DocumentCode
2008484
Title
Experimental confirmation of milliwatt power source concept
Author
Pustovalov, A. ; Gusev, V. ; Borshchevsky, A. ; Chmielewski, A.
Author_Institution
Sci. Production Enterprise BIAPOS, Moscow, Russia
fYear
1999
fDate
Aug. 29 1999-Sept. 2 1999
Firstpage
500
Lastpage
504
Abstract
The results of development and tests of mini RTG, milliwatt power source (PS) are presented. The development of PS model is based on the standard Light Weight Radioisotope Heater Unit (RHU) of 1.0 W thermal power, fueled by Plutonium-238. This RHU was successfully used on the spacecraft Galileo, Cassini, Mars Pathfinder etc. The computations were carried out and the optimum parameters of PS, for which maximum power can be achieved, were determined. Experimental samples of two PS modifications, equipped with electrical equivalents of RHU and thermoelectric batteries (TEB) made of Bi-Te-Sb-Se alloys, were fabricated: PS-1 (with one RPIU) and PS-2 (with two RI-IUs). The results of experimental tests have confirmed that an electrical power level of 25 mW can be achieved in PS-I and of 53 mW-in PS-2. The analysis of the calculations and experiments shows that the electrical power of PS-2 can be increased up to 70 mW at 5 V.
Keywords
radioisotope thermoelectric generators; space vehicle power plants; 1 W; 25 mW; 5 V; 53 mW; 70 mW; Bi-Te-Sb-Se; Bi-Te-Sb-Se alloys; Plutonium-238; Pu; electrical power level; milliwatt power source; mini RTG; radioisotope thermoelectric generator; standard Light Weight Radioisotope Heater Unit; thermal power; thermoelectric batteries; Batteries; Insulation; Leg; Mars; Planets; Radioactive materials; Space heating; Testing; Thermoelectricity; USA Councils;
fLanguage
English
Publisher
ieee
Conference_Titel
Thermoelectrics, 1999. Eighteenth International Conference on
Conference_Location
Baltimore, MD, USA
ISSN
1094-2734
Print_ISBN
0-7803-5451-6
Type
conf
DOI
10.1109/ICT.1999.843440
Filename
843440
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