Atmospheric pressure

`P = P_0*e^(-(mu*g*h)/(R*T))`

Calculation of atmospheric pressure at altitude.
Enter 'x' in the field to be calculated.


Pressure (P) = `2.832413 * 10^4` Pa (pascal)

_____ Steps _____


`P = P_0*e^(-(mu*g*h)/(R*T))`

Inputs and conversions to SI Units

`P_0` = 101325 Pa convert

`h` = 8848 m convert

`T` = -36 °C = 237.15 K convert

Apply the formula

`P` = 28324.126181584 Pa convert

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Atmospheric pressure at altitude formula

This tool calculates the atmospheric pressure based on altitude and air temperature using the following formula:

`P = P_0*e^(-(mu*g*h)/(R*T))`

`P`: Air pressure at elevation h
`P_0`: Air pressure at sea level
`mu`: Constant, molar mass average of air: M = 0.0289644 kg/mol.
g: Earth gravity constant, g = 9.80665 m/s2
h: Altitude in meter
R: Ideal gas constant R = 8.31432 J/k.mol
T: Air temperature in Kelvin at altitude h

See also

Pressure calculators
Unit Converter