Time-resolved investigation of the asymmetric plasma plume in a pulsed plasma thruster

Abstract

Electric propulsion (EP) has become one of the most promising options for the motion control of small satellites. The physics behind the ejected plasma plumes of EP thrusters has attracted significant interest due to their interactions with the critical components of satellites. Axisymmetric plume assumptions are widely used in simulations and plume diagnostics. However, we show here that the plasma plume of a parallel-plate pulsed plasma thruster (PPT) is asymmetrically distributed along the centerline of the electrodes, contrary to the inherent axisymmetric assumption. To study this asymmetric plume structure in depth, a triple Langmuir probe was used to obtain the electron density of a two-dimensional plume area over the operating period of a PPT. The electron density results show that the plasma forms an 'I' shape plume at 2 µs after the initial main discharge. However, over time, the plume appears to cant significantly towards the cathode. The physical mechanism behind the asymmetric plume structure is studied through inter-electrode magnetic probe measurements and plasma trajectory analyses. The successive magnetic profiles indicate that the plasma is accelerated by a non-symmetrical electromagnetic force between the electrodes, which results in the plasma exhausting out with an entirely asymmetric distribution shifted upwards towards the cathode. This was also verified using varying sets of discharge voltage experiments. This work also indicates that care must be taken in the selection of the measurement points in PPT plume diagnostics. The measurement points should be chosen above the centerline of the PPT exit as the plasma parameters along the centerline may not be the most energetic part as previously believed. Furthermore, the asymmetric acceleration component of the electromagnetic force between the electrodes can enlighten us in the design of electromagnetic field configurations for future discharge channel optimization.

Transient buildup and dissipation of a compressed plasma shockwave in arc-discharge plasma beams

“…In this work, we used a cylindrical-type triple Langmuir probe developed in-house [34]. A photo of the triple Langmuir probe can be found in the supplementary material.…”

The ablation characteristics of laser-assisted pulsed plasma thruster with metal propellant

“…However, PPTs still have the disadvantage of 'late-time ablation', in which the propellant surface proceeds to be ablated after the thruster completes the entire working period. Because of late-time ablation, some particles on the propellant surface are not accelerated by the thruster, resulting in low propellant utilisation efficiency and low thruster efficiency [7][8][9]. In addition, PPTs have the difficulties of carbon deposition in spark plugs and plume pollution.…”