| 返回式卫星的热控设计 |
| |
| 引用本文： | 徐济万.返回式卫星的热控设计[J].中国空间科学技术,1990,10(6):49-56. |
| |
| 作者姓名： | 徐济万 |
| |
| 作者单位： | 北京空间飞行器总体设计部 |
| |
| 摘 要： | 介绍我国返回式卫星热控设计方案。根据我国返回式卫星的特点,描述了热惯性法在热设计中的应用。地面热试验数据与飞行遥测温度数据比较表明,两者一致性良好,热控系统工作正常,星体与星内仪器温度均较好地处于所要求的范围内。
|
| 关 键 词： | 卫星 返回式 热动力试验 热分析 |
THERMAL DESIGN OF RETURNABLE SATELLITE |
| |
| Xu Jiwan.THERMAL DESIGN OF RETURNABLE SATELLITE[J].Chinese Space Science and Technology,1990,10(6):49-56. |
| |
| Authors: | Xu Jiwan |
| |
| Institution: | Beijing Institute of Spacecraft Systems Engineering |
| |
| Abstract: | This paper presents the thermal control subsystem of chinese returnable satellite. According to the characteristics of the satellite, a method of thermal inertia used in thermal design is described.The temperatures obtained from orbit telemetry data are in agreement with that from ground testing.Thermal control subsystem operated well the temperatures of the structure and the equipments met the design requirement. |
| |
| Keywords: | Recoverable satellite Temperature control Thermodynamic test Thermal analysis Design |
| 本文献已被 CNKI 维普 等数据库收录！ |
