Single- and Repetitive-Pulse Conical Theta-Pinch Inductive Pulsed Plasma Thruster Performance

被引:11
作者
Hallock, Ashley K. [1 ]
Martin, Adam K. [2 ]
Polzin, Kurt A. [2 ]
Kimberlin, Adam C. [2 ]
Eskridge, Richard H. [2 ]
机构
[1] Yetispace Inc, Huntsville, AL 35811 USA
[2] NASA, George C Marshall Space Flight Ctr, Huntsville, AL 35812 USA
关键词
Accelerators; inductive accelerators; modeling; plasma engines; ACCELERATION;
D O I
10.1109/TPS.2014.2368835
中图分类号
O35 [流体力学]; O53 [等离子体物理学];
学科分类号
070204 ; 080103 ; 080704 ;
摘要
Impulse bits produced by conical theta-pinch inductive pulsed plasma thrusters possessing cone angles of 20 degrees, 38 degrees, and 60 degrees, were quantified for 500-J/pulse operation by direct measurement using a hanging pendulum thrust stand. All three cone angles were tested in single-pulse mode, with the 38 degrees model producing the highest impulse bits at roughly 1-mN-s operating on both argon and xenon propellants. A capacitor charging system, assembled to support repetitively pulsed thruster operation, permitted testing of the 38 degrees thruster at a repetition rate of 5 Hz at power levels of 0.9, 1.6, and 2.5 kW. For similar conditions, the average thrust measured during repetitive-pulse operation exceeded the value obtained when the single-pulse impulse bit is multiplied by the repetition rate, suggesting that a greater impulse bit per pulse was produced when operating in the repetitive-pulse mode.
引用
收藏
页码:433 / 443
页数:11
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