ELECTRON BOMBARDMENT ION SOURCE
Electron bombardment of propellant gas using a mercury ion source
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Electron bombardment of propellant gas using a mercury ion source
Plasma studies in electron bombardment ion engine
Electron bombardment ion source used with various gases to evaluate ion chamber and accelerator system performance
The effects of 5 KeV argon and oxygen ion bombardment on FeTiO3 (ilmenite) at low temperatures have been studied using X-ray photoelectron spectroscopy (XPS). Also, using this same technique, the adsorption of O2, NO, N2O, and CO at 300 K and the adsorption of O2 and D2O at 150K have been studied. Argon and oxygen ion bombardment of ilmenite have confirmed earlier studies on metal oxides that argon ions generally reduce the anion species while oxygen ions generally oxidize the anion species. The two iron states involved were Fe sup +2 and Fe sup O. The reduction of Ti sup +4 was not verified although a significant shift in the Ti(2p1,3) binding energies toward the metallic state was observed after oxygen ion bombardment at low temperatures. At temperatures above 150K, O2 adsorbs dissociatively on ilmenite while D2O adsorbs molecularly below 170K. Above 300 K No, N2O, and CO do not appear to adsorb dissociatively. Low temperature adsorption of D2O was found to be inhibited by predosing the ilmenite with O2.
Plasma measurements in cesium electron bombardment ion engine indicate that reversed cathode-anode configuration improves radial ion distribution
Plasma characteristics of electron bombardment ion engine
High voltage mercury electron bombardment ion thruster power efficiency
Beam vector control from ion bombardment thrustors with dual grid electrostatic, movable screen electrode and discharge chamber extraction systems
Accelerator grid durability tests of mercury electron bombardment ion thrusters
Plasma measurements in cesium electron bombardment ion engine indicate that reversed cathode-anode configuration improves radial ion distribution
Electron-bombardment ion rocket engine with permanent magnet
Durability test of mercury electron-bombardment ion thrustors, measuring lifetime, output, power efficiency, etc
Oxide cathode durability in mercury electron bombardment ion thrustor
The erosion of frozen SO2 due to bombardment by both light and heavy ions (He and F) was measured for bombarding energies of 0.08 to 1.3 MeV/amu. The number of SO2 molecules ejected from the target per incident ion (i.e., the sputtering yield) was 50 for 1.5 MeV He ions and 7300 for 6 MeV F ions. Ion bombardment followed by heating produced an oxygen/sulfur residue which was much more stable against subsequent ion bombardment than the initial frozen SO2. The erosion rate of SO2 frost on Jupiter's moon Io depends strongly on the elemental composition and energy spectra of the magnetospheric ion flux which bombards the surface. The combined effects of ion bombardment and heating which produced residues on the target substrates may also occur on Io from magnetospheric ion bombardment and heating by volcanism. The experimental results compare favorably with a new model of the sputtering process which considers the energy loss of the incident ion to electronic excitation in the target.
Experimental study of an electron bombardment ion motor using cesium as an expellant
Potentialities of electron bombardment ion engines for electric propulsion
Surface blistering of metals due to low energy hydrogen ion bombardment, determining solar absorptance change in gold-plated specimens
Onset of anomalous diffusion in electron- bombardment ion thrustor