If you intend to create a momentum flux of $0.6$ $N$ coming out of a nozzle with an area of $1$ $cm^2$, what should be the pressure inside the air tank connected to the nozzle? Assume nozzle minor loss coefficient, $K_m$, is $1.0$ and density of air is $1.2$ $kg/m^3$.

A. 0.3 kPa
B. 1.8 kPa
C. 2.5 kPa
D. 3.0 kPa
E. 6.0 kPa