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模块化自适应热控技术体系研究

郑红阳 赵欣 王德伟 徐侃 张加迅

航天器工程2019,Vol.28Issue(1):69-76,8.
航天器工程2019,Vol.28Issue(1):69-76,8.DOI:10.3969/j.issn.1673-8748.2019.01.010

模块化自适应热控技术体系研究

Study of Modular and Adaptive Thermal Control Technical System

郑红阳 1赵欣 1王德伟 1徐侃 1张加迅1

作者信息

  • 1. 北京空间飞行器设计总体部,空间热控技术北京市重点实验室,北京 100094
  • 折叠

摘要

Abstract

The current two thermal control technical systems cannot satisfy the need of on-orbit servicing of future spacecraft.On the progress of some maintainable and adaptive thermal control technology,this paper analyzes the potential thermal control technology on maintainability from the view of system,thermal collection,thermal transmission and thermal rejection,and its future development direction.A new modular and adaptive thermal control technical system on the basis of thermal bus is constructed,in which the thermal control equipment and loading are more adaptive and robust.At last,four on-orbit servicing types of thermal control system,re-placement,repairability,reconfiguration and refueling are presented,of which the feasibility analysis is also studied.

关键词

模块化/自适应控制/热控技术体系/可维修

Key words

modular/adaptive control/thermal control technical system/maintainability

分类

航空航天

引用本文复制引用

郑红阳,赵欣,王德伟,徐侃,张加迅..模块化自适应热控技术体系研究[J].航天器工程,2019,28(1):69-76,8.

基金项目

国家高技术研究发展计划(863 计划,2015AA6303) (863 计划,2015AA6303)

航天器工程

OA北大核心CSCDCSTPCD

1673-8748

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