CONTROL AND GUIDANCE OF ELECTRICALLY PROPELLED SPACECRAFT
Flight trajectory, control, guidance and equipment limitations of nuclear-electric spacecraft
SPACECRAFT DESIGN↗
SEARCH · Engineering Papers
Results for “IONIC PROPULSION”
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.
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ION ROCKET WITH A PERMANENT MAGNET
Electron bombardment ion rocket with a permanent magnet circuit described
ELECTRON BOMBARDMENT↗
ELECTRON BOMBARDMENT ION SOURCE
Electron bombardment of propellant gas using a mercury ion source
ELECTRON BOMBARDMENT↗
IN-FLIGHT GENERATION OF FUEL FOR CESIUM ION ENGINES - THE CESIUM HYDRIDE SYSTEM
Thermal decomposition of cesium hydride for in- flight fuel generation for a cesium ion engine
IONIC PROPULSION↗
Ion rocket with a permanent magnet
Permanent magnetic circuit for low current density electron bombardment ion rocket engine
MAGNETIC CIRCUIT↗
Effect of thrustor arcing on ion rocket system design
Electrode arcing effects on ion rocket thrustor system design
THRUSTOR↗
Investigation of rf noise generation from space vehicles.
Radio frequency noise generation from ion engine exhausts, noting electron cyclotron radiation from penning discharge engine
RADIO NOISE↗
A spacecraft for ion thrustor flight tests.
Spacecraft designed to provide flight test measurement of ion thrustor electrical parameters and thrust
IONIC PROPULSION↗
Ion rocket engine development summary report
Design, fabrication, life testing, and supporting research of cesium contact ion rocket engine
ROCKET ENGINE↗
A higher order paraxial ray theory.
Higher order paraxial ray method to obtain space-charge limited axial symmetry flow solutions in electrostatic systems
FLOW EQUATION↗
Development of linear-strip ion thrustors for attitude control Summary report
Single-strip cesium-contact ion thrustor for rocket attitude control
THRUSTOR↗
Design and Development of a Thermo-ionic Electric Thrustor Interim Report
Propellants and thrust performance for thermoionic electric thrustor
THERMOELECTRICITY↗
A 5-centimeter-diameter electron-bombardment thrustor with permanent magnets
Permanent magnet electron bombardment ion thrustor for station keeping and attitude control of synchronous satellite
ELECTRON BOMBARDMENT↗
Transient and Steady Performance of an Ion Rocket Thrust Augmentor Final Report
Performance of ion rocket thrust augmentor, Langmuir probe measurements, secondary electron emission from porous tungsten, and heat transfer from large diameter Pirani pressure gauges
IONIC PROPULSION↗
Operation of one-half inch diameter ion thrustor with a countercurrent electron accelerator
Operation of one-half inch diameter ion thrustor with countercurrent electron accelerator
ELECTRON ACCELERATOR↗
Secondary electron emission
Secondary electron emission from porous tungsten surfaces to determine mechanisms of beam enhancement in ion rocket thrust augmentor
ION BEAM↗
Radioisotope heating of contact ionizers
Radioisotopes for heating ionizers in contact ionization thrustors
IONIC PROPULSION↗
The accumulation of chondritic material.
Melting of solid bodies in chondrule size, discussing accumulation mechanisms involving electrostatic acceleration and gas motions
COSMOLOGY↗