DocumentCode
1597641
Title
Ambipolar ion acceleration in a 20,000 G magnetic nozzle
Author
Longmier, Benjamin W. ; Sheehan, J.P. ; Bering, Edgar A. ; Squire, Jared P. ; Olsen, Christopher S. ; Carter, Mark D. ; Glover, Timothy W. ; Chang-Diaz, F.R.
Author_Institution
Univ. of Michigan, Ann Arbor, MI, USA
fYear
2013
Firstpage
1
Lastpage
1
Abstract
Summary form only given. An observed 50 eV argon ion energy is attributed to a measured axial plasma potential profile within the expanding magnetic nozzle region of a 35 kW helicon plasma source. The ion acceleration mechanism is identified as an ambipolar flow caused by expanding plasma that follows the fluid equations using the adiabatic definition of pressure, resulting in a maximum ion energy of several kTe. The helicon plasma source was operated with 50 to 150 mg/s argon propellant, and had a max and min magnetic field strength of 20,000 G. and 2 G respectively. The size scale and spatial location of the plasma potential structure of the expanding magnetic nozzle region appears to follow the size scale and spatial location of the expanding magnetic field along a 450 cm long section of the magnetic nozzle. The thickness of the potential structure was found to be 1e5 Debye lengths, many orders of magnitude larger than typical double layer structures. The background plasma density and neutral argon pressure were 1e9 cm-3 and 1e-5 Torr respectively. A large parameter scan of electron temperature and resulting ambipolar ion acceleration energies is presented.
Keywords
argon; ion accelerators; nozzles; plasma accelerators; plasma density; plasma sources; plasma temperature; plasma transport processes; Ar; Debye length; adiabatic pressure; ambipolar flow; ambipolar ion acceleration energy; axial plasma potential profile measurement; background plasma density; double layer structure; electron temperature; electron volt energy 50 eV; fluid equation; helicon plasma source; magnetic field expansion; magnetic field strength; magnetic flux density 2 G; magnetic flux density 20000 G; magnetic nozzle region expansion; plasma expansion; plasma potential structure; propellant; size 450 cm; Acceleration; Argon; Educational institutions; Magnetic fields; Plasma sources; Rockets;
fLanguage
English
Publisher
ieee
Conference_Titel
Plasma Science (ICOPS), 2013 Abstracts IEEE International Conference on
Conference_Location
San Francisco, CA
ISSN
0730-9244
Type
conf
DOI
10.1109/PLASMA.2013.6635043
Filename
6635043
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