Air at \(0^{\circ} \mathrm{C}\) is contained in a large tank on the space shuttle. A converging section with exit area \(1 \times 10^{-3} \mathrm{~m}^{2}\) is attached to the tank, through which the air exits to space at a rate of \(2 \mathrm{~kg} / \mathrm{s}\). What are the pressure in the tank, and the pressure, temperature, and speed at the exit?