From the conditions of the foregoing problem determine the boost time τ0\tau_{0}τ0 in the reference frame fixed to the rocket. Remember that this time is defined by the formula τ0=∫0τ1−(v/c)2dt \tau_{0}=\int_{0}^{\tau} \sqrt{1-(v / c)^{2}} d t τ0=∫0τ1−(v/c)2dt where dtd tdt is the time in the geocentric reference frame.