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The Use of RF Waves in Space Propulsion SystemsThis paper will review the ways in which RF and microwave radiation may be used in the design of electric propulsion systems for spacecraft. RF power has been used or proposed in electric propulsion systems to ionize, to heat, and to accelerate the propellant, or to produce plasma used to inflate a magnetic field for solar sail purposes. Direct RF propulsion using radiation pressure or ponderomotive forces is impractical owing to efficiency considerations. Examples of various systems that have been developed or proposed will be reviewed. The Variable Specific Impulse Magnetoplasma Rocket (VASIMR) uses RF for producing, heating and accelerating plasma. Inductive RF and microwave ion thruster schemes use e-m waves to ionize the plasma, which is then accelerated by use of dc grids. The details of the VASIMR, an inductive RF thruster, and a microwave ion thruster are discussed and contrasted with related RF systems.
Document ID
20060023330
Acquisition Source
Johnson Space Center
Document Type
Reprint (Version printed in journal)
Authors
Bering, Edgar A., III
(NASA Johnson Space Center Houston, TX, United States)
Chang-Diaz, Franklin
(NASA Johnson Space Center Houston, TX, United States)
Squire, Jared
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 23, 2013
Publication Date
January 1, 2004
Subject Category
Spacecraft Propulsion And Power
Distribution Limits
Public
Copyright
Other

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