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

机译:单脉冲和重复脉冲锥形Theta-Pinch感应脉冲等离子推进器性能

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Impulse bits produced by conical theta-pinch inductive pulsed plasma thrusters possessing cone angles of 20°, 38°, and 60°, 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° 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° 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.
机译:圆锥角20英寸,38°和60°的锥形theta-pinch感应脉冲等离子推进器产生的脉冲钻头通过悬挂摆推力架直接测量以500-J /脉冲的操作进行了量化。所有三个锥角均在单脉冲模式下进行了测试,其中38°模型在氩气和氙气推进剂上产生的最大脉冲位约为1-mN-s。组装的电容器充电系统可支持脉冲式推进器的重复运行,允许在0.9、1.6和2.5 kW的功率水平下以5 Hz的重复频率测试38°推进器。在类似条件下,重复脉冲操作期间测得的平均推力超过了单脉冲脉冲位乘以重复率所获得的值,这表明在重复脉冲模式下操作时,每个脉冲产生的脉冲位更大。

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