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Title Design of RF Systems for the RTD Mission VASIMR
Creator/Author Baity, F.W. ; Barber, G.C. ; Carter, M.D. ; Chang-Diaz, F.R. ; Goulding, R.H. ; McCaskill, G.E. ; Sparks, D.O. ; Squire, J.P.
Publication Date1999 Apr 12
OSTI IdentifierOSTI ID: 8008; Legacy ID: DE00008008
Report Number(s)ORNL/CP-103576
DOE Contract NumberAC05-96OR22464
Other Number(s)Other: 46 WA A1 80 1; ON: DE00008008
Resource TypeConference
Resource RelationConference: 13th Topical Conference on Applications of Radio Frequency Power to Plasmas, Princeton, NJ, April 12-14, 1999
Research OrgOak Ridge National Laboratory (ORNL), Oak Ridge, TN
Sponsoring OrgUSDOE Office of Science
Subject70 PLASMA PHYSICS AND FUSION; Design; Design; RF Systems; RF Systems; Ion Thrusters; Ion Thrusters; ICR Heating; ICR Heating
Description/AbstractThe first flight test of the variable specific impulse magnetoplasma rocket (VASIMR) is tentatively scheduled for the Radiation and Technology Demonstration (RTD) in 2003. This mission to map the radiation environment out to several earth radii will employ both a Hall thruster and a VASIMR during its six months duration, beginning from low earth orbit. The mission will be powered by a solar array providing 12 kW of direct current electricity at 50 V. The VASIMR utilizes radiofrequency (RF) power both to generate a high-density plasma in a helicon source and to accelerate the plasma ions to high velocity by ion cyclotron resonance heating (ICRH). The VASIMR concept is being developed by the National Aeronautics and Space Administration (NASA) in collaboration with national laboratories and universities. Prototype plasma sources, RF amplifiers, and antennas are being developed in the experimental facilities of the Advanced Space Propulsion Laboratory (ASPL).
PublisherAmerican Inst. of Physics, New York
Country of PublicationUnited States
LanguageEnglish
FormatMedium: ED; Size: 4 pages
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System Entry Date2008 Feb 04
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