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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).
 
==Photon Pressurepressure==
{{see also|nuclearNuclear photonic rocket}}
Even without an exhaust, the [[Radiation pressure|photon pressure]] of the energy emitted by a thermal source can produce thrust, although an extremely tiny amount. A famous example of spacecraft thrust due to photon pressure was the [[Pioneer anomaly]], in which photons from the onboard radioisotope source caused a tiny but measurable acceleration of the Pioneer spacecraft.
 

Retrieved from "https://en.wikipedia.org/wiki/Radioisotope_rocket"
 




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