Computational and Experimental Study of Thermal Mode for Nanosatellite Onboard Computer Module
The work is devoted to the computational and experimental study of the thermal mode of the onboard computer module designed for orbital computational experiment on board a nanosatellite of CubeSat form-factor. Three experiments were performed on the vacuum bench—without computational load, with comp...
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| Veröffentlicht in: | Russian aeronautics 2024, Vol.67 (3), p.660-668 |
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| creator | Zhdanova, K. A. Shcheglov, G. A. Tumanov, N. A. |
| description | The work is devoted to the computational and experimental study of the thermal mode of the onboard computer module designed for orbital computational experiment on board a nanosatellite of CubeSat form-factor. Three experiments were performed on the vacuum bench—without computational load, with computational load, and with cyclic load of the onboard computer module operation. Graphs of processor and heat accumulator temperature versus time are plotted. The results of numerical modeling and vacuum tests are compared. A conclusion was made about the operability of the onboard computer module under high vacuum conditions. |
| doi_str_mv | 10.3103/S106879982403022X |
| format | Article |
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| ispartof | Russian aeronautics, 2024, Vol.67 (3), p.660-668 |
| issn | 1068-7998 1934-7901 |
| language | eng |
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| source | SpringerLink Journals - AutoHoldings |
| subjects | Airborne/spaceborne computers Aircraft Instruments and Instrumentation Computer Complexes Automotive Engineering Cubesat Cyclic loads Engineering High vacuum Microprocessors Modules Nanosatellites Numerical models Thermal cycling Vacuum tests |
| title | Computational and Experimental Study of Thermal Mode for Nanosatellite Onboard Computer Module |
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