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Radioisotope heater units (RHU) are small devices that provide 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

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.

Isotope

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. Soviet missions have used other isotopes, such as the Polonium-210 heat source used in the Lunokhod lunar rovers.^[4]^[5] With a half-life of about 4+1⁄2 months, Po-210 produces more power per unit mass, but is suitable only for shorter duration missions. Strontium-90 has also been proposed.^[5]

Comparison of RHU with RTG

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 RHU (including shielding) is about 40 grams. Similar schemes, such as thermionic generators, have also been used.

GPHS

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.

References

^ 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.
^ Blair, Sean (March 14, 2011)." Rovers learning from Lunokhod", E&T News. Retrieved 23 June 2022.
^ ^a ^b Wang, Xiawa, et al. (2019).Critical design features of thermal-based radioisotope generators: A review of the power solution for polar regions and space", Renewable & Sustainable Energy Reviews. Retrieved 23 June 2022.

External links

NASA Radioisotope Power Systems website – RHU page
Radioisotope heater unit fact sheet from NASA's Cassini mission website

[1] NASA (2016). Radioisotope Heater Units, NASAFacts. Retrieved 23 June 2022.

[doe1-2] "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.

[NASA_Thermal_Systems-3] NASA, Thermal Systems. Retrieved 23 June 2022.

[4] Blair, Sean (March 14, 2011)." Rovers learning from Lunokhod", E&T News. Retrieved 23 June 2022.

[Wang-5] Wang, Xiawa, et al. (2019).Critical design features of thermal-based radioisotope generators: A review of the power solution for polar regions and space", Renewable & Sustainable Energy Reviews. Retrieved 23 June 2022.

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@@ Line 3: / Line 3: @@
 {{more citations needed|date=December 2018}}
 [[Image:Radioisotope heater unit.gif|thumb|right|Diagram of a radioisotope heater unit]]
-'''Radioisotope heater units''' ('''RHU''') are small devices that provide heat through [[radioactive decay]]. They are similar to tiny [[radioisotope thermoelectric generator]]s (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.<ref name=doe1>{{Cite web  | title = Department of Energy Facts: Radioisotope Heater Units
+'''Radioisotope heater units''' ('''RHU''') are small devices that provide heat through [[radioactive decay]].<ref>NASA (2016). [https://rps.nasa.gov/system/downloadable_items/31_Final_RHU_Fact_Sheet_2016_5-26-16.pdf Radioisotope Heater Units], NASAFacts. Retrieved 23 June 2022.</ref> They are similar to tiny [[radioisotope thermoelectric generator]]s (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.<ref name=doe1>{{Cite web  | title = Department of Energy Facts: Radioisotope Heater Units
   | publisher = U.S. Department of Energy, Office of Space and Defense Power Systems  | date = December 1998   | url = https://saturn.jpl.nasa.gov/system/downloadable_items/291_rhu.pdf | archive-url = https://web.archive.org/web/20160810043227/https://saturn.jpl.nasa.gov/system/downloadable_items/291_rhu.pdf | url-status = dead | archive-date = 2016-08-10 | access-date = March 24, 2010}}</ref>
@@ Line 9: / Line 9: @@
 == Spacecraft use ==
-[[File:RHU parts.jpg|right|thumb|'''RHU''' Photo of a disassembled RHU. RHUs use Pu-238 to generate about 1 watt of heat each.]] 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 [[ALSEP#Apollo_11_.28EASEP.29|seismometer deployed]] on the Moon by [[Apollo 11]] in 1969, which contained 1.2&nbsp;ounces (34 grams) of plutonium-238; [[Mars Pathfinder]]; and the [[Mars Exploration Rovers]] ''[[Spirit (rover)|Spirit]]'' and ''[[Opportunity (rover)|Opportunity]]''. RHUs are especially useful on the Moon because of its lengthy and cold two-week night.
+[[File:RHU parts.jpg|right|thumb|'''RHU''' Photo of a disassembled RHU. RHUs use Pu-238 to generate about 1 watt of heat each.]] 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 [[ALSEP#Apollo_11_.28EASEP.29|seismometer deployed]] on the Moon by [[Apollo 11]] in 1969, which contained 1.2&nbsp;ounces (34 grams) of plutonium-238; [[Mars Pathfinder]]; and the [[Mars Exploration Rovers]] ''[[Spirit (rover)|Spirit]]'' and ''[[Opportunity (rover)|Opportunity]]''.<ref name="NASA Thermal Systems"/> RHUs are especially useful on the Moon because of its lengthy and cold two-week night.
 Virtually every [[outer space|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)|Huygens]]'' probe contained thirty-five.
+===Isotope===
+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. 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>Wang, Xiawa, ''et al.'' (2019).[https://pdf.sciencedirectassets.com/271969/1-s2.0-S1364032119X00179/1-s2.0-S1364032119307804/am.pdf Critical design features of thermal-based radioisotope generators: A review of the power solution for polar regions and space]", ''Renewable & Sustainable Energy Reviews''. Retrieved 23 June 2022.</ref> With a half-life of about 4+1⁄2 months, Po-210 produces more power per unit mass, but is suitable only for shorter duration missions. [[Strontium-90]] has also been proposed.<ref name=Wang />
 ===Comparison of RHU with RTG===
-While both RHUs and [[Radioisotope Thermoelectric Generator]]s (RTGs) use the decay heat of a radioactive isotope (usually Pu-238), RHUs are generally much smaller as a result of omitting the [[thermocouple]]s 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 RHU (including shielding) is about 40&nbsp;grams. Similar schemes, such as [[Thermionic converter|thermionic generators]], have also been used.
+While both RHUs and [[Radioisotope Thermoelectric Generator]]s (RTGs) use the decay heat of a radioactive isotope, RHUs are generally much smaller as a result of omitting the [[thermocouple]]s 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 RHU (including shielding) is about 40&nbsp;grams. Similar schemes, such as [[Thermionic converter|thermionic generators]], have also been used.
 ==GPHS==
-The [[United States Department of Energy]] has developed the [[general-purpose heat source]] (GPHS) primarily for space use. These GPHSes 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&nbsp;cm tall, 10&nbsp;cm square and weighs 1.44&nbsp;kg.
+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&nbsp;cm tall, 10&nbsp;cm square and weighs 1.44&nbsp;kg.
 ==See also==