DocumentCode :
2271821
Title :
Development of segmented thermoelectric multicouple converter technology
Author :
Fleurial, Jean-Pierre ; Johnson, Kenneth ; Mondt, Jack ; Sakamoto, Jeff ; Snyder, Jeff ; Huang, Chen-Kuo ; Blair, Richard ; Stapfer, Gerhard ; Caillat, Thierry ; Frye, Patrick ; Determan, William ; Heshmatpour, B. ; Brooks, Michael ; Tuttle, Karen
Author_Institution :
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA
fYear :
0
fDate :
0-0 0
Abstract :
The Jet Propulsion Laboratory (JPL), Pratt & Whitney Rocketdyne, and Teledyne Energy Systems, Inc., have teamed together under JPL leadership to develop the next generation of advanced thermoelectric space reactor power conversion systems. The program goals are to develop the technologies needed to achieve a space nuclear power system specific mass goal of less than 30 kg/kW at the 100 kW power level with a greater than 15 year lifetime. The technologies required for such a power system include liquid metal cooled reactors with outlet temperatures ranging from 1125 K up to 1325 K, segmented thermoelectric multicouple converter (STMC) arrays which can achieve greater than 8 percent system efficiency and carbon-carbon heat pipe radiator panels to reduce the radiator subsystem areal density to a goal of 5 kg/m . The STMC program´s development efforts focused on a highly compact conductively coupled modular thermoelectric converter assembly (TCA) design. STMC design efforts were based on a multicouple design similar to the SP-100 Program´s design but using segmented thermoelectric (TE) legs rather than the single alloy silicon-germanium legs. Efforts have addressed in parallel the selection and optimization of the most promising high temperature thermoelectric materials, the development of the various STMC components and sub-assemblies, design, analysis, fabrication and assembly of subscale STMC devices as well as scale-up plans to the 100 kW-class power level. The performance of the selected high temperature TE materials and initial thermal, electrical and mechanical test results on several STMC demonstration devices are reported
Keywords :
electric propulsion; heat pipes; high-temperature electronics; nuclear power stations; power convertors; space vehicle power plants; thermoelectric conversion; 100 kW; 1125 to 1325 K; Jet Propulsion Laboratory; Pratt & Whitney Rocketdyne; Teledyne Energy Systems; electric propulsion; energy conversion; heat pipe radiator; high temperature thermoelectric materials; segmented thermoelectric multicouple converters; space nuclear power system; thermoelectric space reactor power conversion; Assembly; Inductors; Laboratories; Leg; Power systems; Propulsion; Space technology; Tellurium; Temperature; Thermoelectricity; Energy conversion; electric propulsion; nuclear power; thermoelectric;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2006 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
0-7803-9545-X
Type :
conf
DOI :
10.1109/AERO.2006.1656006
Filename :
1656006
Link To Document :
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