中国空间科学技术2009，Vol.29Issue(5)：1-7,7.
"神舟七号"飞船热控分系统设计和在轨性能评估
Design and On-orbit Performance Evaluation of Thermal Control System for SHENZHOU-7 Spaceship
黄家荣 1范宇峰 1刘炳清 1卢威1
作者信息
- 1. 北京空间飞行器总体设计部,北京100094
- 折叠
摘要
Abstract
The on-orbit flight data were analyzed and the operation performance was evaluated. Flight test shows that TCS has excellent temperature adjust and adapt abilities during prelaunch and ascent stages, orbit flight, EVA and reentry phases, and all apparatus temperature,air temperature and air relative humidity meet the technology requirements.关键词
出舱活动飞船/气闸舱/热控/在轨性能/评估Key words
Extra-vehicular activity spaceship/Airlock cabin/Thermal control/On-orbit performance/Evaluation分类
航空航天引用本文复制引用
黄家荣,范宇峰,刘炳清,卢威.."神舟七号"飞船热控分系统设计和在轨性能评估[J].中国空间科学技术,2009,29(5):1-7,7.
