DocumentCode :
2602839
Title :
Advanced solar dynamic power systems for future space missions
Author :
Friefeld, J.M. ; Wallin, W.E.
Author_Institution :
Rockwell Int., Canoga Park, CA, USA
fYear :
1989
fDate :
6-11 Aug 1989
Firstpage :
2717
Abstract :
A design and analysis study has been conducted to evaluate the applicability of solar dynamic power generation systems to a wide variety of future space missions. The most promising approach is to limit peak power cycle temperatures to approximately 1090 K by the utilization of lithium fluoride as a thermal energy storage medium which allows energy to be stored at a moderate temperature (1121 K). It was found that the Stirling system has potentially the highest performance, assuming that future test results of space systems fulfil theoretical predictions. Brayton systems, such as those being developed for the Space Station Freedom, will provide competitive performance with lower development risk
Keywords :
heat engines; solar absorber-convertors; solar energy concentrators; space vehicle power plants; thermal energy storage; Brayton systems; LiF; Space Station Freedom; Stirling system; heat engines; performance; power generation; solar absorber-convertors; solar dynamic power systems; space missions; space power; thermal energy storage; Energy storage; Lithium compounds; Power system analysis computing; Power system dynamics; Power systems; Solar power generation; Space missions; Space stations; System testing; Temperature;
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.1989.74859
Filename :
74859
Link To Document :
بازگشت