Solar flare-style rocket thruster ‘could send astronauts to outer solar system’
imeche.org
imeche.org
All these technologies are limited by their power source, not by the thruster. That's the actual problem.
If you use higher exhaust velocity, you need less propellant but need more power. After a certain point, power source mass dominates the propellant mass. The total system gets worse with higher exhaust velocity than that.
Aka 1/100 th the mass = 100 times as much total energy.
Full paper: https://arxiv.org/abs/2011.04192
Edit: To be clear about the unreality of field lines, since that's apparently necessary: magnetic fields are not made of finite numbers of discrete 1D elements. They are continuous. The placement of individual "field lines" in a drawing is purely arbitrary. This part I understand quite well.
Magnetic field is a vector field, not scalar field.
Magnetic field line is visualization of the direction of the field, not related to the strength. The strength shows in the density of the field lines.
Because nothing is 100% efficient, high specific impulse means dissipating a lot of waste heat. Increase the thrust too much and you melt your vehicle.
That looks like a Freudian typo. They get up to their top speed faster, but that top speed is lower. Their high thrust comes from spewing out lots of mass at relatively low exhaust velocity, i.e. low specific impulse. And delta-v is directly proportional to specific impulse:
https://en.wikipedia.org/wiki/Tsiolkovsky_rocket_equation
The lady's quote may have been a reference to gravitational assist, which must currently be used to get planetary probes to destination with puny chemical rockets:
https://en.wikipedia.org/wiki/Gravity_assist
It gets the job done... eventually, after long detours around another planet or two than the one you actually want to reach.
Also, how is this better than existing ion thrusters? Isn't it just a bigger ion thruster?
Besides just operating on a different principle, the theoretical exhaust velocity is about ten times higher than the highest actually flown ion thruster.
So flying the same mission with this thruster would require significantly less propellant. But you don't get to throw something out the back of the spacecraft faster for free. Kinetic energy scales as the square of velocity, so ~10x exhaust velocity is going to mean ~100x power draw.
Is that it?
magnetic reconnection
– a process found throughout the universe, including the surface of the Sun – in which
magnetic field lines converge, suddenly separate, and then join together again
,
generating lots of energy
. Reconnection also occurs inside doughnut-shaped tokamak fusion devices."
(Side note: I think that there's something here with respect to understanding Energy -- itself...
Also, I think the word "Energy" is etymologically interesting... because we see the same root: "En" -- in words like 'Entangle', 'Entropy' and 'Enharmonic'... is there a relationship there? Or is it mere coincidence?)
Future ToDo: Study Magnetic Reconnection in the context of understanding Energy...
Maybe it's a bit of a Rorschach test, but I thought the comment sounded suspiciously like a reference to a Star Trek: TNG episode with a similar plot about warp drives[1].
[1] https://memory-alpha.fandom.com/wiki/Force_of_Nature_(episod...