徐济万 江经善 |
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| 作者单位： | 北京空间飞行器总体设计部
(徐济万，江经善，钱盛瑜)，北京空间飞行器总体设计部(张世玲) |
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| 摘 要： | 文章介绍了中国气球卫星的热设计与热试验。根据气球卫星的特性,讨论了无源热控制方法在热设计中的应用。说明热试验数据同热计算数据基本一致,气球卫星的温度满足设计要求。
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| 关 键 词： | 热特性 卫星 气球 设计 |
THERMAL DESIGN FOR DQ-1 BALLOON SATELLITE |
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| Xu Jiwan Jiang Jingshan Qian Shengyu Zhang Shiling.THERMAL DESIGN FOR DQ-1 BALLOON SATELLITE[J].Chinese Space Science and Technology,1993,13(2):31-35. |
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| Authors: | Xu Jiwan Jiang Jingshan Qian Shengyu Zhang Shiling |
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| Institution: | Beijing Institute of Spacecraft Systems Engineering |
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| Abstract: | This paper presents the thermal design and thermal testingof the chinese balloon satellite.According to the characteristics of theballoon satellite,the method of passive thermal control used in thermaldesign is described.The temperatures derived from the thermal testingdata are in agreement with those from the thermal calculating data.Thetemperatures of the balloon satellites have met the design requirements. |
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| Keywords: | Thermal property Satellite Balloon Design |
| 本文献已被 CNKI 维普 等数据库收录！ |
