What is the missle's speed with respect to the planet?

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The discussion centers on calculating the speed of a missile relative to a stationary planet when fired from a spacecraft moving at 0.75c. The correct formula for relativistic velocity addition is provided: Va/c = (Va/b + Vb/c) / (1 + (Va/b * Vb/c) / c2). In this scenario, Va/b is 0.30c (the missile's speed relative to the spacecraft), and Vb/c is 0.75c (the spacecraft's speed relative to the planet). The user seeks clarification on setting up inertial frames for accurate calculations.

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i am working though some practice Q's in my course book and i am stuck on this question, the book doesn't give fully worked answers so I am not sure if this is correct or not

a spacecraft moving at 0.75c fires a missle travlling at 0.30c with respect to itself at a stationary planet, what is the missles speed with respect to the planet

i think i need to use

u = v1+v2 / 1 + v1xv2 / c^2

but i am not sure if this is going to give me the speed with respect to the planet, i think i need a bit more help with how to set up the inertial frames

the frame of the spaceship is S then the missle is S' and the planet S'' ?

thanks
 
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I find it useful to write the Relativistic addition of velocities like this:

[tex]V_{a/c} = \frac{V_{a/b} + V_{b/c}}{1 + (V_{a/b} V_{b/c})/c^2}[/tex]

Where Va/c means the velocity of a with respect to c. In your problem, let a stand for the missle, b for the rocket, and c for the earth.
 

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