8th Electric Propulsion Conference 1970
DOI: 10.2514/6.1970-1112
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Experimental study of colloid annular thrusters

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“…The specific charge of the emitted species is defined as (7) where is the particle charge, its mass, and is the propellant density. In a colloid thruster, it is desired to increase as much as possible the specific charge because this implies larger specific impulse values for a fixed potential drop (8) Therefore, the engine should use as little flowrate as possible, down to , the minimum flowrate at which steady-sate operation can be sustained [4] (9)…”
Section: Introductionmentioning
confidence: 99%
“…The specific charge of the emitted species is defined as (7) where is the particle charge, its mass, and is the propellant density. In a colloid thruster, it is desired to increase as much as possible the specific charge because this implies larger specific impulse values for a fixed potential drop (8) Therefore, the engine should use as little flowrate as possible, down to , the minimum flowrate at which steady-sate operation can be sustained [4] (9)…”
Section: Introductionmentioning
confidence: 99%