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交会对接组合体热管理研究

满广龙 曹剑峰 孟繁孔

航天器工程2011,Vol.20Issue(6):32-37,6.
航天器工程2011,Vol.20Issue(6):32-37,6.

交会对接组合体热管理研究

Research on a Thermal Management System for Docking Spacecraft Combination

满广龙 1曹剑峰 1孟繁孔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

Thermal management system is important to maintain the environment within the combination of target spacecraft and manned spacecraft.A thermal management system design based on inter cabin ventilation is proposed.The system's performance is verified through thermal balance test and thermal simulation.The results show that the air temperature in the cabins can be within 19~26℃.In the end,some suggestions on thermal management system design for such complex spacecraft as space station is proposed.

关键词

交会对接/目标飞行器/载人飞船/组合体/热管理

Key words

rendezvous and docking/target spacecraft/manned spacecraft/combination/thermal management

分类

航空航天

引用本文复制引用

满广龙,曹剑峰,孟繁孔..交会对接组合体热管理研究[J].航天器工程,2011,20(6):32-37,6.

基金项目

国家重大科技专项工程 ()

航天器工程

OACSTPCD

1673-8748

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