# Relatavistic velocitys

i am working though some practice Q's in my course book and i am stuck on this question, the book doesnt give fully worked answers so im 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

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