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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. 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.

  4. Gridded ion thruster - Wikipedia

    en.wikipedia.org/wiki/Gridded_ion_thruster

    Electrostatic ion thrusters have also achieved a specific impulse of 30–100 kN·s/kg, or 3,000 to 10,000 s, better than most other ion thruster types. Electrostatic ion thrusters have accelerated ions to speeds reaching 100 km/s.

  5. NASA Solar Technology Application Readiness - Wikipedia

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

    Although the engine produces just 92 millinewtons (0.331 ounce-force) thrust at maximum power (2,100W on DS1 mission), the craft achieved high speed because ion engines thrust continuously for long periods of time. [7] "The 30-cm ion thruster operates over a 0.5 kW to 2.3 kW input power range providing thrust from 19 mN to 92 mN.

  6. 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.

  7. Dual-Stage 4-Grid - Wikipedia

    en.wikipedia.org/wiki/Dual-Stage_4-Grid

    A 4-grid ion thruster with only 0.2 m diameter is projected to absorb 250 kW power. With that energy input rate, the thruster could produce a thrust of 2.5 N . The specific impulse (a measure of fuel efficiency ), could reach 19,300 s at an exhaust velocity of 210 km/s if xenon propellant was used. [ 3 ]

  8. Game of the Day: IonDrift - AOL

    www.aol.com/news/2014-10-10-game-of-the-day-ion...

    Set ion thrusters to "race" in today's Game of the Day! IonDrift:epsilon puts you in a futuristic race where fearless pilots risk everything to claim the title of the Ultimate Racer! Blast along ...

  9. Specific impulse - Wikipedia

    en.wikipedia.org/wiki/Specific_impulse

    A variety of other rocket propulsion methods, such as ion thrusters, give much higher specific impulse but with much lower thrust; for example the Hall-effect thruster on the SMART-1 satellite has a specific impulse of 1,640 s (16.1 km/s) but a maximum thrust of only 68 mN (0.015 lbf). [45]