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Radioisotope Electric Propulsion for Fast Outer Planetary Orbiters
Author(s) -
Steven R. Oleson,
Scott Benson
Publication year - 2002
Publication title -
nasa technical reports server (nasa)
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2002-3967
Subject(s) - propulsion , electrically powered spacecraft propulsion , aerospace engineering , astrobiology , computer science , environmental science , physics , engineering
Recent interest in outer planetary targets by the Office of Space Science has spurred the search for technology options to enable relatively quick missions to outer planetary targets. Several options are being explored including solar electric propelled stages combined with aerocapture at the target and nuclear electric propulsion. Another option uses radioisotope powered electric thrusters to reach the outer planets. Past work looked at using this technology to provide faster flybys. A better use for this technology is for outer planet orbiters. Combined with medium class launch vehicles and a new direct trajectory these small, sub-kilowatt ion thrusters and Stirling radioisotope generators were found to allow missions as fast as 5 to 12 years for objects from Saturn to Pluto, respectively. Key to the development is light spacecraft and science payload technologies.

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