kev said:
The correct equation for the proper time d \tau of the traveling twin with cruising time T_c and acceleration time T_a (both as measured in the inertial stay at home twins rest frame) can be stated as a function of v only like this:
d \tau=\frac{T_c}{\gamma}+\frac{c T_a}{v \gamma} \, \, asinh(v \gamma/c)
Where v is the cruising velocity and \gamma is 1/\sqrt{1-v^2/c^2}.
It depends on how you choose to express things, your method avoids having to know the value of the proper acceleration while starthaus' equation assumed we did know it. If we do know the value of the proper acceleration
a, we also know the rocket will be decelerating from v to 0 for T
a/2 and accelerating from 0 to v for T
a/2, and according to the http://math.ucr.edu/home/baez/physics/Relativity/SR/rocket.html , the proper time for a rocket that accelerates with constant proper acceleration
a starting from a speed of 0 would be given by tau = (c/
a)*arcsinh(
aT/c), so for T=T
a/2 we get tau = (c/
a)*arcsinh(
aT
a/2c), and by the symmetry we can double that to get the total proper time elapsed from the beginning of the acceleration to the end, giving tau = (2c/
a)*arcsinh(
aT
a/2c). So, I get a total elapsed time of:
d \tau=\frac{T_c}{\gamma}+\frac{2c}{a} \, \, arcsinh(a T_a / 2c)
If we want to express it without reference to
a, another equation on the relativistic rocket page says that velocity v as a function of coordinate time T would be v(T) = aT / sqrt[1 + (aT/c)^2], so if we know it takes a time of T
a/2 to go from 0 to the cruising speed v, that means that v = aT
a / 2 * sqrt[1 + (aT
a/2c)^2], which means:
v^2 = a^2 T
a^2 / 4*[1 + (a^2*T
a^2 / 4c^2)]
4v^2 + 4*v^2*a^2*T
a^2 / 4c^2 = a^2 * T
a^2
4v^2 + (v^2/c^2)*a^2*T
a^2 = a^2*T
a^2
4v^2 = a^2*T
a^2*(1 - v^2/c^2)
a^2 = 4v^2 / (T
a^2 * (1 - v^2/c^2))
a = 2v*gamma/T
a
Substituting that into my equation above:
d \tau=\frac{T_c}{\gamma}+\frac{c T_a}{v \gamma} \, \, arcsinh(v\gamma /c)
...which is the same as the equation you wrote down.
edit: whoops, I read your post hastily and thought you were objecting to the part of starthaus' post where he wrote the equation \frac{c}{a} arcsinh(aT_a/c) for the proper time during the acceleration phase, but now I think you probably objecting to this other equation starthaus posted:
d \tau=2T_c/ \sqrt{1+(aT_a/c)^2}+4\frac{c}{a} asinh(aT_a/c)
Maybe in this equation starthaus is actually letting T
a represent half the acceleration period, which would explain why he uses asinh(aT
a/c) rather than asinh(aT
a/2c) as I did, but why is there a 4 out in front? I don't know where the first term comes from either...