A 30-cm-diameter, low specific impulse, hollow cathode mercury thruster
Low specific impulse hollow cathode mercury thrustor for deep space electric propulsion, using SERT 2 configuration
Engineering topics
Publications and source records attributed to Poeschel, R. L..
Low specific impulse hollow cathode mercury thrustor for deep space electric propulsion, using SERT 2 configuration
Kaufman thrustor with predominant radial field, noting electron mobility across ion extraction screen and advantages of uniform plasma distribution
Development and testing of low specific impulse ion thruster
Kaufman thrustor performance dependence on transmission of ion extraction optics and magnetic field shape
Kaufman thrustor with predominant radial field, noting electron mobility across ion extraction screen and advantages of uniform plasma distribution
Kaufman thrustor performance dependence on transmission of ion extraction optics and magnetic field shape
Hot cathode reflex discharges investigated to improve ion generation efficiency in space ion thrustors
Discharge chamber performance optimization for mercury bombardment ion thrusters