DocumentCode :
2563272
Title :
A Brayton cycle solar dynamic heat receiver for space
Author :
Sedgwick, L.M. ; Nordwall, H.L. ; Kaufmann, K.J. ; Johnson, S.D.
Author_Institution :
Boeing Aerosp. & Electron., Seattle, WA, USA
fYear :
1989
fDate :
6-11 Aug 1989
Firstpage :
905
Abstract :
The detailed design of a heat receiver developed to meet the requirements of the US Space Station Freedom, which will be assembled and operated in low Earth orbit beginning in the mid-1990s, is described. The heat receiver supplies thermal energy to a nominal 25 kW closed-Brayton-cycle power conversion unit. The receiver employs an integral thermal energy storage system utilizing the latent heat of a eutectic-salt phase-change mixture to store energy for eclipse operation. The salt is contained within a felt metal matrix which enhances heat transfer and controls the salt void distribution during solidification
Keywords :
heat engines; heat transfer; latent heat; space vehicle power plants; thermal energy storage; 25 kW; Brayton cycle solar dynamic heat receiver; Space Station Freedom; eutectic-salt phase-change mixture; heat transfer; integral thermal energy storage system; latent heat; power conversion unit; salt void distribution; solidification; Aerodynamics; Aerospace electronics; Energy storage; Multichip modules; Power conversion; Solar heating; Space heating; Space stations; Space technology; Testing;
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.1989.74576
Filename :
74576
Link To Document :
بازگشت