Experimental evaluation of a two-directional electron-bombardment ion thrustor.
Electron bombardment ion thrustors with two accelerator-grid systems for producing ion beams in directions 180 or 90 degrees apart
THRUST CONTROL↗
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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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Investigation of the discharge and exhaust beam of a small arc plasma thrustor.
Discharge and exhaust beam of small low-power DC magnetic expansion thrustor
PLASMA PROPULSION↗
Durability tests of mercury electron- bombardment ion thrustors.
Durability test of mercury electron-bombardment ion thrustors, measuring lifetime, output, power efficiency, etc
ION ENGINE↗
Development of multistrip cesium contact thrustors.
Multistrip cesium contact thrustors, integral focus life test engine and various integral focus ionizers
CESIUM ENGINE↗
Ion trajectory studies of the integral-focus, linear-strip cesium contact thrustor.
Computer program for current profile and trajectory analysis for cesium contact thrustor leading to integral focus configuration of multistrip contact engines for long space missions
TRAJECTORY ANALYSIS↗
Experimental performance of a low-thrust, divergent-flow, Contact-ionization electrostatic thrustor.
Low thrust divergent flow cesium-on-tungsten contact ionization electrostatic thrustor for satellite attitude control and stationkeeping missions
ION ENGINE↗
The distribution of neutral atoms and charge-exchange ions downstream of an ion thrustor
Distribution of neutral atoms and charge exchange ions downstream of ion thrustor
NEUTRAL PARTICLE↗
Oxide-cathode durability in mercury electron-bombardment ion thrustor
Oxide cathode durability in mercury electron bombardment ion thrustor
ION ENGINE↗
Experimental performance of a low-power MPD ARC thrustor.
Low power MPD arc thrustor design and performance with radiation cooled electromagnets and permanent magnets
RADIATION COOLING↗
The distribution of neutral atoms and charge- exchange ions downstream of an ion thrustor.
Energy and angular distributions of neutral atoms and charge-exchange ions from mercury electron bombardment thrustor, determining particle effluxes
PARTICLE FLUX↗
A thermodynamic flow analysis of particle formation efficiency in a mixed flow colloid thrustor.
Thermodynamic flow analysis of feasibility of coolant gas addition to nozzle flow for improved particle formation efficiency in mixed flow colloid thrustor
GAS COOLING SYSTEM↗
Performance tests of a 1/2-millipound /2.2 mN/ ammonia resistojet thrustor system
Performance tests of ammonia resistojet thrustor system for various spacecraft control maneuvers
Ferguson, H.↗
Performance of a 15-centimeter diameter, hollow-cathode Kaufman thrustor
15-cm diameter, hollow-cathode Kaufman thrustor for SERT 2 mission
Bechtel, R. T.↗
Magnetoplasmadynamic thrustor research Final report
Radiation-cooled and water-cooled magnetoplasmadynamic thrustors tested in 10 to kW power range with 1000 to 5000 sec specific impulse
Bennett, S.↗
A Critical Review of the Magnetoplasmadynamic /MPD/ Thrustor for Space Applications
Magnetoplasmadynamic thrustor for space applications
Kelly, A. J.↗
Experimental performance of a low-thrust, divergent-flow, contact-ionization electrostatic thrustor
Electrostatic ion thrustor employing cesium on tungsten contact ionization for satellite attitude control and stationkeeping missions
Lathem, W. C.↗
Experimental investigation of reaction control, storable bipropellant thrustors
Performance of low thrust storable bipropellant thrustors in spacecraft reaction control system
Rollbuhler, R. J.↗
Divergent-flow contact-ionization electrostatic thrustor for satellite attitude control and station keeping
Divergent-flow contact-ionization electrostatic thrustor for satellite attitude control and stationkeeping
Lathem, W. C.↗