DocumentCode :
3711230
Title :
Solar electric propulsion for future NASA missions
Author :
Geoffrey A. Landis;Steven R. Oleson;Carolyn R. Mercer
Author_Institution :
NASA Glenn Research Center, 21000 Brookpark Road, Cleveland OH 44135, United States of America
fYear :
2015
fDate :
6/1/2015 12:00:00 AM
Firstpage :
1
Lastpage :
4
Abstract :
Use of high-power solar arrays, at power levels up to a megawatt, have been proposed for a solar-electric propulsion (SEP) missions, using photovoltaic arrays to provide energy to high-power xenon-fueled engines. One of the proposed demonstrations of high-power SEP technology is a mission to rendezvous with an asteroid and move it into lunar orbit for human exploration, the Asteroid Redirect mission. NASA´s Solar Electric Propulsion project is dedicated to developing critical technologies to enable trips destinations such as Mars or asteroids. NASA needs to reduce the cost of these ambitious exploration missions. High power and high efficiency SEP systems will require much less propellant to meet those requirements.
Keywords :
"Propulsion","Space vehicles","Mars","NASA","Moon","Orbits"
Publisher :
ieee
Conference_Titel :
Photovoltaic Specialist Conference (PVSC), 2015 IEEE 42nd
Type :
conf
DOI :
10.1109/PVSC.2015.7355948
Filename :
7355948
Link To Document :
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