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

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

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.

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Bibliographische Detailangaben
Veröffentlicht in:Russian engineering research 2024-02, Vol.44 (2), p.177-179
Hauptverfasser: Bakhvalov, Yu. O., Iosifov, P. A., Kulikov, S. N., Trunova, E. A.
Format: Artikel
Sprache:eng
Schlagworte:
Design optimization
Droplets
Engineering
Engineering Design
Spacecraft
Spacecraft power supplies
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Beschreibung
Zusammenfassung: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.
ISSN:1068-798X
1934-8088
DOI:10.3103/S1068798X24020047