Air pressure at altitude calculator

Atmospheric pressure, temperature and air density at a given altitude.

Inputs

Air pressure at altitude calculator

1 field

Height is the adopted standard-model coordinate; geometric height is not separately converted to geopotential height. The 11000 m boundary belongs to the model layer, not a fixed tropopause in all weather. Humidity, season and actual pressure changes are excluded. The adopted rounded R=8.314462618 means this does not literally reproduce every constant in the 1976 tables.

Fill in the fields and the result will appear here automatically.

Obtain model pressure, temperature and density in the first standard-atmosphere layer for heights −430 to 11000 m. This is a consistent calculation with stated constants, not a weather forecast or measured route pressure.

FAQ
4 questions
Freshness
formula-based

How it works

Formula and logic

T=288.15−0.0065 h K; p=101325·(1−0.0065 h/288.15)^(9.80665·0.0289644/(8.314462618·0.0065)) Pa. Density ρ=p·0.0289644/(8.314462618·T). This power law uses a linear temperature lapse, not an isothermal exponential.

Example

At 2000 m the model gives 79.496 kPa,596.27 mmHg,2 °C and about 1.006 kg/m³. h=0 returns 101.325 kPa before rounding and 15 °C.

Fields and units

  • Altitude above sea level — m

How to use

  • — Enter metres relative to the adopted sea-level datum.
  • — Use a barometer for actual pressure; this form has no weather correction.
  • — kPa and mmHg rows express the same model pressure in different units.

Method and limitations

Calculation method
Formula and logic
Limitation
Height is the adopted standard-model coordinate; geometric height is not separately converted to geopotential height. The 11000 m boundary belongs to the model layer, not a fixed tropopause in all weather. Humidity, season and actual pressure changes are excluded. The adopted rounded R=8.314462618 means this does not literally reproduce every constant in the 1976 tables.

FAQ

Why does pressure not fall in proportion to height?

T=288.15−0.0065 h K; p=101325·(1−0.0065 h/288.15)^(9.80665·0.0289644/(8.314462618·0.0065)) Pa. Density ρ=p·0.0289644/(8.314462618·T). This power law uses a linear temperature lapse, not an isothermal exponential.

Does the oxygen fraction change with altitude?

No, it stays near twenty-one per cent up to very great heights. What changes is the number of molecules in the same volume — which is exactly why oxygen runs short while its percentage does not.

Why is the upper bound eleven kilometres?

Height is the adopted standard-model coordinate; geometric height is not separately converted to geopotential height. The 11000 m boundary belongs to the model layer, not a fixed tropopause in all weather. Humidity, season and actual pressure changes are excluded.

How does this compare with a barometer?

A barometer measures actual pressure. Departure from the standard model is not pressure tendency: tendency means change over time. This form has neither time nor weather observations.