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  2. Ion thruster - Wikipedia

    en.wikipedia.org/wiki/Ion_thruster

    An ion thruster, ion drive, or ion engine is a form of electric propulsion used for spacecraft propulsion. An ion thruster creates a cloud of positive ions from a neutral gas by ionizing it to extract some electrons from its atoms. The ions are then accelerated using electricity to create thrust.

  3. Gridded ion thruster - Wikipedia

    en.wikipedia.org/wiki/Gridded_ion_thruster

    The gridded ion thruster is a common design for ion thrusters, a highly efficient low-thrust spacecraft propulsion method running on electrical power by using high-voltage grid electrodes to accelerate ions with electrostatic forces.

  4. Ion-propelled aircraft - Wikipedia

    en.wikipedia.org/wiki/Ion-propelled_aircraft

    Current EHD thrusters are far less efficient than conventional engines. [15] An MIT researcher noted that ion thrusters have the potential to be far more efficient than conventional jet engines. [16] Unlike pure ion thruster rockets, the electrohydrodynamic principle does not apply in the vacuum of space. [17]

  5. Hall-effect thruster - Wikipedia

    en.wikipedia.org/wiki/Hall-effect_thruster

    6 kW Hall thruster in operation at the NASA Jet Propulsion Laboratory. In spacecraft propulsion, a Hall-effect thruster (HET) is a type of ion thruster in which the propellant is accelerated by an electric field. Hall-effect thrusters (based on the discovery by Edwin Hall) are sometimes referred to as Hall thrusters or Hall-current thrusters.

  6. Field-emission electric propulsion - Wikipedia

    en.wikipedia.org/wiki/Field-emission_electric...

    This type of thruster can accelerate a large number of different liquid metals or alloys. The best performance (in terms of thrust efficiency and power-to-thrust ratio) can be obtained using high atomic weight alkali metals, such as cesium (Cs, 133 amu) and rubidium (Rb, 85.5 amu).

  7. NEXT (ion thruster) - Wikipedia

    en.wikipedia.org/wiki/NEXT_(ion_thruster)

    The NEXT thruster has demonstrated, in ground tests, a total impulse of 17 MN·s; which as of 2010 was the highest total impulse ever demonstrated by an ion thruster. [2] A beam extraction area 1.6 times that of NSTAR allows higher thruster input power while maintaining low voltages and ion current densities, thus maintaining thruster longevity.

  8. Pulsed inductive thruster - Wikipedia

    en.wikipedia.org/wiki/Pulsed_inductive_thruster

    Cross-section diagram of a pulsed inductive thruster. [1] The gas is puffed inward through a central nozzle, towards the flat electromagnetic coil where it is ionized. [2] The plasma (pink) is then accelerated to the rear by the Lorentz force. A pulsed inductive thruster (PIT) is a form of ion thruster, used in spacecraft propulsion.

  9. NASA Solar Technology Application Readiness - Wikipedia

    en.wikipedia.org/wiki/NASA_Solar_Technology...

    The NASA Solar Technology Application Readiness (NSTAR) is a type of spacecraft ion thruster called electrostatic ion thruster. [1] [2] It is a highly efficient low-thrust spacecraft propulsion running on electrical power generated by solar arrays. It uses high-voltage electrodes (including two fine grids) to accelerate ions with electrostatic ...