... according to Atomic Insights:
The only planned use of RTGs in the US space program in the near term is the unmanned, 1997 Cassini mission to explore Saturn. The Cassini spacecraft will be powered by three General Purpose Heat Source Radioisotope Thermal Generators (GPHS RTGs) each designed to provide 276 W of electrical power at the beginning of the mission.
The GPHS RTGs planned for use on Cassini are nearly identical in design to those used on Voyager 1 and 2 and Lincoln Experimental Satellites (LES) 8 and 9. These RTGs have been in continuous operation for 21 years (LES 8/9) and 20 years (Voyager 1/2). Nearly all of the degradation that these devices have experienced during their lives is due to the decay of the plutonium heat source.
The three RTGs that will be on the Cassini spacecraft each weigh 56 kilograms, have a diameter of 42.2 cm and a length of 114 cm. Like the SNAP-27 that served as a power source on the moon during the Apollo mission, the GPHS RTG consists of a cylindrical fuel supply surrounded by rings of thermocouples. Again, there are cooling fins attached to the cold shoes of the thermocouples.
Plutonium-238 is the fuel source. The fuel elements are modularized with each module producing approximately 250 watts of thermal power. The fuel modules are encased in a heat and impact resistant shell designed to prevent any postulated vehicle accident from releasing plutonium. Sufficient testing has been done to show that the modules will remain intact, even in a Challenger type launch explosion or a reentry accident.
This is the description of the power pack used on the lunar lander and for outside experiments:
SNAP-27 Characteristics
The SNAP-27 power supply weighed about 20 kilograms, was 46 cm long and 40.6 cm in diameter. It consisted of a central fuel capsule surrounded by concentric rings of thermocouples. Outside of the thermocouples was a set of fins to provide for heat rejection from the cold side of the thermocouple.
Each of the SNAP devices produced approximately 75 W of electrical power at 30 VDC. The energy source for each device was a rod of plutonium-238 weighing approximately 2.5 kilograms and providing a thermal power of approximately 1250 W.
Even though the only radiation from Pu-238 is alpha particles which require little shielding, it is necessary to use thick gloves when handling a 2.5 kilogram rod of Pu-238. The surface temperature will reach about 500 degrees C because of the energy being released by radioactive decay. After ten years of continuous power output, a Pu-238 based RTG will still produce 92% of its initial power.
One measure of performance that is often used for chemical storage batteries is the amp-hour. A modern battery might have a capacity of 1.5 amp-hrs/kg. The SNAP-27 power supplies demonstrated the ability to provide more than 4380 amp-hrs/kg during the four years that their performance was monitored. Similar RTGs have produced 24,000 amp-hrs/kg during a 20 year operating life and are still going strong.
Use of, say, Peltier-effect chips instead of thermocouples might raise the efficiency quite a bit, reducing the amount necessary, although engineering for those temperatures might be a bit of a trick. :) Or, they could be used on the outside of the container, or on the heat sinks on the cold end of the thermocouples in a kind of co-generation scheme.
Cheers.