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Plasma Flow During RF Discharges in VASIMRThe Variable Specific Impulse Magnetoplasma Rocket (VASIMR) plasma source consists of a helical antenna, driven at frequencies of 4 to 19 MHz with powers up to 1 kW, in a magnetic field up to 3 kG. Helium is the current test gas, and future experiments with hydrogen are planned. Plasma density and temperature profiles were measured by a reciprocating Langmuir probe, and plasma flow profiles were measured with a reciprocating Mach probe. Both probes were located about 0.5 m downstream from the helical antenna. The plasma source operated in capacitive and inductive modes in addition to a helicon mode. During capacitive and inductive modes, densities were low and plasma flow was < 0.5 Cs. When the plasma operated in a helicon mode, the densities measured downstream from the source were higher [10(exp 12) / cubic cm ] and plasma flow along the magnetic field was of the order Mach 1. Details of the measurements will be shown.
Document ID
20000092093
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Jacobson, V. T.
(NASA Johnson Space Center Houston, TX United States)
Chang Diaz, F. R.
(NASA Johnson Space Center Houston, TX United States)
Squire, J. P.
(NASA Johnson Space Center Houston, TX United States)
Ilin, A. V.
(NASA Johnson Space Center Houston, TX United States)
Bengtson, R. D.
(Texas Univ. Austin, TX United States)
Carter, M. D.
(Oak Ridge National Lab. TN United States)
Goulding, R. H.
(Oak Ridge National Lab. TN United States)
Date Acquired
August 19, 2013
Publication Date
January 1, 1999
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: Plasma Propulsion Physics Mini Conference
Location: Seattle, WA
Country: United States
Start Date: November 15, 1999
End Date: November 19, 1999
Sponsors: American Physical Society
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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