RedDwarfIV
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That would be good, but I'm afraid my Google skills were not enough to unearth such a paper. In any case, the power requirements were cut by changing the shape of the warp ring to a fatter doughnut, then adding a second ring. IIRC, anyway.Ryan_m_b said:By reference I meant to a peer-reviewed paper, not a pop-sci news report as there is no explanation in either of these. Either way lots of energy.
Depends on how big the space station is, and how strong it is structurally.Ryan_m_b said:If you accelerate in orbit you change your orbit, so that would need to be taken into consideration. Beyond that presumably most planets would have satellites in orbit so would be able to detect something like this. And destroying something would send some debris your way but if you can divert the bulk (and deal with the subsequent Kessler event) it would be preferable to do so. Or even just dodge, there's no reason why a space station couldn't have thrusters.
As for accelerating to change your orbit, I know this. The idea was that a spacecraft in a lower or higher orbit than the space station makes an intercept burn. This is exactly what a normal spacecraft would do. The difference comes when, on final approach to the space station, the spacecraft fails to slow its relative velocity and collides with the station. This means a short reaction time for the space station's command crew, and a short amount of time for the space station to do anything about it. If the space station destroys the spacecraft with weapons, then tries to dodge, then it needs to have powerful engines to move it, and be strong enough not to just fold under the force of acceleration. This is not impossible, but would be difficult (especially if you had spacecraft docked to it, because they're not structurally connected. Spacecraft under construction likely would be unable to vacate the station to let it move.)
I think a good solution to that would be to have a ban on direct orbital changes to intercept space stations. Instead, a low-thrust "spiral-orbit" where the spacecraft slowly makes its way in or out in a spiral shaped orbit. That way, relative velocity is minimised, and anyone trying a high relative velocity intercept would be immediately obvious.