Thick target bremsstrahlung produced by electron bombardment of targets of Be, Sn, and Au in the energy range 0.2-2.8 MeV
Angular distribution of thick target bremsstrahlung produced by electron bombardment of Be, Sn and Au surfaces
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.
Angular distribution of thick target bremsstrahlung produced by electron bombardment of Be, Sn and Au surfaces
Cesium bombardment ion engine system design, modification, and testing
Electron bombardment hollow cathode ion thruster performance
Polished metals exposed to hypervelocity impact by micrometer size projectiles to determine bombardment effect on spectral reflectance
Electric rocket engine with electron bombardment ionization chamber
Low frequency plasma noise from mercury electron bombardment ion thrustor studied for several magnetic field configurations
Operational performance of electron bombardment mercury ion thruster system during life testing in space simulation for SERT 2
Research and development of mercury electron bombardment thrusters
Development and tests of flight prototype power conditioner for 20 cm mercury bombardment electric thruster system
Potential star tracker interference from radiation produced by mercury bombardment thrustors using electric propulsion systems
Fabrication and testing of bonded metal-ceramic, glass-coated metal, and glass-coated ceramic bonded to metal composite electrodes for cesium bombardment ion thrusters
Optical transmittance of fused silica at elevated temperatures during high energy electron bombardment
Maximum propellant utilization in electron bombardment ion thrusters using mercury for propellant
Neutralizer location for minimum accelerator erosion on 30 centimeter diameter ion bombardment thruster
Submillipound mercury electron bombardment ion thrustor efficiency, noting cathode pole piece, baffle position and geometry influence on ion chamber performance
Electron emission from He ion by proton bombardment, calculating double differential cross sections relative to ejection energy and angle
Hypervelocity projectile material impact on ultimate reflectance of bombarded polished metals from shock tube tests
Performance tests of electron bombardment ion thrustor, using xenon, krypton argon, neon, nitrogen, helium and carbon dioxide