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

被引:0
|
作者
Scurtu, A. [1 ]
Ticos, D. [1 ]
Udrea, N. [1 ]
Mitu, M. L. [1 ]
Ticos, C. M. [1 ,2 ]
机构
[1] Natl Inst Laser Plasma & Radiat Phys, Bucharest 077125, Romania
[2] Horia Hulubei Natl Inst R&D Phys & Nucl Engn IFIN, Magurele, Romania
关键词
plasma gun; ballistic pendulum; plasma propulsion; magnetoplasmadynamic thruster; DUST PARTICLES; PERFORMANCE; PROPULSION; PARAMETERS; TRIPLE;
D O I
10.1088/1402-4896/ad6b4d
中图分类号
O4 [物理学];
学科分类号
0702 ;
摘要
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 CO2 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.
引用
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页数:16
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