The Multihundred-Watt radioisotope thermoelectric generator (MHW RTG) is a type of US radioisotope thermoelectric generator (RTG) developed for the Voyager spacecraft, Voyager 1 and Voyager 2.[1]
Each RTG has a total weight of 37.7 kg including about 4.5 kg of Pu-238[2] and uses 24 pressed plutonium-238 oxide spheres to provide enough heat to generate approximately 157 Watts of electrical power initially – halving every 87.7 years.[3]
Each RTG initially generated about 2400 Watts of thermal power.[4] Conversion of the decay heat of the plutonium to electrical power uses 312 silicon-germanium (SiGe) thermoelectric couples. The initial thermoelectric couple hot junction temperature was 1273 K (1000 °C, 1832 °F) with a cold junction temperature of 573 K (300 °C, 572 °F).[5]
Each Voyager spacecraft has 3 RTGs. Collectively, the RTGs supply each Voyager spacecraft with 470 Watts at launch.[6][7]
MHW-RTGs were used on the Lincoln Experimental Satellites 8 and 9.
Subsequent US spacecraft used the GPHS-RTG which used similar SiGe thermoelectric devices but a different packaging of the fuel.
The MMRTG is a newer RTG type, used on the Curiosity rover.
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RTG heat source unit
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RTG diagram 1
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RTG unit
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RTG Safety Tests
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"Uptime 15,364 days - The Computers of Voyager" by Aaron Cummings
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How Long Will the Voyager Spacecraft Last?
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References
- ^ Heacock (1980). "The Voyager Space Craft". Proceedings of the Institution of Mechanical Engineers. 194: 267–270. doi:10.1243/PIME_PROC_1980_194_026_02. Archived from the original on 2014-03-31.
- ^ "Space Nuclear Power" G.L.Bennett 2006
- ^ "NASA Celebrates 45 Years of Voyager 1, Enabled by Radioisotope Power". NASA. September 5, 2022. Retrieved December 11, 2022.
- ^ "Totse.com | Nuclear Power in Space". Archived from the original on 2008-06-19. Retrieved 2012-10-19.
- ^ Furlong, Richard R.; Wahlquist, Earl J. (1999). "U.S. space missions using radioisotope power systems" (PDF). Nuclear News. 42 (4): 26–34. Archived from the original (PDF) on 2018-10-16. Retrieved January 2, 2011.
- ^ "VOYAGER 2:Host Information". NASA. 1989. Archived from the original on July 21, 2011. Retrieved January 2, 2011.
- ^ "Voyager 2 Craft Details". NASA-NSSDC-Spacecraft-Details. NASA. Retrieved March 9, 2011.
See also
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This page was last edited on 11 April 2023, at 03:46