DocumentCode
916888
Title
Rockets for the Red Planet
Author
Upson, Sandra
Volume
46
Issue
6
fYear
2009
fDate
6/1/2009 12:00:00 AM
Firstpage
42
Lastpage
47
Abstract
The paper describes VASIMR (variable specific impulse magnetoplasma rocket), nuclear-electric rocket engine - a fission reactor with a plasma thruster that could potentially push people to Mars and back using a fraction of the propellant and time needed for a chemical rocket.
Keywords
Mars; aerospace propulsion; fission reactors; rocket engines; space vehicles; Mars; fission reactor; nuclear-electric rocket engine; plasma propulsion rocket; plasma thruster; variable specific impulse magnetoplasma rocket; Chemicals; Earth; Engines; Magnetosphere; Mars; Moon; Planets; Plasma chemistry; Rockets; Testing;
fLanguage
English
Journal_Title
Spectrum, IEEE
Publisher
ieee
ISSN
0018-9235
Type
jour
DOI
10.1109/MSPEC.2009.4977611
Filename
4977611
Link To Document