Development of a thin-film space-charge- limited triode Final report, Mar. 1965 - Jun. 1966
Development of thin film space charge limited triode
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Development of thin film space charge limited triode
Materials development is crucial for the advancement of electric aviation. Current research focusing on novel multifunctional materials is underway to solve the needs for aerospace systems; however, additional testing of these materials to understand their failure modes is equally critical. This project will utilize pulsed electroacoustic (PEA) instrumentation to investigate space charge accumulation of multifunctional composites and other insulation materials critical to robust high power transmission systems. Evaluating the space charge phenomena in dielectric materials will provide unique and fundamentally necessary data to determine the feasibility and lifetime of any high voltage insulation system. When electrical charge is injected into a solid dielectric, charge can accumulate and become trapped, leading to the failure of the insulation via breakdown or arcing events. This study will discuss the pulsed electroacoustic methodology and its use on evaluating various dielectric polymer and composite films.
Combination scattering of electromagnetic waves from driven space charge waves in magnetoplasma
Space charge effects resulting from trapping of thermalized irradiation electrons in insulating materials /polyethylene terephthalate/
Space charge limitations of currents for use in dosimeters
Thermal noise in space charge limited solid state diodes by Langevin equation, relating spectral intensity for open and short circuit voltage and current
The dispersion characteristics of small signal electrohydrodynamic space charge and polarization waves in continuously and discretely stratified liquids are developed. The liquids, modeled as incompressible, inviscid, and perfectly insulating have distributions of mass density, charge density, permittivity, and electric field. A general set of relations for perturbation field and flow variables defined for a prototype layer are used to describe the dynamics of many superposed planar layers. It is shown that the general relations can be used to represent systems of coupled layers which approximate continuous distributions by a series of step functions. Specific examples of weak gradient and exponential distributions are presented showing that the solution found directly from the distributed theory is approached by the system of coupled layers, if the limit is taken in which the number of layers become large while each layer thickness approaches zero.
Molecular flow in electron bombardment ion chamber and analysis of space charge flow in ion acceleration
Conduction through thin insulating films with large ionic space charge, discussing potential barrier valley
Current increase in Townsend discharge under influence of space charging
Analytic integration of Langmuir equation for spherical space charge flow obtained in terms of Airy equation or Bessel functions solution
Coefficients of space charge effects for growing oxide films, derived from perturbation treatment, evaluated in terms of boundary concentrations of diffusing species
Monte Carlo method for determining electron flow in low density argon gas including space charge and elastic collisions
Thermionic conversion system performance analysis based on space charge theory and isothermal diode sheath theory
Compensation of ion beam space charge by electrons in high vacuum magnetic field
A high precision, high resolution Ocean Color Instrument (OCI) was developed for the Plankton, Aerosol, Cloud ocean Ecosystem (PACE) mission which required the use of electrically isolated Hybrid Bearings (silicon nitride balls). While desirable for technical performance of the instrument, this application caused portions of the instrument to become electrically isolated and come under threat of space charging effects from charged particles and the resultant differential charging. An evaluation of the environment, susceptibility of the components, such as bearings and electronics, and mitigation strategies were performed. As part of that process, simulations of the charging environment, analysis of internal mechanism charging and prediction of most likely discharge paths, testing of the bearings for susceptibility as well as resulting damage were performed and analyzed. Additionally, a novel method to deal with charging was developed. Considerations for dealing with electrically isolated mechanisms, results of the above-mentioned efforts as well as lessons learned are presented.
Ion currents may be several times Child law limit if initial kinetic energies of one-dimensional bipolar space-charge current are of order of potential energy
Design and sensitivity tests of a modified version of the so-called reversal electron attachment detector (READ) are presented. The new version uses a spherical cathode capable of emitting higher electron currents. As in the original READ (which used a planar emitter) electrons are focused into an electrostatic mirror which reverses their trajectories. In the reversal region electrons have essentially zero energy and attach to target molecules to form negative ions. The electron gun lens system has been modified using a field and trajectory code with space charge included. Electron trajectories have been calculated for 1-mA current focused into a reversal region of 3.5-mm diameter. The detection limit of the apparatus is approximately 25 times lower than for the original READ. Nonlinearity in the measured signal vs electron current is described by a model in which a spherical ball of ions expands outward with velocity determined by the space-charge force and the initial velocity of ion formation.