The rocket has an initial total mass $m_{0}$, including the fuel. When it is fired, it ejects a mass flow of $\dot{m}_{e}$ with a velocity of $v_{e}$ measured relative to the rocket. As this occurs, the pressure at the nozzle, which has a crosssectional area $A_{c}$ is $p_{e}$. If the drag force on the rocket is $F_{D}=c t,$ where $t$ is the time and $c$ is a constant, determine the velocity of the rocket if the acceleration due to gravity is assumed to be constant.