Selecting the Design Parameters of a Heat Store in Spacecraft Thermal Management

被引:0
作者
Belyaevskii A.E. [1 ]
Sorokin A.E. [1 ]
机构
[1] Moscow Aviation Institute, Moscow
关键词
design parameters; heat store; temperature; thermal management system;
D O I
10.3103/S1068798X22120073
中图分类号
学科分类号
摘要
Abstract: The design parameters of a heat store for use in spacecraft thermal management systems are optimized. The optimization criterion and procedure are established. © 2022, Allerton Press, Inc.
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收藏
页码:1303 / 1305
页数:2
相关论文
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