Design and performance of a thermal storage resistojet.
Single nozzle thermal storage resistojet thrustor for low thrust satellite attitude and orbit control applications, noting design and performance
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Single nozzle thermal storage resistojet thrustor for low thrust satellite attitude and orbit control applications, noting design and performance
Liquid metal cathode electron bombardment thrustor operable at high temperatures, noting stability in neutralizer current range
Anode heat transfer in MPD arc, discussing configurations and thrustors
High endurance thermionic cathodes for Kaufman thrustors, discussing emissive coatings and emissive layer starvation
Steady flow ammonia MPD arc jet thrustor propulsion performance, discussing test chamber pressure variation, thrust data and cooling systems
Primary electric propulsion application to satellite and other space missions, considering auxiliary systems and experimental thrustor systems
Kaufman mercury-ion thrustor grid design, discussing radial slot configuration
Development of a 1-kw arc plasmajet thrustor for attitude control and orbit adjustment of a satellite
Experimental results concerning the design of resistance-heated hydrogen thrustors, including performance considerations
Space electric rocket tests /sert/ which will provide data for systems design, including neutralization of space ion beams and qualification of electric thrustors for mission applications
Solutions for knudsen flow flux distributions with particles entering circular tube through small axial orifice - rocket thrustor application
Spin stabilization and ion thrustor engines for space electric rocket test /sert/ spacecraft
Electrothermal, electrostatic and electromagnetic thrustor for spacecraft propulsion
Pulsed and continuous resistojet thrustors for attitude control and station keeping of synchronous satellite
Space propulsion systems including solid core nuclear rockets, electric propulsion thrustors and nuclear electric generators
Thrustor efficiency in pulsed coaxial gun critically dependent upon amount of neutral gas swept up by plasma as it accelerates
Stress analysis for reliability of NASA-Lewis electron bombardment thrustor used in Sert 1 spacecraft
MPD arc thrustor operated with cesium plasma and external magnetic field