State-of-the-art of electric propulsion - 1965.
Electric propulsion systems discussing thrustors, propellant tankage and feed systems, power conditioning and controls
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Electric propulsion systems discussing thrustors, propellant tankage and feed systems, power conditioning and controls
Solid propellant rocket engine environmental and static testing for use as retrograde thrustor in Atlas-Centaur space vehicle
Preparation of colloid particles for electrostatic thrustors by reaction of vapors
Improvements in electric subsystem and capacity of thrust stand system for testing chemical, subliming, and cold gas thrustors
Electric propulsion in 1965, discussing electron bombardment and contact ionization thrustors, nuclear and solar-electric power systems, etc
Electric propulsion including thrustors, power systems, solar power, hybrids, etc
Ionization characteristics of various porous metal ionizers and suitability for use in cesium contact thrustors
Electron bombardment thrustors using liquid mercury cathodes, noting lifetime, propellant and power efficiency, feed system, temperature limits, etc
Design of gravity-independent force-fed liquid-metal cathode providing unlimited cathode life in gas discharge devices and mercury electron-bombardment thrustors
Electron cyclotron resonance plasma accelerator design for thrustor application and measuring techniques
Energy storage film capacitors for pulsed plasma thrustors developed for coaxial plasma gun and pulsed arc gun
Design, fabrication, and life test of ion engine system using oxide cathode mercury electron bombardment thrustor
Adiabat flame temperature calculation for aluminum oxide colloid formation by vapor phase chemical reaction, for electric thrustor propellant
POODLE low thrust radioactive propulsion technology, discussing operation, mission application, tests, capsule and thrustor performance
Ion extractor system for electrostatic thrustors designed, using salient features of digital computer and electrolytic tank analog methods
Ion thrustor, including mercury feed system and shielded neutralizer, designed and tested for spacecraft station keeping and attitude control
Electron bombardment ion thrustors with two accelerator-grid systems for producing ion beams in directions 180 or 90 degrees apart
Electron bombardment thrustors using liquid mercury cathodes noting lifetime, propellant and power efficiency, feed system, temperature limits, etc