Thermal Analyses and Verification for HAUSAT-2 Small Satellite

Details Thermal Analyses and Verification for HAUSAT-2 Small Satellite Thermal Analyses and Verification for HAUSAT-2 Small Satellite

Mar 2006

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2006jass...23...39l&link_type=abstract

Journal of Astronomy and Space Sciences, Vol. 23, no. 1, p. 39-54

Astronomy and Astrophysics

Astronomy

1

Hausat-2 Nanosatellite, Thermal Analysis, Thermal Modeling, High-Power Dissipating Parts

Scientific paper

HAUSAT-2 is nano satellite with 25 kg mass being developed by Space System Research Lab. in Hnakuk Aviation University. This paper addresses HAUSAT-2 small satellite thermal analyses and its verification at satellite system, electronic box, and PCB levels. Thermal model which is used for system-level and box-level thermal analyses was verified and corrected through thermal vacuum/balance test. The new board-level thermal analysis methodology, modelling high-power dissipating EEE parts directly, was proposed. The proposed methodology has been verified with test results.

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