DocumentCode :
2613987
Title :
Hubble Space Telescope solar generator design for a decade in orbit
Author :
Gerlach, L. ; Fournier-Sicre, A. ; Fromberg, A. ; Kroehnert, S.
Author_Institution :
ESA/ESTEC, Noordwijk, Netherlands
fYear :
1990
fDate :
21-25 May 1990
Firstpage :
1308
Abstract :
The Space Telescope Solar Array (STSA), which is supplying the power for the Hubble Space Telescope (HST), is the largest flexible solar array built to date, carrying 48760 back surface field with reflector (BSFR) silicon cells. STSA is designed to survive at least five years in low Earth orbit (30000 thermal cycles) and will supply at least 4400 W at 34 V after four years. STSA had to be designed to survive the aggressive atomic oxygen (ATOX) environment. This was achieved by the development of an ATOX-resistant carrier substrate and of two different types of ATOX-resistant interconnectors. A 10 Ω-cm BSFR solar cell with all extremely smooth surface was developed to ensure a high-quality interconnector weld. The array is protected against shadowing and hot spots by solar cell shunt diodes. Thermal cycling was performed up to 65000 cycles, which demonstrated that the lifetime of the array should be in the order of ten years
Keywords :
elemental semiconductors; silicon; solar cell arrays; space vehicle power plants; Hubble Space Telescope; Space Telescope Solar Array; aggressive atomic oxygen environment; back surface field; hot spot protection; low Earth orbit; reflector; shadowing protection; solar cell shunt diodes; solar generator design; thermal cycling; Low earth orbit satellites; Optical design; Photovoltaic cells; Power supplies; Protection; Shadow mapping; Silicon; Solar power generation; Telescopes; Welding;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Photovoltaic Specialists Conference, 1990., Conference Record of the Twenty First IEEE
Conference_Location :
Kissimmee, FL
Type :
conf
DOI :
10.1109/PVSC.1990.111824
Filename :
111824
Link To Document :
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