DocumentCode :
1863409
Title :
Impact of the operating voltage on high power solar arrays
Author :
Brandhorst, Henry W., Jr. ; Ferguson, Dale C.
Author_Institution :
Carbon-Free Energy, LLC, Auburn, AL, USA
fYear :
2011
fDate :
19-24 June 2011
Abstract :
As the power level of commercial, civil and military satellites has increased, there has been a concurrent increase in their operating voltage. Oftentimes this increase in operating voltage has serious consequences. Most scientific satellites operate in Low Earth Orbit (LEO) over a range of inclinations from sun-synchronous, near polar to equatorial. Their operating voltage generally ranges from a nominal 28V to 56V. Communication satellites at (GEO have power levels from about 12 kW to 25 kW and have suffered major failures caused by charge accumulation and discharge in the presence of solar storms when the satellite is emerging from a shadow period. As future satellite power needs climb to 100 s of kilowatts and beyond for electric propulsion and other missions, the operating voltage will increase in order to save mass, hence a study of the implications of voltage increases is timely and warranted.
Keywords :
aerospace propulsion; electric propulsion; solar cell arrays; solar power satellites; solar powered vehicles; GEO communication satellites; LEO satellite; charge accumulation; civil satellites; electric propulsion; high power solar arrays; low earth orbit satellite; military satellites; scientific satellites; solar storms; sun-synchronous inclinations; time 100 s; voltage 28 V to 56 V; Electric potential; Low earth orbit satellites; NASA; Orbits; Space vehicles; Surface charging;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Photovoltaic Specialists Conference (PVSC), 2011 37th IEEE
Conference_Location :
Seattle, WA
ISSN :
0160-8371
Print_ISBN :
978-1-4244-9966-3
Type :
conf
DOI :
10.1109/PVSC.2011.6186251
Filename :
6186251
Link To Document :
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