Thermoelectric Alloys and Devices for Radioisotope Space Power Systems: State of the Art and Current Developments

Technical Report · Sun Jan 01 00:00:00 EST 1989

DOI:https://doi.org/10.2172/1033425· OSTI ID:1033425

Barnett, W. ^[1]; Dick, P. ^[2]; Beaudry, B. ^[3]; Gorsuch, P ^[4]; Skrabek, E. ^[5]

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1. US Department of Energy (USDOE), Washington, DC (United States)
2. Teledyne Energy Systems, Timonium, MD (United States)
3. Ames Laboratory (AMES), Ames, IA (United States)
4. H. L. Yoh Co., Philadelphia, PA (United States)
5. Fairchild Space Company, Germantown, MD (United States)

Lead telluride and silicon germanium type alloys have served over the past several decades as the preferred thermoelectric conversion materials for U. S. radioisotope thermoelectric generator (RTG) power systems for planetary deep space exploration missions. The Pioneer missions to Jupiter and Jupiter/Saturn and the Viking Mars Lander missions employed TAGS-2N (lead and germanium telluride derivatives) power conversion devices. Since 1976, silicon germanium (SiGe) alloys, incorporated into the unicouple device, have evolved as the thermoelectric materials of choice for U. S. RTG powered space missions. These include the U. S. Air Force Lincoln Experimental Satellites 8 & 9 for communications, in 1976, followed in 1977 by the National Aeronautics and Space Administration Voyager 1 and 2 planetary missions. In 1989, advanced SiGe RTGs were used to power the Galileo exploration of Jupiter and, in 1990, will be used to power the Ulysses investigation of the Sun. In addition, SiGe technology has been chosen to provide RTG power for the 1995 Comet Rendezvous and Asteroid Flyby mission and the 1996 Cassini Saturn orbiter mission. Summaries of the flight performance data for these systems are presented.; Current U. S. Department of Energy thermoelectric development activities include (1) the development of conversion devices based on hi-density, close packed couple arrays and (2) the development of improved performance silicon germanium type thermoelectric materials. The silicon germanium type "multicouple", being developed in conjunction with the Modular RTG program, is discussed in a companion paper. A lead telluride type close-packed module, discussed herein, offers the promise of withstanding high velocity impacts and, thus, is a candidate for a Mars Penetrator application.; Recent projects sponsored by the U. S. Department of Energy, including the Improved Thermoelectric Materials and Modular Radioisotope Thermoelectric Generator programs, have shown that improvements in silicon germanium thermoelectric energy conversion capabilities of at least 50 percent can be achieved by tailoring the characteristics of the silicon germanium alloy materials and devices. This paper compares the properties and characteristics of the SiGe alloys now being developed with those used in the operational space power system.

• Research Organization: US Department of Energy (USDOE), Washington, DC (United States); Teledyne Energy Systems, Timonium, MD (United States); Ames Laboratory (AMES), Ames, IA (United States); H. L. Yoh Co., Philadelphia, PA (United States); Fairchild Space Company, Germantown, MD (United States)
• Sponsoring Organization: USDOE Office of Nuclear Energy (NE), Office of Space and Defense Power Systems (NE-75)
• OSTI ID: 1033425
• Country of Publication: United States
• Language: English

Related Subjects

Conversion materials
Devices
Galileo
Jupiter
NESDPS Office of Nuclear Energy Space and Defense Power Systems
PIONEER
RTG
Radioisotope Space Power Systems
Saturn
SiGe
Silicon Germanium
Thermoelectric Alloys
Unicouple
Viking Mars Lander
Voyager 1 & 2