Effects of electron emission on electrostatic probes at arbitrary pressures
Electrostatic probes response due to thermionic electron emission, considering I-V characteristics and space-charge-limited current
SEARCH · Search NASA
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Electrostatic probes response due to thermionic electron emission, considering I-V characteristics and space-charge-limited current
LF electrostatic waves oblique to magnetic field in plasma, evaluating dispersion relation near ion cyclotron frequency
Fast time-resolved spectra of earth bow shock electrostatic turbulence based on broadband analog electric data from OGO-5
HF electrostatic waves generation by electrons in magnetosphere
Normal wave propagation modes existence in magnetized plasma, deriving criteria for electrostatic approximation validity
Electrostatic turbulence in bow shock magnetic structures observed by OGO 5, explaining turbulence as ion acoustic or Buneman mode due to two stream instability
Cs and Hg electrostatic thrustor effluents effects on spacecraft materials, describing chemical, metallurgical and thermophysical experiments
LF electrostatic instability of Van Allen belt in outer trapping zone causing electric field in plasmapause
Electric propulsion plasma thrust beam and ambient space plasma electrostatic equilibration, considering various charged particle parameters involved in bi-plasma system interactions
Multistage depressed electrostatic collector for magnetically focused spaceborne klystrons
High voltage insulators for direct current in acceleration system of electrostatic thrustor
Effects of electrostatic propulsion beam divergence effects on spacecraft surfaces
Electrostatic hazards during launch vehicle flight operations
Flight prototype electrostatic ballistic pendulum momentum transducer
Charged particle analyzer with periodically varying voltage applied across electrostatic deflection members
A high-altitude electrostatic probe experiment is described and data are presented for three RAM C reentries at velocities of approximately 25 OOO feet per second. The electron density profiles inferred from the probe measurements are compared with theoretical calculations, and the probable cause of significant disagreement is briefly discussed. Probe measurements during material-addition sequences for radio-blackout alleviation are presented, and comparisons of probe measurements with other pertinent diagnostic measurements are made.
Long-range electrostatic and electromagnetic interactions between two neutral hydrogenic atoms in ground state
Computational method for determining performance of ten stage electrostatic depressed collector for klystrons