NASA's NEXT Ion Thruster Runs Five and a Half Years Nonstop To Set New Record
cylonlover writes "Last December, NASA's Evolutionary Xenon Thruster (NEXT) passed 43,000 hours of operation. But the advanced ion propulsion engine wasn't finished. On Monday, NASA announced that it has now operated for 48,000 hours, or five and a half years, setting a record for the longest test duration of any type of space propulsion system that will be hard to beat."
Running your engines at full power but standing in one spot for 5 years. That pretty much sums up our space program since Apollo.
I want to delete my account but Slashdot doesn't allow it.
I wonder if they had felt a specific impulse to switch it off?
Which all but guarantees that this engine will never do anything more.
Sort of like the ion thruster on the Dawn probe, which left Vesta about a year ago with an ETA on Ceres sometime in 2015?
My Hope if we could build a space craft that can accelerate 9.8m/s^2 (1g) for the duration of going to Mars and Back. You go to at 1g half way to mars, then you decelerate at 1g the other half. Orbit for a period of time. Drop down a landing party for a while. And go back at 1g half way decelerate at 1g the other half. Then you would have a good long range mission with out the 0g effect messing up the body.
If something is so important that you feel the need to post it on the internet... It probably isn't that important.
Running that engine for 5 years attached to the planet already caused a diversion of 0.01 on the orbit we have around the sun! That's why the sudden global warming! Tin foil ionic hat
If you had one of these on a spacecraft like Voyager with 1000kg of fuel running for 50,000 hours, what does that acceleration translate to in terms of velocity, assuming an initial velocity after launch of something like 40,000km/h?
the growth in cynicism and rebellion has not been without cause
So, if they had launched it into space, how fast would it be going after all this time? And would it still be receiving enough energy from the sun to maintain that level of thrust?
09F91102 no, 455FE104 nope, F190A1E8 uh-uh, 7A5F8A09 that's not it, C87294CE no. Ah! 452F6E403CDF10714E41DFAA257D313F.
1G of thrust would require, as you mentioned, almost 10m/s2 of acceleration, or your mass x 10 in Newtons.
NEXT produces 236 mN of thrust at 7kW of power
A typical terrestrial nuclear power plant will produce about 1 GW of power, or enough to power 143,000 of these engines. That would result in 33,700 Newtons of thrust, able to accelerate a spacecraft at 1G weighing 3433kg.
To put that into perspective, those (143,000) engines would burn 2860kg/hr in fuel alone.
Is it just my observation, or are there way too many stupid people in the world?
Don't know where you got these numbers from, but:
- There is no way this ion engine can produce 0.3g acceleration on 2000kg probe; something is way off.
- in addition to propellant, ion engine requires power - a lot of power ; you need to add weight of nuclear reactor on top of that (which is probably only thing able to produce enough power for long term with small amount of consumable fuel); for 2000N you would need something like 50MW of constant power supply
But yes, if you can create imaginary engine giving you even 0.1g of constant acceleration for spaceship over period of few decades, entire galaxy is yours.