Non Invasive Measurement on the Pulsed and Steady-State , High Power MadHeX Helicon Plasma Thruster IEPC-2009-206
Non Invasive Measurement on the Pulsed and Steady-State , High Power MadHeX Helicon Plasma Thruster IEPC-2009-206
复制标题
对脉冲和稳态高功率 MadHeX Helicon 等离子推进器的非侵入式测量 IEPC-2009-206
DOI:
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发表时间:
2009
期刊:
影响因子:
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通讯作者:
J. Scharer
中科院分区:
文献类型:
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作者:
M. Wiebold;J. Scharer
Non-invasive measurements are performed on a pulsed and steady-state argon helicon plasma thruster with a static axial magnetic nozzle field (1 kG source, 1.5 kG nozzle peak). Flow rates are between 1 and 76 sccm with coupled 13.56 MHz rf power levels of between 700 W and 10 kW. Collisional-radiative (CR) models for Ar II and Ar I are used to spectroscopically determine the electron temperature (Te) and the neutral density, respectively. The electron density (nemax= 8 x 10 13 /cm −3 ) is measured via 105 GHz microwave interferometry and is an input to the CR models. In collisionless, highly neutraldepleted regions, Te rises linearly with power while ne remains constrained. Regions of pressure balance and pressure gradients are present, and evidence of substantial axially accelerated ion flows is observed. Regimes where cooler (5 eV) and hotter (>20 eV) electron temperatures are observed for lower and higher flow rates. The axial ion energy distribution function and its acceleration is measured in these different regimes from the source region through the nozzle using tunable diode laser-induced fluorescence.