Discharge Chamber Optimization of the SERT II Thrustor
Optimum discharge chamber configuration of permanent magnet mercury-bombardment thrustor for SERT II mission
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Optimum discharge chamber configuration of permanent magnet mercury-bombardment thrustor for SERT II mission
Conventional and composite grid designs tested with low voltage Kaufman thrustor
Space electric rocket test /SERT/ II thrustor system, discussing flight worthiness and mercury bombardment discharges
Kaufman thrustor with curved stainless steel accelerating-grid system, studying operation, efficiency, plasma instability, etc
Radioisotope heating for ionizer temperature of contact ionization thrustors for satellite attitude control and stationkeeping, studying power source mass saving
Nasa research report on heavy-particle electrostatic spacecraft thrustors using colloidal particles
Performance of a high current density cylindrical concave porous tungsten emitter for cesium propellant ion thrustors
Measurements of the thrust of a colloidal-particle electrostatic engine and their correlation to thrustor operation
Breakdown and arcing phenomena in an electron- bombardment ion thrustor
Electric breakdown and arcing in ion thrustors for power supplies
Spacecraft designed to provide flight test measurement of ion thrustor electrical parameters and thrust
Electrolytic tank analog for two-dimensional analysis of electrostatic thrustor ion optics
Energy storage film capacitors for pulsed plasma thrustors developed for coaxial plasma gun and Pulsed Arc Gun
Electron cyclotron resonance plasma accelerator design for thrustor application and measuring techniques
High-frequency dc-dc converter for ion thrustors using modular design and inductive energy pumping technique for conversion, regulation, and protection
Cesium surface contact ionization electrostatic thrustors
Electron-ion emitting characteristics of various electrode materials with cesiated surfaces for cesium contact ion thrustors
Ion thrustor, including mercury feed system and shielded neutralizer, designed and tested for spacecraft station keeping and attitude control