DocumentCode :
586537
Title :
Thermal design and characterization of solar cell arrays aimed to be used in CubeSat missions
Author :
Horvath, Gabor ; Czifra, D. ; Marosy, G. ; Varhegyi, Z.
Author_Institution :
Fac. of Electr. Eng. & Inf., Budapest Univ. of Technol. & Econ., Budapest, Hungary
fYear :
2012
fDate :
25-27 Sept. 2012
Firstpage :
1
Lastpage :
4
Abstract :
Besides their important place in space education, the significance of CubeSats as technological and scientific demonstrators is also increasing, due to the miniaturization and their low cost associated with the maturing CubeSat technology. The primary energy sources for these spacecraft are solar cells. It is a key question to maximize the available electrical energy gained from the minimal solar cell area available, while coping with the extreme thermal conditions of space which the panels are exposed to. In this paper we describe the structural design of solar cell arrays aimed at maximal energy yield in space along with the thermal characterization techniques used during the thermal optimization of the structure. The presented procedure resulted in an enhanced solar array design which was successfully used in the Masat-1 CubeSat mission, supported by flight telemetry data regarding solar cell temperature values.
Keywords :
solar cell arrays; solar power satellites; space telemetry; Masat-1 CubeSat mission; flight telemetry data; miniaturization; primary energy source; solar cell array; solar cell temperature values; space education; spacecraft; structural design; thermal characterization technique; thermal condition; thermal design; thermal optimization; Materials; Photovoltaic cells; Satellites; Temperature; Temperature measurement; Thermal conductivity; Thermal resistance;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Thermal Investigations of ICs and Systems (THERMINIC), 2012 18th International Workshop on
Conference_Location :
Budapest
Print_ISBN :
978-1-4673-1882-2
Type :
conf
Filename :
6400624
Link To Document :
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