DocumentCode :
2545171
Title :
Solar dynamic power module design
Author :
Secunde, Richard R. ; Labus, Thomas L. ; Lovely, Ronald G.
Author_Institution :
NASA Lewis Res. Center, Cleveland, OH, USA
fYear :
1989
fDate :
6-11 Aug 1989
Firstpage :
299
Abstract :
A design for a solar dynamic (SD) power module that meets all of the performance requirements for operating on orbit as a power source on the Space Station Freedom is presented. Assembly of the module in orbit will incorporate methods and procedures to be developed for other Freedom elements; no special equipment will be needed. The technology base for SD module development and production is shown to exist at both the system and component levels. The reasons are clearly indicated for adding SD power to Freedom; they include tremendous life-cycle cost savings, in conjunction with the advantage of having a hybrid or alternate power source in case some anomaly with PV occurs
Keywords :
photovoltaic power systems; space vehicle power plants; Space Station Freedom; solar dynamic power module; Aerodynamics; Assembly; Costs; Earth; Hardware; Multichip modules; Photovoltaic systems; Solar energy; Solar power generation; Space stations;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Energy Conversion Engineering Conference, 1989. IECEC-89., Proceedings of the 24th Intersociety
Conference_Location :
Washington, DC
Type :
conf
DOI :
10.1109/IECEC.1989.74479
Filename :
74479
Link To Document :
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