12 m
- Jet exit pressure, $p_e = 1$ atm = 101325 Pa
- Jet exit temperature, $T_e = 30^\circ$C = 303.15 K
- Hull drag coefficient, $k = 19$ N $\bullet$ s$^2$/m$^2$
- Air density, $\rho_{air} = 1.165$ kg/m$^3$ (This is given as the air density, but it's important to
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