Electric propulsion.
Electrothermal, electrostatic and electromagnetic thrustor for spacecraft propulsion
Engineering topics
Publications and source records attributed to Mickelsen, W. R..
Electrothermal, electrostatic and electromagnetic thrustor for spacecraft propulsion
Radioisotopes for heating ionizers in contact ionization thrustors
Performance characteristics and power requirements of large modules and arrays of electrostatic thrustor
Electromagnetic, electrothermal, and electrostatic thrustors for propulsion systems
Radioisotope electrostatic propulsion system feasibility and its potential for future space missions without undue radiation hazards
Operation and design of a cerium-144 radioisotope electrostatic space propulsion system considering radiation hazards and radioisotope availability
Problems associated with a cerium-144 radioisotope electrostatic propulsion system, such as radiation hazards, fuel availability, and spacecraft design
Nasa research report on heavy-particle electrostatic spacecraft thrustors using colloidal particles
Heavy-particle electrostatic thrustors - nasa program
Radioisotopes for electrostatic propulsion of small space vehicles
Electrostatic propulsion system with direct nuclear electrogenerator
High-vacuum condenser tank for testing ion rocket engines
Turbulent diffusion and anemometer measurements
Electrostatic propulsion system with direct nuclear electrogenerator
Electrostatic propulsion system with a direct nuclear electrogenerator
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Explore the source record for details and available documents.
Explore the source record for details and available documents.