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| Title: | Transient heat transfer analysis on a satellite in an orbit |
| Authors: | C. W., Chan
C. P., Tso |
| Keywords: | Transient heat transfer
Satellite in orbit
Thermal design |
| Issue Date: | Sep-2004 |
| Publisher: | The Institution of Engineers, Malaysia |
| Citation: | The Journal of the Institution of Engineers, Malaysia, vol. 65(3/4), 2004, pages 50-54 |
| Abstract: | A parametric study has been carried out on emissivities of the surfaces, shell thicknesses and materials of a satellite structure
in order to obtain useful information for satellite thermal engineering design. This is done through a three-dimensional finite
element transient heat transfer model on a simple satellite structure using the commercial software ANSYS. The satellite is
subjected to several heat loadings in an orbit of sun-tracking mode. Using actual empirically available data, a numerical model
is developed and the temperature distribution in the satellite structure predicted. The numerical results of the thermal analysis
are analyzed and discussed. |
| Description: | Link to publisher's homepage at http://www.myiem.org.my/ |
| URI: | http://myiem.org.my/content/iem_journal_2004-175.aspx
http://hdl.handle.net/123456789/13551 |
| ISSN: | 0126-513X |
| Appears in Collections: | IEM Journal
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