Optimizing the Intake Design of a Droplet Cooler for Thermal Regulation of Spacecraft

被引：0
|
作者：
Bakhvalov Y.O. [1 ,2 ]
Iosifov P.A. [2 ]
Kulikov S.N. [2 ]
Trunova E.A. [2 ]
机构：
[1] Proekt Tekhnika, Moscow
[2] Moscow Aviation Institute, Moscow
来源：
Russian Engineering Research | 2024年 / 44卷 / 02期
关键词：
cooling; droplet cooler; power systems; power units; spacecraft; thermal regulation;
D O I：
10.3103/S1068798X24020047
中图分类号：
学科分类号：
摘要：
Abstract: The intake of a radiative droplet cooler used in thermal stabilization of spacecraft power systems is tested. The cooler produces monodisperse droplet flows. On the basis of the test results, the design is optimized. © Allerton Press, Inc. 2024. ISSN 1068-798X, Russian Engineering Research, 2024, Vol. 44, No. 2, pp. 177–179. Allerton Press, Inc., 2024. Russian Text The Author(s), 2023, published in Vestnik Mashinostroeniya, 2023, No. 12, pp. 983–986.
引用
收藏
页码：177 / 179
页数：2
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