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Radioisotope rocket: Difference between revisions





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[[TRW Inc.|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 inadvertent construction of a radioisotope rocket is one of the suggested solutions to the [[Pioneer anomaly]]. The Pioneer space probes are powered by [[radioisotope thermal generator]]sgenerators located on the end of a long arm to keep their radiation away from the spacecraft electronics. In this position the back of the main radio dish is preferentially exposed, meaning that radiation (primarily infra-red) scattered by the dish would tend to be scattered to the rear of the spacecraft. This could lead to a ''tiny'' amount of net thrust being generated, although all calculations to date suggest it is not enough in itself to fully explain the effect.{{Citation needed|date=November 2008}}
 
A similar phenomenon occurred on the [[New Horizons]] spacecraft; photons (thermal infrared) from the RTG, reflected from the spacecraft's antenna, produced a very small thrust which propelled the spacecraft slightly off course.<ref>[http://pluto.jhuapl.edu/overview/piPerspective.php?page=piPerspective_05_21_2010 New Horizons official website article mentioning the thrust from the RTG]</ref>

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