A rocket fired vertically up from the north pole achieves a velocity of $27000 \mathrm{km} / \mathrm{h}$ at an altitude of $350 \mathrm{km}$ when its fuel is exhausted. Calculate the additional vertical height $h$ reached by the rocket before it starts its descent back to the earth. The coasting phase of its flight occurs above the atmosphere. Consult Fig. $1 / 1$ in choosing the appropriate value of gravitational acceleration and use the mean radius of the earth from Table D/2. (Note:
Launching from the earth's pole avoids considering the effect of the earth's rotation.)