Fundamental plasma processes in electron bombardment thrustor ionization chambers
Fundamental plasma processes in electron bombardment thrustor ionization chambers
THRUSTOR↗
Engineering topics
Mickelsen, W. R.
Publications and source records attributed to Mickelsen, W. R..
Approximate methods in electric propulsion mission analysis
Approximate methods in electric propulsion missions such as lunar orbiter lander
ELECTRIC PROPULSION↗
A direct-conversion device using thermally- accelerated, charged colloidal particles
Direct conversion device using thermally accelerated, charged colloidal particles
COLLOID↗
Advanced concepts in electric propulsion.
Primary electric propulsion application to satellite and other space missions, considering auxiliary systems and experimental thrustor systems
AUXILIARY POWER SOURCE↗
Advanced electric propulsion research Annual report, 1 Jan. - 31 Dec. 1966
Advanced electric propulsion research, thermal power augmentation, thrustor operation, and colloidal propellant production
THRUSTOR↗
Electric propulsion for payload transport from moon to earth
Electric propulsion and payload mass ratio for moon-earth payload transport
ELECTRIC PROPULSION↗
Radioisotope heating of contact ionizers
Radioisotope heating of ionizers in contact ionization thrustor in primary electric propulsion systems
RADIOACTIVE ISOTOPE↗
Propellant from spent tankage
Mission performance gains from using spent booster tankage as propellant source for electric propulsion spacecraft
SPACECRAFT PROPULSION↗
Thermal power augmentation in electric propulsion systems
Electric propulsion system performance gains using thermal power augmentation
PROPULSION SYSTEM PERFORMANCE↗
Applications of the ATEP concept
Electrostatic, electrothermal thrustors in electric propulsion system augmented with thermal power
ELECTRIC PROPULSION↗
Aluminum colloid formation by homogeneous nucleation
Aluminum colloid formation by homogenous nucleation for electrostatic thrustor propellant
NUCLEATION↗
Aluminum-oxide colloid formation by vapor- phase chemical reaction
Adiabat flame temperature calculation for aluminum oxide colloid formation by vapor phase chemical reaction, for electric thrustor propellant
ELECTRIC PROPULSION↗
Electric propulsion for satellites
Electrostatic, resistojet, colloidal, and plasma propulsion for satellite thrust and control
Mickelsen, W. R.↗
Colloid-particle electrostatic thrustors.
Colloid particle electrostatic thrustors for lunar ferry missions in specific impulse range 1000-3000 sec
COLLOIDAL PROPELLANT↗
Colloid-particle electrostatic thrustors
Specific impulse requirements for electric rocket lunar ferries
SPECIFIC IMPULSE↗
Lunar-supply mission study
Profiles for lunar supply missions involving electric propulsion
LUNAR FLIGHT↗
Propellant from spent tankage
Feasibility of using aluminum spent tankage as source of propellant for electric spacecraft
PROPELLANT TANK↗
Electrostatic propulsion system with a direct nuclear electrogenerator Patent
Nuclear electric generator for accelerating charged propellant particles in electrostatic propulsion system
Low, C. A., Jr.↗