Beam Neutralization Test of a Flight Model Electron Bombardment Engine
Beam neutralization tests of electron bombardment engine model in simulated space environment
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Beam neutralization tests of electron bombardment engine model in simulated space environment
Electron bombardment ion engine - beam current limited by either arc or electrodes
Plasma theory of lewis type bombardment ion engine
Langmuir probe data of current-voltage characteristics inside kaufman-type ion engine - plasma discharge
Thermionic electron emission currents from cesium coated tungsten accelerator electrodes in ion thrusters
Neutralization of ion beams from engines of annular geometry
Beam neutralization tests of a flight model electron bombardment engine
Ac power supply for use in an electron-bombardment ion rocket engine
Performance and design of the lewis-type electron bombardment ion engine
Performance of a high current density cylindrical concave porous tungsten emitter for cesium propellant ion thrustors
Model for determining regions of weak and strong plasmas, and calculation of radial variation of plasma density and potential
Method of electrostatic ion gun design with central trajectory beam requirements, and an extension of this method to thick beams
Properties of the plasma inside an operating kaufman-type electron bombardment engine, with langmuir probes
Breakdown and arcing phenomena in an electron- bombardment ion thrustor
Utilization of a permanent magnet circuit in an electron-bombardment ion rocket
Evaluation of a cesium-ion rocket engine employing a large porous tungsten ionizer
Optimization of ion engine control systems for synchronous satellites
Experimental investigation of the properties of the plasma inside an operating kaufman-type electron bombardment engine, with langmuir probes