The primary application for this thruster design is intended for satellite station-keeping, long term LEO to GEO orbit transfers and deep space applications. While a typical design could provide a 50-year life span,[citation needed] or a saving of 1000 lb (˜454 kg) of launch weight for large satellites, this type of thruster could also significantly reduce the length of interplanetary space trips.[4]
For example, a trip to Mars could be shortened to 3 months instead of the 8 to 9 months with conventional chemical rockets.[5]
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