Control analysis of an ion thruster with programmed thrust.
Digital computer simulation and analysis of control loops for ion thrustor control
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Digital computer simulation and analysis of control loops for ion thrustor control
Liquid mercury cathode thrustors characteristics satisfying constraints imposed by solar flux variations with distance from sun
Electrothermal instabilities for explanation of MPD arc thrustor rotating spoke phenomenon, noting agreement with experimental results
SERT 2 thrustor system performance over expected mission parameters, noting operational lifetime excess over mission requirements
Research and development program in annular slit colloid thrustor technology, proving thrustor feasibility by performance tests
Ion accelerators design for Kaufman thrustors in terms of beam optics and grid lifetime, using digital computer and electrolytic tank analog
Electrostatic electron bombardment ion thrustor with magnetoelectrostatically contained plasma
Performance analysis for electrothermal thrustor using lithium propellant with supersonic heat addition
Liquid mercury cathode electron bombardment thrustors applicability to electric propulsion missions
Kaufman thrustor with predominant radial field, noting electron mobility across ion extraction screen and advantages of uniform plasma distribution
Kaufman thrustor performance dependence on transmission of ion extraction optics and magnetic field shape
Causes and magnitudes of thrust misalignment of Kaufman type electron bombardment ion thrustor
Axial velocities in ammonia MPD thrustor exhaust by measuring Doppler shifts of spectral lines emitted by plasma constituents
Discharge chamber plasma processes in electron bombardment ion thrustors, considering factors affecting thrustor performance
Valving concepts and functional approaches for inert gas attitude control thrustor systems providing redundancy safeguards at minimum weight, volume and power costs
ATS 3 spacecraft ammonia-fueled resistojet engine test performance
Theoretical performance analyses for electrothermal thrustor using lithium propellant with combination of radioisotope and electrical energy sources
Experimental design of 20-cm mercury electron bombardment thrustor