NASA NTRS · 19900061970
Thermoelectric power conversion in space
Abstract
A radiatively-heated multicouple for use in the next generation of radioisotope thermoelectric generator (RTG) will employ 20 individual couples within a single cell, so that 40 n- and p-semiconductor legs will be interconnected in series. At the hot end of the RTG, the legs will be electrically interconnected using silicon molybdenum; on the cold side, the legs are interconnected by tungsten. The entire cell is then mechanically attached to a radiator, which conducts heat away and radiates it into space. Deep-space applications will use RTGs developed for vacuum operation; thermoelectric converter power systems using a unicouple configuration have flown on such missions as Pioneers 10 and 11, which used lead telluride thermoelectric converters, and Voyagers I and II, which used silicon germanium-based thermoelectrics.
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Awaya, Henry I., Ewell, Richard, Nesmith, Bill, Vandersande, James. 1990-09-01. Thermoelectric power conversion in space. https://ntrs.nasa.gov/citations/19900061970
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