Title :
Single- and Repetitive-Pulse Conical Theta-Pinch Inductive Pulsed Plasma Thruster Performance
Author :
Hallock, Ashley K. ; Martin, Adam K. ; Polzin, Kurt A. ; Kimberlin, Adam C. ; Eskridge, Richard H.
Author_Institution :
Yetispace, Inc., Huntsville, AL, USA
Abstract :
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.
Keywords :
aerospace propulsion; plasma devices; propellants; argon propellants; capacitor charging system; cone angles; conical theta-pinch inductive pulsed plasma thruster; direct measurement; electrodeless space propulsion device; frequency 5 Hz; hanging pendulum thrust stand; power 0.9 kW; power 1.6 kW; power 2.5 kW; repetitive-pulse conical theta-pinch inductive pulsed plasma thruster performance; single-pulse conical theta-pinch inductive pulsed plasma thruster performance; single-pulse impulse bit; xenon propellants; Capacitors; Coils; Force; Plasmas; Propellants; Pulse measurements; Switches; Accelerators; inductive accelerators; modeling; plasma engines; plasma engines.;
Journal_Title :
Plasma Science, IEEE Transactions on
DOI :
10.1109/TPS.2014.2368835