Thermal Stores in Spacecraft Heating Systems

A. E. Belyavskii; S. V. Novikov; A. E. Sorokin; I. A. Shangin

doi:10.3103/S1068798X19060078

Thermal Stores in Spacecraft Heating Systems

作者: Belyavskii A.E.¹, Novikov S.V.¹, Sorokin A.E.¹, Shangin I.A.¹
隶属关系:
1. Moscow Aviation Institute
期: 卷 39, 编号 6 (2019)
页面: 507-509
栏目: Article
URL: https://journals.rcsi.science/1068-798X/article/view/227733
DOI: https://doi.org/10.3103/S1068798X19060078
ID: 227733

如何引用文章

全文:

开放存取

##reader.subscriptionAccessGranted##
受限制的访问

订阅存取

详细
作者简介
参考
补充文件
统计

详细

In the present work, we consider the use of thermal stores in spacecraft heating systems. The advantages and disadvantages of various approaches to heat storage are compared. The use of heat stores with a melting working material is most promising and practicable at present.