$\bullet$$\bullet$ At an altitude of $11,000 \mathrm{m}$ (a typical cruising altitude for a
jet airliner), the air temperature is $-56.5^{\circ} \mathrm{C}$ and the air density is 0.364 $\mathrm{kg} / \mathrm{m}^{3} .$ What is the pressure of the atmosphere at that altitude? The molar mass of air is 28.8 $\mathrm{g} / \mathrm{mol}$ .