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Le 14/03/2024 à 15:02, "Paul B. Andersen" a écrit :I do indeed understand that you telling me:A rocket is accelerating at the constant proper acceleration a.You don't understand anything I'm telling you...
An inertial frame of reference K(x,t) is at the time t = 0
instantly co-moving with the rocket.
You claim:
According to SR the speed of the rocket in K is Vr(t) = a⋅t
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Note that this means that Vr > c when t > c/a
which according to SR is impossible.
A rocket is accelerating at the constant proper acceleration a.
An inertial frame of reference K(x,t) is at the time t = 0
instantly co-moving with the rocket.
You claim:
According to SR the speed of the rocket in K is Vr(t) = a⋅t
===========================================================
Note that this means that Vr > c when t > c/a
which according to SR is impossible.
Contradicting fact:
-------------------
So this is wrong.
You can see the correct derivation here:
https://paulba.no/pdf/TwinsByMetric.pdf
See chapter 2.3, equation (15)
>
Vr(t) = a⋅t/√(1+(a⋅t/c)²)
>
Note that:
Vr → a⋅t when t → 0
Vr → c when t → ∞
>
>
Your problem is that you do not understand the difference
between proper acceleration of the rocket, and the rocket's
coordinate acceleration in the inertial frame.
>
If A is the coordinate acceleration in K, we have:
>
A = dVr/dt = a/(√(1+(a⋅t/c)²))³
>
Note that:
A → a when t → 0
A → 0 when t → ∞
>
So Vr(t) = ∫(from 0 to t)A⋅dt = a⋅t/√(1+(a⋅t/c)²)
>
You claim:
According to SR is the average speed of the rocket Vm(t) = Vr(t)/2
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>
Contradicting fact:
-------------------
This is wrong.
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Vr(t) = a⋅t/√(1+(a⋅t/c)²)
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The average speed Vm at the time t is:
Vm = (integral from t=0 to t=t of Vr(t)dt)/t
Vm = c²⋅(√(1+(a⋅t/c)²)-1)/a⋅t
>
Note that:
Vm → a⋅t/2 when t → 0
Vm → c when t → ∞
>
So:
Vm/Vr → 1/2 when t → 0
rm/Vr → 1 when t → ∞
>
So for any t > 0 Vm > Vr/2
>
It is not possible to make SR predict anything else!
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In these conditions, it is very difficult to discuss.I do understand that you find it difficult to defend your own words.
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