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Scale height

Distance over which a quantity decreases by a factor of e

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Through Physical quantity, Natural logarithm and Atmospheric pressure

Scale height used in a simple atmospheric pressure model

For planetary atmospheres, scale height is the increase in altitude for which the atmospheric pressure decreases by a factor of e. The scale height remains constant for a particular temperature. It can be calculated by H=kBTmg, or equivalently, H=RTMg, where

kB = Boltzmann constant = 1.381×10−23 J⋅K−1‍
R = molar gas constant = 8.31446 J⋅K−1⋅mol−1
T = mean atmospheric temperature in kelvins = 250 K for Earth
m = mean mass of a molecule
M = mean molar mass of atmospheric particles = 0.029 kg/mol for Earth
g = acceleration due to gravity at the current location

The pressure (force per unit area) at a given altitude is a result of the weight of the overlying atmosphere. If at a height of z the atmosphere has density ρ and pressure P, then moving upwards an infinitesimally small height dz will decrease the pressure by amount dP, equal to the weight of a layer of atmosphere of thickness dz.

Thus: dPdz=−gρ, where g is the acceleration due to gravity. For small dz it is possible to assume g to be constant; the minus sign indicates that as the height increases the pressure decreases. Therefore, using the equation of state for an ideal gas of mean molecular mass M at temperature T, the density can be expressed as ρ=MPRT.

Combining these equations gives dPP=−dzkBT/mg, which can then be incorporated with the equation for H given above to give dPP=−dzH, which will not change unless the temperature does. Integrating the above and assuming P0 is the pressure at height z = 0 (pressure at sea level), the pressure at height z can be written as P=P0exp⁡(−zH). This translates as the pressure decreasing exponentially with height.

In Earth's atmosphere, the pressure at sea level P0 averages about 1.01×105 Pa, the mean molecular mass of dry air is 28.964 Da, and hence m = 28.964 Da × 1.660×10−27 kg/Da = 4.808×10−26 kg. As a function of temperature, the scale height of Earth's atmosphere is therefore H/T = kB/mg = 1.381×10−23 J⋅K−1 / (4.808×10−26 kg × 9.81 m⋅s−2) = 29.28 m/K. This yields the following scale heights for representative air temperatures:

T = 290 K, H = 8500 m,
T = 273 K, H = 8000 m,
T = 260 K, H = 7610 m,
T = 210 K, H = 6000 m.

These figures should be compared with the temperature and density of Earth's atmosphere plotted at NRLMSISE-00, which shows the air density dropping from 1200 g/m3 at sea level to 0.125 g/m3 at 70 km, a factor of 9600, indicating an average scale height of 70 / ln(9600) = 7.64 km, consistent with the indicated average air temperature over that range of close to 260 K.

Note:

  • Density is related to pressure by the ideal gas laws. Therefore, density will also decrease exponentially with height from a sea-level value of ρ0 roughly equal to 1.2 kg⋅m−3.
  • At an altitude over 100 km, the atmosphere is no longer well-mixed, and each chemical species has its own scale height.
  • Here temperature and gravitational acceleration were assumed to be constant, but both may vary over large distances.

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