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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| Veröffentlicht in: | Russian engineering research 2024-02, Vol.44 (2), p.177-179 |
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| container_end_page | 179 |
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| container_issue | 2 |
| container_start_page | 177 |
| container_title | Russian engineering research |
| container_volume | 44 |
| creator | Bakhvalov, Yu. O. Iosifov, P. A. Kulikov, S. N. Trunova, E. A. |
| description | 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. |
| doi_str_mv | 10.3103/S1068798X24020047 |
| format | Article |
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| fulltext | fulltext |
| identifier | ISSN: 1068-798X |
| ispartof | Russian engineering research, 2024-02, Vol.44 (2), p.177-179 |
| issn | 1068-798X 1934-8088 |
| language | eng |
| recordid | cdi_proquest_journals_3047514472 |
| source | SpringerLink Journals |
| subjects | Design optimization Droplets Engineering Engineering Design Spacecraft Spacecraft power supplies |
| title | Optimizing the Intake Design of a Droplet Cooler for Thermal Regulation of Spacecraft |
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