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RADIOISOTOPE THERMOELECTRIC
GENERATOR
SUBMITTED BY:
GUIDED BY:
INTRODUCTION
 A radioisotope thermoelectric generator
(RTG, RITEG) is an electrical generator that
obtains its power from radioactive decay.
 In this device, the heat released by the decay
of a suitable radioactive material is converted
into electricity by the See beck effect using an
array of thermocouples.
TYPICAL CUT-OUT OF RTG
CONSTRUCTION & DESIGN
 The design of an RTG is simple by
the standards of nuclear technology
the main component is a sturdy
container of a radioactive material
(the fuel).
 Thermocouples are placed in the
walls of the container, with the
outer end of each thermocouple
connected to a heat sink.
 Radioactive decay of the fuel
produces heat which flows through
the thermocouples to the heat sink,
generating electricity in the process.
Desirable Characteristics of
Fuel For RTG
 High energy output
 Easy absorption and conversion into thermal
radiation
 Long half life
 High specific power output
 Low shielding requirements
A PLUTONIUM238Pu
PELLET
FUELS(ISOTOPES)
 Plutonium-238
 curium-244
 strontium-90
 polonium-210
 promethium-147,
 caesium-137,
 cerium-144, ruthenium-106, cobalt-60, etc..
Potential Fuels for RTG
238Pu 90Sr 210Po 241Am
Shielding
(mm of lead)
2.5 16 100 18
Half life (years) 87.7 28.78 0.38 432.7
Specific Power
(Wg-1)
0.448 0.128 17.81 0.089
Characteristic Of Fuels
LIFESPAN
 Most RTGs use 238Pu, which
decays with a half-life of 87.7
years. RTGs using this material
will therefore diminish in power
output by 0.787% of their
capacity per year. 23 years after
production, such an RTG will
have decreased in power by
16.6%, i.e. providing 83.4% of its
initial output.Thus, with a
starting capacity of 470W, after
23 years it would have a capacity
of 392W.
EFFICIENCY
 Higher efficiency means less radioactive fuel is
needed to produce the same amount of power and
therefore a lighter overall weight for the generator.
 Thermocouples used in RTGs are very reliable and
long lasting, but are very inefficient.
 So efficiency above 10% have never been achieved
and most RTGs have efficiency between 3 to 7 %.
SAFETY
 RTGs may pose a risk of
radioactive contamination:
if the container holding the
fuel leaks, the radioactive
material may contaminate
the environment.
 Iridium cladding
 Graphite aero-impact shell
 Composite covering
 Alloying
Applications
 Used as power sources in satellites, space probes
and unmanned remote facilities.
 Used as power sources for navigation beacons,
radio beacons, light houses and weather
stations.
 Used at places where solar cells are not viable.
 Most desirable power source for unmanned and
unmaintained situations needing a few 100 watts
or less of power of durations too long for fuel
cells, batteries and generators.
Challenges
 Low overall efficiencies (6 - 7%)
 Degradation of thermoelectric elements
 Design of effective thermal path
 Breakdown of insulators
THANKYOU!!!

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Generator for space shuttles-Radioisotope thermoelectric generator

  • 2. INTRODUCTION A radioisotope thermoelectric generator (RTG, RITEG) is an electrical generator that obtains its power from radioactive decay. In this device, the heat released by the decay of a suitable radioactive material is converted into electricity by the See beck effect using an array of thermocouples.
  • 4. CONSTRUCTION & DESIGN The design of an RTG is simple by the standards of nuclear technology the main component is a sturdy container of a radioactive material (the fuel). Thermocouples are placed in the walls of the container, with the outer end of each thermocouple connected to a heat sink. Radioactive decay of the fuel produces heat which flows through the thermocouples to the heat sink, generating electricity in the process.
  • 5. Desirable Characteristics of Fuel For RTG High energy output Easy absorption and conversion into thermal radiation Long half life High specific power output Low shielding requirements A PLUTONIUM238Pu PELLET
  • 6. FUELS(ISOTOPES) Plutonium-238 curium-244 strontium-90 polonium-210 promethium-147, caesium-137, cerium-144, ruthenium-106, cobalt-60, etc..
  • 7. Potential Fuels for RTG 238Pu 90Sr 210Po 241Am Shielding (mm of lead) 2.5 16 100 18 Half life (years) 87.7 28.78 0.38 432.7 Specific Power (Wg-1) 0.448 0.128 17.81 0.089
  • 9. LIFESPAN Most RTGs use 238Pu, which decays with a half-life of 87.7 years. RTGs using this material will therefore diminish in power output by 0.787% of their capacity per year. 23 years after production, such an RTG will have decreased in power by 16.6%, i.e. providing 83.4% of its initial output.Thus, with a starting capacity of 470W, after 23 years it would have a capacity of 392W.
  • 10. EFFICIENCY Higher efficiency means less radioactive fuel is needed to produce the same amount of power and therefore a lighter overall weight for the generator. Thermocouples used in RTGs are very reliable and long lasting, but are very inefficient. So efficiency above 10% have never been achieved and most RTGs have efficiency between 3 to 7 %.
  • 11. SAFETY RTGs may pose a risk of radioactive contamination: if the container holding the fuel leaks, the radioactive material may contaminate the environment. Iridium cladding Graphite aero-impact shell Composite covering Alloying
  • 12. Applications Used as power sources in satellites, space probes and unmanned remote facilities. Used as power sources for navigation beacons, radio beacons, light houses and weather stations. Used at places where solar cells are not viable. Most desirable power source for unmanned and unmaintained situations needing a few 100 watts or less of power of durations too long for fuel cells, batteries and generators.
  • 13. Challenges Low overall efficiencies (6 - 7%) Degradation of thermoelectric elements Design of effective thermal path Breakdown of insulators