DocumentCode
2543474
Title
Design of the Space Station Freedom power system
Author
Thomas, Ronald L. ; Hallinan, George J.
Author_Institution
NASA Lewis Res. Center, Cleveland, OH, USA
fYear
1989
fDate
6-11 Aug 1989
Firstpage
245
Abstract
The design of Space Station Freedom´s electric power system (EPS) is reviewed, highlighted the key design goals of performance, low cost, reliability and safety. Tradeoff study results that illustrate the competing factors responsible for many of the more important design decisions are discussed. When Freedom´s EPS is compared with previous space power designs, two major differences stand out. The first is the size of the EPS, which is larger than any prior system. The second major difference between the EPS and other space power designs is the indefinite expected life of Freedom; 30 years has been used for life-cycle-cost calculations
Keywords
design engineering; power systems; space vehicle power plants; Space Station Freedom; cost; design; life; performance; power system; reliability; safety; space power; Costs; Nuclear power generation; Photovoltaic systems; Power generation; Power system reliability; Power systems; Satellites; Solar power generation; Space shuttles; 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.1989.74470
Filename
74470
Link To Document