q5

Review | Constants PartA At an altitude of 11,000 m (a typical cruising altitude for a jet airliner), the air temperature is -60.0"C and the air density is 0.313 kg/m". The What is the pressure of the atmosphere at that altitude? (Note: The temperature at this altitude is not the same molar mass of air is 28.8 g/mol as at the surface of the earth, so the equation P = Pi exp Mgy RT doesn't apply.) Express your answer with the appropriate units. ? p= Value Units Submit Request