The plasma-induced magnetic field in an electron cyclotron resonance plasma thruster is measured non-intrusively by means of a diamagnetic loop that encloses the plasma flow. The calibration process is described, and parasitic currents in the thruster walls and plasma oscillations are identified as the dominant sources of uncertainty. The integrated magnetic flux is seen to depend on the applied power and less significantly on the mass flow rate. The effect of the diamagnetic loop radius is also studied by testing two loops of different diameters. To estimate the perpendicular electron pressure in the plasma from the loop measurements, two plasma beam models, 1D and 2D, are used. While both models give similar results for the small loop, th...
It is shown analytically that the thrust from a simple plasma thruster (in the absence of a magnetic...
Magnetic field measurements were made in the discharge channel of the 5 kW-class P5 laboratory-model...
This thesis is concerned with characterising the plume expansion in the magnetic nozzle of a helicon...
The plasma-induced magnetic field in an electron cyclotron resonance plasma thruster is measured non...
Proceeding of: 35th International Electric Propulsion Conference (IEPC), October 8-12 2017, Atlanta,...
Experimental characterization of plasma properties along the magnetic nozzle of an electron cyclotro...
A circular waveguide electron cyclotron resonance plasma thruster prototype driven by microwaves at ...
International audienceA quasi-linear heating model for an electron cyclotron resonance acceleration ...
International audienceA coaxial ECR thruster is simulated using a 1D3V electromagnetic Particle-In-C...
A previous axisymmetric model of the supersonic expansion of a collisionless, hot plasma in a diverg...
Experimental results are presented from the plume of a high powered (200 kW) DC plasma gun emitting ...
Thesis (Ph.D.)--University of Washington, 2013The high power helicon (HPH) is a compact plasma sourc...
Diamagnetic measurements of poloidal beta have been performed in the STOR-M tokamak by a flux loop p...
An electron-cyclotron resonance thruster (ECRT) prototype is simulated numerically, using two couple...
Proceeding of: Space Propulsion Conference, SP 2018,14-18 mayo, SevillaThis paper presents experimen...
It is shown analytically that the thrust from a simple plasma thruster (in the absence of a magnetic...
Magnetic field measurements were made in the discharge channel of the 5 kW-class P5 laboratory-model...
This thesis is concerned with characterising the plume expansion in the magnetic nozzle of a helicon...
The plasma-induced magnetic field in an electron cyclotron resonance plasma thruster is measured non...
Proceeding of: 35th International Electric Propulsion Conference (IEPC), October 8-12 2017, Atlanta,...
Experimental characterization of plasma properties along the magnetic nozzle of an electron cyclotro...
A circular waveguide electron cyclotron resonance plasma thruster prototype driven by microwaves at ...
International audienceA quasi-linear heating model for an electron cyclotron resonance acceleration ...
International audienceA coaxial ECR thruster is simulated using a 1D3V electromagnetic Particle-In-C...
A previous axisymmetric model of the supersonic expansion of a collisionless, hot plasma in a diverg...
Experimental results are presented from the plume of a high powered (200 kW) DC plasma gun emitting ...
Thesis (Ph.D.)--University of Washington, 2013The high power helicon (HPH) is a compact plasma sourc...
Diamagnetic measurements of poloidal beta have been performed in the STOR-M tokamak by a flux loop p...
An electron-cyclotron resonance thruster (ECRT) prototype is simulated numerically, using two couple...
Proceeding of: Space Propulsion Conference, SP 2018,14-18 mayo, SevillaThis paper presents experimen...
It is shown analytically that the thrust from a simple plasma thruster (in the absence of a magnetic...
Magnetic field measurements were made in the discharge channel of the 5 kW-class P5 laboratory-model...
This thesis is concerned with characterising the plume expansion in the magnetic nozzle of a helicon...