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But, rockets carry their own reaction mass. And it's this mass - expelled out as \"exhaust\" - that gives the rocket it's acceleration. As the rocket approaches C, would not it's reaction mass increase at the same rate as the rocket's mass? The rocket's mass would be increasing, but the mass of it's exhaust would be increasing at the same rate. Wouldn't the 2 cancel eachother out?
So, what is stopping that rocket from punching through C?
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I'm trying to work the numbers to see the theoretical max limits for a rocket journey, that's why i need to understand how C effects things.
If a theoretical rocket had an exhaust velocity of C (ie: a photonic rocket), so it's reaction mass was traveling at C (ie: the theoretical max efficiency for a rocket).
If that entire theoretical rocket was reaction mass, in otherwords 100% fuel.
Then that rocket would be able to accelerate at 1G nonstop for 354 days before it runs out. That seems to be the theoretical limit.
But i'm sure C gets in the way somehow as well, how do i factor that in? Say i wanted to goto Alpha Cenauri (4.39light years away) with this theoretical rocket, what will C do to this situation? Will it ever slow down my acceleration to somethign lower than 1G?