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卫星用两种单相流体回路方案对比研究
引用本文:张立,姜军,赵启伟.卫星用两种单相流体回路方案对比研究[J].航天器工程,2010,19(4):35-40.
作者姓名:张立  姜军  赵启伟
作者单位:北京空间飞行器总体设计部,北京,100094
摘    要:单相流体回路系统是航天器主动热控技术中的一种重要方式。文章概述了流体回路的工作原理及理论基础,总结了单相流体回路的设计思路,结合某卫星型号,设计了两种流体回路方案,在SINDA/FLUINT中建立数值仿真模型进行分析计算,并比较了两种方案的应用性能。结果显示,将单相流体回路系统应用于卫星,可取得较好的控温效果。

关 键 词:卫星  热控制  单相流体回路  数值仿真

Comparison between Two Schemes of Single-phase Fluid Loop System for Satellite
ZHANG Li,JIANG Jun,ZHAO Qiwei.Comparison between Two Schemes of Single-phase Fluid Loop System for Satellite[J].Spacecraft Engineering,2010,19(4):35-40.
Authors:ZHANG Li  JIANG Jun  ZHAO Qiwei
Institution:(Beijing Institute of Spacecraft System Engineering, Beijing 100094, China)
Abstract:Single-phase fluid loop system is one of the most important method for active thermal control technique on spacecraft. The fundamental and process of designing single-phase fluid loop are summarized. Two schemes of fluid loop for satellite are designed, and their performances are evaluated and compared through numerical simulation in SINDA/FLUINT. It proves that using fluid loop system for satellite thermal control is effective.
Keywords:satellite  thermal control  single-phase fluid loop  numerical simulating
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