(c) $\frac{dM}{dt} = 0.1kg/s,\ v_{gas} = 50\ m/s$,
Mass of the rocket = $2\ kg.$ $Mv =$ constant
$- v\frac{dM}{dt} + M\frac{dv}{dt} = 0$ $\therefore\frac{dv}{dt} = \frac{1}{M}v\frac{dM}{dt}$
$\Rightarrow \ $Acceleration$\ = \frac{1}{2} \times 50 \times 0.1 = 2.5\ m/s^{2}$