Abstract
The use of shielded electrostatic probe to measure spatial plasma parameters of the quasineutral plasma in Hall thrusters was studied. The probe-induced perturbations could produce changes in the plasma parameters and discharge current on the order of their steady-state values, in Hall thrusters. The perturbations were explored by varying the material, residence time and penetration distance of various probe designs. In a set of experiments with a segmented shield probe, the thruster was operated in the discharge voltages of 200-500 V and input power range of 500 W-2.5 kW, while the probe-induced perturbations of the discharge current were below 4% of its steady-state value.
| Original language | English (US) |
|---|---|
| Pages (from-to) | 393-399 |
| Number of pages | 7 |
| Journal | Review of Scientific Instruments |
| Volume | 75 |
| Issue number | 2 |
| DOIs | |
| State | Published - Feb 2004 |
All Science Journal Classification (ASJC) codes
- Instrumentation