摘要
在充分继承载人飞船成功研制经验的基础上,结合我国载人运输飞船新任务的要求,热控分系统开展了方案设计优化和验证工作,主要包括:密封舱空气温度控制改进,分系统配置优化和减重设计,分系统在轨自主管理与智能化控温设计,以及停靠阶段热控分系统方案设计优化等。
Based on the successful experience of the previous manned spaceship flights, considering the new reqairements for manned transport spaceship missions of China, the optimization design and validation on thermal control system are carried out, that mainly including： improvement of air temperature control in sealed cabin, system configure optimization and weight reduce design, system independence management of subsystems on orbit and aptitude temperature control design, thermal control system optimization in berth, etc.
出处
《载人航天》
CSCD
2009年第4期7-10,39,共5页
Manned Spaceflight
关键词
载人运输飞船
热控
方案
优化设计
Manned transport spaceship, Thermal control,Seheme, Optimization design
