Air flows into the nozzle shown in Figure $1.22,$ where the inflow air has a temperature and pressure of $27^{\circ} \mathrm{C}$ and $101 \mathrm{kPa}$, respectively, and the outflow air has a temperature of $-73^{\circ} \mathrm{C}$. Flow within the nozzle can be assumed to be adiabatic and frictionless. Estimate the pressure and density of the air exiting the nozzle.