Consider a planet with an atmosphere of ideal gas at constant temperature. The following is known:
Determine the atmospheric pressure near the top of the highest mountain. Give your answer in kilopascals, rounded to the nearest integer.
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The density of an ideal gas is directly proportional to the pressure: ρ ∝ P .
The pressure gradient is d y d P = − ρ g = − κ P , where κ is a constant depending on the gravitational constant, temperature, and molar mass of the gas.
Solving this differential equation we find P = P 0 e − κ y . It follows that γ : = − d y d P ∣ ∣ ∣ ∣ 0 = κ P 0 ∴ κ = P 0 γ , so that P = P 0 e − γ y / P 0 . Substitute the given values: P = 1 0 5 ⋅ e − 1 2 ⋅ 9 0 0 0 / 1 0 5 = 1 0 5 ⋅ e − 1 0 . 8 = 3 3 9 6 0 Pa , which we convert to 3 4 kPa.