At an altitude of m (a typical cruising altitude for a jet airliner), the air temperature is °C and the air density is kg/m3 . What is the pressure of the atmosphere at that altitude? (Note: The temperature at this altitude is not the same as at the surface of the earth, so the calculation of Example in Section doesn't apply.)
Martian Climate. The atmosphere of Mars is mostly CO2 (molar mass 44.0 g/mol) under a pressure of 650 Pa, which we shall assume remains constant. In many places the temperature varies from 0.0°C in summer to -100°C in winter. Over the course of a Martian year, what are the ranges of (b) the density (in mol/m^3) of the atmosphere?
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Key Concepts
Ideal Gas Law
Temperature Conversion
Density of a Gas
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