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The '''radioisotope rocket''' is a type of [[rocket engine]] that uses the heat generated by the decay of [[radioactive]] elements to heat a [[working fluid]], which is then exhausted through a
The basic idea is a development of existing [[radioisotope thermoelectric generator]], or RTG, systems, in which the heat generated by decaying nuclear fuel is used to generate power. In the rocket application the generator is removed, and the working fluid is instead used to produce thrust directly. Temperatures of about 1500 to 2000°C are possible in this sytem, allowing for [[specific impulse]]s of about 700 to 800 seconds (7 to 8 kN·s/kg), about double that of the best chemical engines such as the [[LH2]]-[[LOX]] [[SSME]].
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[[TRW]] maintained a fairly active development program known as '''Poodle''' from 1961 to 1965, and today the systems are still often known as '''Poodle thrusters'''. The name was a play on the larger systems being developed under '''Project Rover''', which led to NERVA. In April 1965 they ran their testbed engine for 65 hours at about 1500°C, producing a specific impulse of 650 to 700 seconds (6.5 to 7 kN·s/kg).
The inadvertant construction of a radioisotope rocket is one of the suggested solutions to the [[Pioneer
[[Category:Nuclear spacecraft propulsion]]
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