cfrogue
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DaleSpam said:Any of the PF mentors or science advisors that post here.Yes, S and S' disagree on the distance. In S the distance is fixed at d as a part of the specification of the problem. In S' the distance is found by equation 4:
[tex]d' = \gamma d[/tex]
or, more explicitly by substituting in equation 1
[tex]d' = d \frac{1}{\sqrt{1-v^2}}[/tex]
As you can plainly see, d' depends on the velocity v (in units where c=1) and not on the acceleration a. So, when you stop accelerating you do not change v and therefore you do not change d'.
More explicitly, let the acceleration stop at a time [itex]t_f[/itex] (in the unprimed frame) where the ship has obtained a velocity [itex]v_f[/itex] (in the unprimed frame). Since the acceleration has stopped, the velocity at any time [itex]t \geq t_f[/itex] is also [itex]v_f[/itex]. Since d' depends only on v then [itex]d'_f[/itex] also remains constant after the acceleration has stopped and equal to [tex]d'_f = d \frac{1}{\sqrt{1-v_f^2}}[/tex]
Yes, therefore, the ship's frame and the launch frame will disagree on the distance after acceleration.
The launch frame still has it at d < d'.
Therefore, after acceleration, a launch frame must apply the above equations of yours and the paper's and calculate this new d' itself and then apply this further for LT if that is the goal of the frame.
Do you agree?