The Effect of Ignition Techniques on a Capillary Discharge Based Pulsed Plasma Thruster

In order to better understand the operating characteristics of a capillary discharge based electrothermal pulsed plasma source, a variety of ignition techniques were investigated to determine performance effects and viability in a real system. Discharge current profiles along with thrust and specifi...

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Hauptverfasser:	Pancotti, A P, Gilpin, M R, Young, M
Format:	Report
Sprache:	eng
Schlagworte:	CAPILLARY DISCHARGE ELECTRODES EXPLODING WIRES GAS BREAKDOWN IGNITION SYSTEMS Jet and Gas Turbine Engines MATERIALS NOZZLE EXPANSION OPTIMIZATION Physical Chemistry RELIABILITY SPACE TECHNOLOGY SPECIFIC IMPULSE SURFACE FLASHOVER SYMPOSIA TEST AND EVALUATION THRUSTERS VIABILITY WUAFRL50260542
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