Momentum sensor - Electrostatic ballistic pendulum laboratory calibration unit Final report
Electrostatic ballistic pendulum momentum transducer for measuring particle impact
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Electrostatic ballistic pendulum momentum transducer for measuring particle impact
Electrostatic zero-gravity work bench prototype for spacecraft use
Acceleration of charged particles in strong DC magnetic field by electrostatic waves with spatially varying phase velocities integrated numerically on IBM 360/65
Integrated charged particle energy spectra from gridded electrostatic analyzers, relating retarding potential curve to particle floating potential, kinetic temperature, etc
Electrostatic electron bombardment ion thrustor with magnetoelectrostatically contained plasma
Electrostatic rocket exhaust condensation on spacecraft solar electric panels cover glasses, noting deleterious effects
Electrostatic charge distribution on ultrahigh vacuum cleaved silicates including instrumentation, UV irradiation, half life, Paschen relation, etc
Electrostatic heating of solar wind ions from instability in two fluid solar wind model leading to preferential heating of protons over electrons
Positive ion concentration in D region, using spherical stationary electrostatic probe in weakly ionized collision dominated gas
Ion collecting cylindrical electrostatic probes as flow field tracing instruments in low density slightly ionized flows
Cylindrical electrostatic probes on Alouette 2 and Explorer 31 satellites used in intersatellite comparison of directly measured ionospheric electron temperature and density
Cylindrical electrostatic probe measurements on Alouette 2 and Explorer 31, considering implications for future missions
Ionospheric VLF electrostatic noise observed by sounding rocket, noting proton gyrofrequency harmonics effects within emission attenuation bands
Existence criteria for normal modes in magnetized plasma related to electrostatic approximation
Electrostatic acceleration system for hypervelocity microparticles with selected kinematic properties
Nuclear electric generator for accelerating charged propellant particles in electrostatic propulsion system
Calculating drift of electrostatic gyroscopes due to rotor asphericity
Electrostatic propulsion beam divergence effects on spacecraft surfaces - Vol. 1