Research and development in needle and slit colloid thrusters
Electrostatic charge spraying obtained through use of slightly conductive propellants and high voltages
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Electrostatic charge spraying obtained through use of slightly conductive propellants and high voltages
Hollow cathodes in mercury ion thrustors
Electrophoretic glass coating deposition on molybdenum ion accelerator grids
Performance evaluation of MPD arc jets operating in quasi-steady modes
Performance of magnetoplasmadynamic arc thrustor
Comparative in-flight thrust measurements of SERT 2 ion thrustor
Automated parameter search techniques applied to low thrust mission design, stressing trajectories and mission optimization
Performance analysis for electrothermal thrustor using lithium propellant with supersonic heat addition
Optical spectra of discharge chambers of electron bombardment mercury ion thrustors with hollow and oxide cathodes
SERT 2 thrustor system performance over expected mission parameters, noting operational lifetime excess over mission requirements
30 cm diameter mercury bombardment low impulse thrustor development for potential space applications, discussing performance and control
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
Background pressure and magnetic field shape effect on MPD thrustor performance, testing radiation cooled thrustors
Causes and magnitudes of thrust misalignment of Kaufman type electron bombardment ion thrustor
Discharge chamber plasma processes in electron bombardment ion thrustors, considering factors affecting thrustor performance
Liquid mercury /LM/ cathode thrustor characteristics, power conditioning and control requirements
Hollow cathode ion thrustor and lightweight power conditioner of solar-electric propulsion system for unmanned deep space probes