DocumentCode :
321531
Title :
Two-stage concentrators for solar bimodal power and propulsion systems
Author :
Ender, Andrei Ya ; Kolyshkin, Lgor N. ; Kuznetsov, Victor I.
Author_Institution :
A.F. Ioffe Physicotech. Inst., Acad. of Sci., St. Petersburg, Russia
Volume :
1
fYear :
1997
fDate :
27 Jul-1 Aug 1997
Firstpage :
422
Abstract :
A solar bimodal system provides both electrical power for an on-orbit operation and high-performance thermal propulsion capability for an orbital transfer. An orbital transfer payload strongly depends on solar concentrator mass which is determined by its efficiency. This paper is devoted to an analysis and comparison of concentrator-receiver system efficiency for one- and two-stage solar concentrators. A new computer code TANDEM for calculating the concentrator-receiver system efficiency was developed. The basic principles of this code are discussed
Keywords :
aerospace computing; aerospace propulsion; aerospace simulation; power engineering computing; software packages; solar energy concentrators; solar power stations; space vehicle power plants; thermionic conversion; TANDEM; computer simulation; concentrator-receiver system efficiency; orbital transfer; payload; solar bimodal power/propulsion systems; space power; space thermal propulsion; two-stage solar concentrators; Apertures; Hydrogen; Mirrors; Optical reflection; Orbital calculations; Payloads; Propulsion; Solar energy; Solar heating; Temperature;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Energy Conversion Engineering Conference, 1997. IECEC-97., Proceedings of the 32nd Intersociety
Conference_Location :
Honolulu, HI
Print_ISBN :
0-7803-4515-0
Type :
conf
DOI :
10.1109/IECEC.1997.659226
Filename :
659226
Link To Document :
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