Radionuclide heating element

Radionuclide heating elements are used in space travel and, by breaking down a small amount of a radionuclide, provide heat to heat cold-sensitive parts of a space probe , lander or rover .
Differentiation from radionuclide batteries
In contrast to radionuclide batteries , which are primarily used to generate electricity, the focus of heating elements is the decay heat from radioactivity. It is used to heat sensitive equipment (e.g. electronics) in spacecraft. Radionuclide batteries have a low degree of efficiency in converting the decay heat into electricity, but the unconverted part of the power can also be used for heating.
construction
The use of different radioisotopes is possible depending on the length of the mission, heat requirements and other criteria . The RHU (Radioisotope Heater Unit) manufactured by the United States each contain a pellet of 2.7 g of plutonium dioxide . This "fuel" is surrounded by a shell made of a platinum-rhodium alloy, which is in an insulation made of graphite and this in turn is in a heat shield made of the same material. The total mass of a single RHU, including the shield, is approximately 40 grams. A RHU is 3.2 cm long and 2.6 cm in diameter, the heat output is 1 watt .
use
In the cold outer solar system, space probes and landers often use radionuclide heating elements in cold-sensitive areas, even if they get their electrical energy from RTGs . In the case of battery-operated immersion and landing capsules in the outer solar system, the use of radionuclide heating elements has so far been the standard in order to prevent cooling. The battery power of these capsules is only sufficient for the relatively short measuring phase. In the inner solar system, landers and rovers on planets and moons use radionuclide heating elements in order not to cool down in the absence of solar radiation, even if they draw their energy from solar cells during the day . Battery systems for storing energy for heating during the night are often too heavy.
The Soviet Lunochod moon rovers used heating elements with Polonium 210 Po, while the American Mars rovers and probes used plutonium 238 Pu in their heating elements. The Chinese rover Yutu of the Chang'e-3 moon lander also uses plutonium 238 Pu in its heating elements so as not to cool down during the 14-day moon night.
year | Surname | mission | number | Radioisotope |
---|---|---|---|---|
1969 | 15 watt RHU | EASEP | 2 | 238 Pu |
1970 | V3-R70-4 | Lunochod 1 | ? | 210 Po |
1972 | RHU | Pioneer 10 | 12 | 238 Pu |
1973 | V3-R70-4 | Lunochod 2 | ? | 210 Po |
1973 | RHU | Pioneer 11 | 12 | 238 Pu |
1977 | RHU | Voyager 1 | 9 | 238 Pu |
1977 | RHU | Voyager 2 | 9 | 238 Pu |
1989 | RHU | Galileo Orbiter | 103 | 238 Pu |
1989 | RHU | Galileo rehearsal | 17th | 238 Pu |
1996 | RHU | Mars Pathfinder Rover | 3 | 238 Pu |
1997 | RHU | Cassini orbiter | 82 | 238 Pu |
1997 | RHU | Huygens Lander | 35 | 238 Pu |
2003 | RHU | Spirit | 8th | 238 Pu |
2003 | RHU | Opportunity | 8th | 238 Pu |
2011 | RHU | Mars Science Laboratory | ? | 238 Pu |
2013 | ? | Yutu | ? | 238 Pu |
swell
- ↑ DOE: Radioisotope Heating Unit , accessed: May 24, 2012 ( Memento from August 5, 2012 in the web archive archive.today )
- ↑ http://www.bernd-leitenberger.de/luna.shtml Bernd Leitenberger: Das Luna Programm , accessed: May 24, 2012
- ↑ a b Günther Glatzel: Chang'e 3 on the way to the moon , in Raumfahrer.net, accessed December 1, 2013, date: December 3, 2013
- ↑ http://space.skyrocket.de/doc_sat/nuclear.htm Guenter's Space Page: Nuclear Powered Payloads , accessed: May 24, 2012
- ↑ http://solarsystem.nasa.gov/rps/rhu.cfm NASA: Radioisotope Power Systems, Radioisotope Heater Unit , accessed: May 24, 2012