Radioisotope heater unit: Difference between revisions
Zirconscot (talk | contribs) →Isotope: added Am-241 Isotope used by ExoMars rover. |
Zirconscot (talk | contribs) |
||
| Line 22: | Line 22: | ||
Radioisotope heater units for NASA missions have used plutonium-238<ref name="NASA Thermal Systems">NASA, [https://rps.nasa.gov/power-and-thermal-systems/thermal-systems/light-weight-radioisotope-heater-unit/ Thermal Systems]. Retrieved 23 June 2022.</ref> as the isotope for heat sources, since the radioactive half-life of 87.7 years means that the decay of the isotope will not limit the mission lifetime. The isotope produces 0.57 watts of thermal power per gram of <sup>238</sup>Pu.<ref>{{cite web|title=Assessment of Plutonium-238 production alternatives|url=https://www.energy.gov/sites/prod/files/NEGTN0NEAC_PU-238_042108.pdf|last=Miotla|first=Dennis|date=April 21, 2008|access-date=September 21, 2020|website=www.energy.gov|page=3}}</ref> |
Radioisotope heater units for NASA missions have used plutonium-238<ref name="NASA Thermal Systems">NASA, [https://rps.nasa.gov/power-and-thermal-systems/thermal-systems/light-weight-radioisotope-heater-unit/ Thermal Systems]. Retrieved 23 June 2022.</ref> as the isotope for heat sources, since the radioactive half-life of 87.7 years means that the decay of the isotope will not limit the mission lifetime. The isotope produces 0.57 watts of thermal power per gram of <sup>238</sup>Pu.<ref>{{cite web|title=Assessment of Plutonium-238 production alternatives|url=https://www.energy.gov/sites/prod/files/NEGTN0NEAC_PU-238_042108.pdf|last=Miotla|first=Dennis|date=April 21, 2008|access-date=September 21, 2020|website=www.energy.gov|page=3}}</ref> |
||
The ESA's [[ExoMars]] [[Rosalind Franklin rover]] will use [[americium-241]] RHUs. The half-life of Am-241 is five times that of <sup>238</sup>Pu. |
The ESA's [[ExoMars]] [[Rosalind Franklin rover]] will use [[americium-241]] RHUs. The half-life of Am-241 is five times that of <sup>238</sup>Pu, with a concomitant reduction in power-density. |
||
Soviet missions have used other isotopes, such as the [[polonium-210]] heat source used in the [[Lunokhod]] lunar rovers.<ref>Blair, Sean (March 14, 2011)." [https://eandt.theiet.org/content/articles/2011/03/rovers-learning-from-lunokhod/ Rovers learning from Lunokhod]", ''E&T News''. Retrieved 23 June 2022.</ref><ref name=Wang>{{Cite journal|doi=10.1016/j.rser.2019.109572 |hdl=1721.1/129634 |hdl-access=free |title=Critical design features of thermal-based radioisotope generators: A review of the power solution for polar regions and space |year=2020 |last1=Wang |first1=Xiawa |last2=Liang |first2=Renrong |last3=Fisher |first3=Peter |last4=Chan |first4=Walker |last5=Xu |first5=Jun |journal=Renewable and Sustainable Energy Reviews |volume=119 |page=109572 |s2cid=209776036 }} </ref> With a half-life of 138.376 days, polonium-210 produces more thermal power per unit mass, but is suitable only for shorter duration missions. [[Strontium-90]] has also been proposed.<ref name=Wang /> |
Soviet missions have used other isotopes, such as the [[polonium-210]] heat source used in the [[Lunokhod]] lunar rovers.<ref>Blair, Sean (March 14, 2011)." [https://eandt.theiet.org/content/articles/2011/03/rovers-learning-from-lunokhod/ Rovers learning from Lunokhod]", ''E&T News''. Retrieved 23 June 2022.</ref><ref name=Wang>{{Cite journal|doi=10.1016/j.rser.2019.109572 |hdl=1721.1/129634 |hdl-access=free |title=Critical design features of thermal-based radioisotope generators: A review of the power solution for polar regions and space |year=2020 |last1=Wang |first1=Xiawa |last2=Liang |first2=Renrong |last3=Fisher |first3=Peter |last4=Chan |first4=Walker |last5=Xu |first5=Jun |journal=Renewable and Sustainable Energy Reviews |volume=119 |page=109572 |s2cid=209776036 }} </ref> With a half-life of 138.376 days, polonium-210 produces more thermal power per unit mass, but is suitable only for shorter duration missions. [[Strontium-90]] has also been proposed.<ref name=Wang /> |
||
Latest revision as of 01:06, 26 October 2024
 | This article needs additional citations for verification. (December 2018) |
A radioisotope heater unit (RHU) is a small device that provides heat through radioactive decay.[1] They are similar to tiny radioisotope thermoelectric generators (RTG) and normally provide about one watt of heat each, derived from the decay of a few grams of plutonium-238—although other radioactive isotopes could be used. The heat produced by these RHUs is given off continuously for several decades and, theoretically, for up to a century or more.[2]
In spacecraft, RHUs are used to keep other components at their operational temperatures, which may be very different to the temperature of other parts of the spacecraft. In the vacuum of space any part of the spacecraft which doesn't receive direct sunlight will cool down so much that electronics or delicate scientific instruments break down. They are simpler and more reliable than other ways of keeping components warm, such as electric heaters.[2]
Spacecraft use
[edit]
Most lunar and Martian surface probes use RHUs for heat, including many probes that use solar panels rather than RTGs to generate electricity. Examples include the seismometer deployed on the Moon by Apollo 11 in 1969, which contained 1.2 ounces (34 grams) of plutonium-238; Mars Pathfinder; and the Mars Exploration Rovers Spirit and Opportunity.[3] RHUs are especially useful on the Moon because of its lengthy and cold two-week night.
Virtually every deep space mission beyond Mars uses both RHUs and RTGs. Solar insolation decreases with the square of the distance from the Sun, so additional heat is needed to keep spacecraft components at nominal operating temperature. Some of this heat is produced electrically because it is easier to control, but electrical heaters are far less efficient than a RHU because RTGs convert only a few percent of their heat to electricity and reject the rest to space.
The Cassini–Huygens spacecraft sent to Saturn contained eighty-two of these units (in addition to three main RTGs for power generation). The associated Huygens probe contained thirty-five.
ISRO included two radioisotope heater units developed by India's Department of Atomic Energy (DAE) in the propulsion module of Chandrayaan-3 on a trial basis which worked flawlessly.[4]
Isotope
[edit]Radioisotope heater units for NASA missions have used plutonium-238[3] as the isotope for heat sources, since the radioactive half-life of 87.7 years means that the decay of the isotope will not limit the mission lifetime. The isotope produces 0.57 watts of thermal power per gram of 238Pu.[5]
The ESA's ExoMars Rosalind Franklin rover will use americium-241 RHUs. The half-life of Am-241 is five times that of 238Pu, with a concomitant reduction in power-density.
Soviet missions have used other isotopes, such as the polonium-210 heat source used in the Lunokhod lunar rovers.[6][7] With a half-life of 138.376 days, polonium-210 produces more thermal power per unit mass, but is suitable only for shorter duration missions. Strontium-90 has also been proposed.[7]
Comparison of RHU with RTG
[edit]While both RHUs and Radioisotope Thermoelectric Generators (RTGs) use the decay heat of a radioactive isotope, RHUs are generally much smaller as a result of omitting the thermocouples and heat sinks/radiators required to generate electricity from heat. Both RHUs and RTGs feature rugged, heat-resistant casings to safely contain the radioisotope in the event of a launch or re-entry vehicle failure. The total mass of a single one-watt RHU (including shielding) is about 40 grams. Similar schemes, such as thermionic generators, have also been used.
GPHS
[edit]The United States Department of Energy has developed the general-purpose heat source (GPHS) primarily for space use. These GPHSs can be used individually or in groups of up to eighteen for component heating, but are primarily used as the heat source for RTGs. Each GPHS contains four iridium-clad Pu-238 fuel pellets, standing 5 cm tall, 10 cm square and weighs 1.44 kg.
See also
[edit]
- Nuclear fuel
- Radioisotope generator
- Stirling radioisotope generator
- Radioisotope thermoelectric generator
References
[edit]- ^ NASA (2016). Radioisotope Heater Units, NASAFacts. Retrieved 23 June 2022.
- ^ a b "Department of Energy Facts: Radioisotope Heater Units" (PDF). U.S. Department of Energy, Office of Space and Defense Power Systems. December 1998. Archived from the original (PDF) on 2016-08-10. Retrieved March 24, 2010.
- ^ a b NASA, Thermal Systems. Retrieved 23 June 2022.
- ^ Laxman, Srinivas (2023-12-29). "Nuclear sector set to power Indian space missions: Isro chief". The Times of India. ISSN 0971-8257. Retrieved 2023-12-29.
- ^ Miotla, Dennis (April 21, 2008). "Assessment of Plutonium-238 production alternatives" (PDF). www.energy.gov. p. 3. Retrieved September 21, 2020.
- ^ Blair, Sean (March 14, 2011)." Rovers learning from Lunokhod", E&T News. Retrieved 23 June 2022.
- ^ a b Wang, Xiawa; Liang, Renrong; Fisher, Peter; Chan, Walker; Xu, Jun (2020). "Critical design features of thermal-based radioisotope generators: A review of the power solution for polar regions and space". Renewable and Sustainable Energy Reviews. 119: 109572. doi:10.1016/j.rser.2019.109572. hdl:1721.1/129634. S2CID 209776036.
External links
[edit]- NASA Radioisotope Power Systems website – RHU page
- Radioisotope heater unit fact sheet from NASA's Cassini mission website