Tbh, while i still don't think the thing actually work, i'm a bit perplexed at all the "it violate the conservation of momentum" crowd. I mean, there are already experiments which violate the conservation of momentum, the most famous being described by Fenyman in its book about eletromagnetism (17-4), as the disk with charged spheres that start spinning when you stop flowing current in its central solenoid . The solution to the paradox is that the momentum that is being "given" is the one lost by the field and as such give a total momentum to the material.
But if i can create such a field with simply currents and solenoids, this mean that we already accept that we just need electricity (movement of electrons) to create "real" momentum.
Now, why would it be so hard to believe that virtual electrons, created and destroyed constantly, may do the same in an hard vacuum? Casimir effects are very real, and already proved that "virtual" electrons can act on "real" matter.
Why would this be much different? If someone could explain where i'm going wrong, i'd be glad because it's bugging me.
EDIT: also technically, a laser pointer create thrust with just electricity, while being absurdly inefficient.
So we doubt an American scientist and do not even give him an opportunity to display his concept. Chinese scientists say why not worst is it works and it does well. NASA sees this and bites his idea. I saw fuck don't share no more tech. So this is how we support our greatest minds.
Aliens/time travellers have simply deemed us okay to travel further in the next ten years and so have unlocked the next layer of physics we can now access and manipulate.
Let's be fair. Scientists are frequently wring as well, and it is difficult to tell who is doing genuine science and who is not.
Let's be fair. Scientists are frequently wring as well, and it is difficult to tell who is doing genuine science and who is not.
That example isn't a case of the conservation of momentum being violated, because the total momentum in the greater system (field + solenoid) is conserved. There are no experiments that violate the conservation of energy or linear/angular momentum.
Virtual (off-shell) particles, which are essentially mathematical constructs, are allowed to "appear" not to obey the conservation of momentum and energy because of the uncertainty principle - however, their measurable effects (ie. the Casimir force) do not violate the conservation of energy.
I dont get you argument that nothing containing energy leaves the ship. An easy way out of this is the following . You can simply radiate heat outwards. Because radiation in all directions induces no net acceleration on the ship, it is not a propellant and does not contribute to the deceleration of the ship. This will explain the decreased rest mass of the ship. The fact that the engine produces heat coincides neatly with the 2nd law of thermodynamics.
also,an argument based on acceleration will work for thrust as well. Thrust just induces time dependent acceleration, and you can always slice the time interval thin enough such that over each infinitesimally small time interval, acceleration is constant. Thats fundamental calculus. So i believe my arguments still make sense.
The thrust seems fairly low compared to something like Ion drives.
Still cool even if it doesn't work outside of Earth.
They've tested it in a vacuum, so wouldn't that mean it should work in space?
They've tested it in a vacuum, so wouldn't that mean it should work in space?
They've tested it in a vacuum, so wouldn't that mean it should work in space?
That's what I thought as well.
Is this how the Event Horizon is created?
They need to remake that movie. Or another movie like it. Finding an as abandoned space ship and finding out what horrors happened on it is one of the coolest themes ever. Are any other movies like this? Ive watched Sunshine, Moon, Supernova, and Pandorum. Is interstellar any good? Similar to event horizon? Sorry for off topic

It's not known whether the test was performed in a vacuum at all yet, the project brief states:
"... within a stainless steel vacuum chamber with the door closed but at ambient atmospheric pressure..."
Which suggests they have tested in a vacuum capable environment, but not actually in a vacuum yet.
There is no way to resolve the conflict of testing in a vacuum with he statement that it took place "at ambient atmospheric pressure" other than to accept that it hasn't yet been tested in a vacuum.
That's what I thought as well.
Earth's magnetic field could be a factor I guess
If anyone spots any mistakes, please let me know, this was just a hasty calculation I did during my lunch break. However, I would expect the logarithmic time dependence to be correct even if there are errors since a rocket burning fuel has also has a velocity that scales with the natural logarithm of the mass. When accounting for the mass being lost due to energy expenditure, I would expect the velocity to scale similarly to a rocket losing mass from burning fuel.
So, so far, this is holding up to scrutiny?
For reals?
This is amazing news. Especially if they can adapt it to an actual ship and significantly cut down travel time for the Moon, Mars, etc. Hell would it be possible for this to make escaping Earth's gravity easier? Or is that still a different problem and along a different technology line?
Right, this is a potential issue. You'd want to do an experiment where you rotate the entire apparatus rather than just reversing the engine.
Given that the device doesn't actually appear to be that involved - it seems to basically be an oddly-shaped microwave oven - before you go on to space testing you probably want to go ahead and build a really big one to make sure that the signal you're seeing is real. Strap a dozen of these together and run kilowatts through them and see if you get much more thrust.
I've not checked, but while this doesn't look unreasonable it's beside the point. The spacecraft's kinetic energy still increases much faster than its velocity (edit: momentum is probably the better quantity to use here) while it's using a constant amount of energy to generate thrust. Even if acceleration is non-constant, at high velocities a velocity change dV will produce a higher energy change dE than at low velocities. With a normal rocket, this works out because it's throwing mass out behind it, which from the perspective of a stationary observer has lost kinetic energy - the exhaust is moving more slowly than it was when it was fuel being carried inside the fast rocket. You need this reaction mass to not violate conservation laws. You need a way for the system to lose energy in order for this to work, and not "lose" in the sense of emitting heat - adding heat emission makes the problem even worse because now there's even more new energy in the universe.
I've not checked, but while this doesn't look unreasonable it's beside the point. The spacecraft's kinetic energy still increases much faster than its velocity (edit: momentum is probably the better quantity to use here) while it's using a constant amount of energy to generate thrust. Even if acceleration is non-constant, at high velocities a velocity change dV will produce a higher energy change dE than at low velocities. With a normal rocket, this works out because it's throwing mass out behind it, which from the perspective of a stationary observer has lost kinetic energy - the exhaust is moving more slowly than it was when it was fuel being carried inside the fast rocket. You need this reaction mass to not violate conservation laws. You need a way for the system to lose energy in order for this to work, and not "lose" in the sense of emitting heat - adding heat emission makes the problem even worse because now there's even more new energy in the universe.
I'm not clear on why the mass of the stored energy doesn't satisfy that requirement, though. Since stored electromagnetic energy does contribute to the mass, why should the consumption of electricity be any different from a reaction mass in principle? The kinetic energy still increases with ln^2 like it would for a traditional engine due to that mass loss.
Perhaps I'm missing something here, but my point is that the ship will still lose mass, not that it is losing energy through heat emission.
I didn't type that second quote.
Was it another me?
I'm panicking.
If you have a little nuclear power cell (atomic battery) producing power, like the one in Voyager, the mass loss from the radioactive decay of the material is negligible, and does not explain or offset anything.
I'm not clear on why the mass of the stored energy doesn't satisfy that requirement, though. Since stored electromagnetic energy does contribute to the mass, why should the consumption of electricity be any different from a reaction mass in principle? The kinetic energy still increases with ln^2 like it would for a traditional engine due to that mass loss.
Perhaps I'm missing something here, but my point is that the ship will still lose mass, not that it is losing energy through heat emission.
Assuming this is true, the inventor will likely end up in Hibernity.
(+1 internet geek point if you get the reference).
sorry to bump an old thread, but just curious, would this engine work for the space station? was asking in the other thread but nobody seems to have an answer. since the space station's funding is a huge problem, would this engine help with some of that? can it keep the ISS in orbit without too much cost?
It would be cheaper to fund the station than to fund the R&D of using this engine design on the ISS, building and shipping to the ISS, and installing on the ISS.
ah, it's a shame then.