I am having difficulty solving the following problem:
How fast must a rocket travel relative to the earth so that time in the rocket "slows down" to half its rate as measured by earth-based observers?
My approach to the question:
$ \Delta t $ is the time measured by the earth-based "rest frame" observers. $ \Delta t_0 $ is the time measured by the rocket in the "moving frame" relative to earth.
If the rocket "slows down" to half its rate as measured by earth-based observers, does that mean $ \Delta t= \frac{\Delta t_0}{2} $ ?
If so, then $ \Delta t= \frac{\Delta t_0}{2} = \gamma \Delta t_0 $ , Where $ \gamma $= $\frac{1}{\sqrt[]{1-u^2/c^2}} $
Rearranging becomes $ \frac{1}{2} = \frac{1}{\sqrt[]{1-u^2/c^2}}$
so $ 1- \frac{u^2}{c^2} =2^2$
then $ c^2 (1-4)=u^2$
then $u^2=-3c^2$
However, this cannot be correct, since I get a negative square root by solving for u.
All help is greatly appreciated!