Thrust of a pulsed plasma jet measured from deviations of a ballistic pendulum

Abstract We measured the peak force of the plasma jet produced by a pulsed coaxial plasma gun operated at voltages up to 2 kV, using a home-made ballistic pendulum positioned in two locations, one in the proximity of the gun nozzle at 0.75 cm and the second at a distance of 9 cm from the gun nozzle. The force of the plasma wind is inferred and ranges from 11 to 60 N, which is almost an order of magnitude higher than that of typical ion-based thrusters. The results of various models of self-field magneto-plasmadynamic thrusters indicate that the magnetic component thrust tends to dominate over the thermal expansion, particularly at higher discharge voltages of 1.5 kV and 2 kV. The highest thrust of 60 N is obtained for a 2 kV discharging voltage. The plasma was ignited in CO 2 at pressures between 1 and 5 Torr. The displacement of the pendulum pushed by the plasma wind force was measured using a high-speed camera.

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Publication Details

Journal
Physica Scripta
Published
2024-08-05
DOI
https://doi.org/10.1088/1402-4896/ad6b4d
Citations
5
Primary Topic
Plasma Diagnostics and Applications
Type
article
Field-Weighted Citation Impact
1.04
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article

Thrust of a pulsed plasma jet measured from deviations of a ballistic pendulum

A. Scurtu, Maria Luiza Mitu, Nicoleta Udrea, Dorina Ticoş et al.
5 citations
Physica Scripta
Plasma Diagnostics and Applications
1.04
article

Thrust of a pulsed plasma jet measured from deviations of a ballistic pendulum

A. Scurtu, Maria Luiza Mitu, Nicoleta Udrea, Dorina Ticoş, C. M. Ticoş
article en
5 citations

Abstract

Abstract We measured the peak force of the plasma jet produced by a pulsed coaxial plasma gun operated at voltages up to 2 kV, using a home-made ballistic pendulum positioned in two locations, one in the proximity of the gun nozzle at 0.75 cm and the second at a distance of 9 cm from the gun nozzle. The force of the plasma wind is inferred and ranges from 11 to 60 N, which is almost an order of magnitude higher than that of typical ion-based thrusters. The results of various models of self-field magneto-plasmadynamic thrusters indicate that the magnetic component thrust tends to dominate over the thermal expansion, particularly at higher discharge voltages of 1.5 kV and 2 kV. The highest thrust of 60 N is obtained for a 2 kV discharging voltage. The plasma was ignited in CO 2 at pressures between 1 and 5 Torr. The displacement of the pendulum pushed by the plasma wind force was measured using a high-speed camera.

Physica ScriptaVol. 99(9)
Horia Hulubei National Institute for R and D in Physics and Nuclear Engineering (RO), National Institute for Laser Plasma and Radiation Physics (RO)
Affordable and clean energy
Openalex Percentile: Top 23%
Plasma Diagnostics and Applications
1.04
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Thrust of a pulsed plasma jet measured from deviations of a ballistic pendulum — A. Scurtu, Maria Luiza Mitu, et al. · Physica Scripta (2024) | TGRS Research Map | TGRS