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Please use this identifier to cite or link to this item: http://dspace.unimap.edu.my:80/xmlui/handle/123456789/13551

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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