NASA's Evolutionary Xenon Thruster (NEXT) ion engine has set a new world record by clocking up 43,000 hours of continuous operation at NASA’s Glenn Research Center’s Electric Propulsion Laboratory. The seven-kilowatt thruster is intended to propel future NASA deep space probes on missions where chemical rockets aren't a practical option.
Ion propulsion has come a long way from the 1960s when it was an engineering curiosity with a cool Star Trek name. Instead of burning fuel, an ion thruster gets its electrical power from solar panels or a nuclear power source. It uses this electricity to ionize molecules (in NEXT’s case, xenon) and then a cathode to accelerate them electrostatically. As the molecules shoot out the back of the engine, they create thrust.
That sounds simple, but the amount of thrust is tiny – about the equivalent of the weight of a coin resting on a table. Where the ion thruster has it over chemical rockets is, firstly, in terms of efficiency – ion thrusters are 10 to 12 times as fuel efficient as chemical rockets. Secondly, an ion thruster can run for a much longer period of time. Where chemical rockets burn for minutes, ion thrusters can burn for thousands of hours, which allows that tiny amount of thrust to build up into speeds needed for deep space missions.
The NEXT ion thruster is one of NASA’s latest generation of engines. With a power output of seven kilowatts, it’s over twice as powerful as the ones used aboard the unmanned Dawn space probe. Yet it is simpler in design, lighter and more efficient, and is also designed for very high endurance.
Its current record of 43,000 hours is the equivalent of nearly five years of continuous operation while consuming only 770 kg (1697.5 lbs) of xenon propellant. The NEXT engine would provide 30 million-newton-seconds of total impulse to a spacecraft. What this means in simple terms is that the NEXT engine can make a spacecraft go (eventually) very far and very fast.
Source: NASA
Now, what kind of nuclear power will they use to run it? How much does it mass? What is it's fuel mass loss? Couldn't they use a denser, solid material instead of xenon and heat it to the useful temperature and save on storage mass/volume? Can the process be scaled up to 1000 times current power? Can any form of mass be used as long as it is heated to gas/vapor temperature? If so, then you could use solar panels when near a sun for power and then use their mass as fuel when away from the sun. Thus reducing vehicle mass at the same time.
How far? How fast?
This engine is for space travel. Not take-offs or landings. And in space, where there's pretty much nothing to slow down the spacecraft, any amount of force will do. This engine is a constant, reliable and durable source of thrust, which is exactly what NASA wanted for space travel. This engine is gonna get people to Mars one day.