Skip to main content
Calcimator

Standard Atmosphere (ISA) Calculator

Look up ISA standard atmosphere values at any altitude: temperature, pressure, density, density ratio, and speed of sound.

Inputs

ft

Troposphere: 0–36,089 ft, Stratosphere: 36,089–65,617 ft

Results

ISA Temperature

74.05°F

Pressure

696.8 hPa

ISA Temperature23.3°F
Pressure20.58 inHg
Density Ratio (σ)0.7385
Air Density0.9046 kg/m³
Speed of Sound638 kt
Pressure Ratio (δ)0.6877
Temperature Ratio (θ)0.9312
How to Use This Calculator
  1. Enter any altitude to see ISA standard atmosphere properties.
  2. Use ISA temperature to calculate ISA deviation (OAT − ISA temp).
  3. Density ratio is used in airspeed conversions (TAS = CAS ÷ √σ).

How the result changes with Altitude

AltitudeISA TemperaturePressure
015°C1,013.3 hPa
18,000-20.7°C506 hPa
35,000-54.3°C238.4 hPa
36,089-56.5°C226.3 hPa

What each input means

Altitude
Altitude above mean sea level in feet.

What each result means

Density Ratio (σ)
Ratio of density to sea-level standard.

How this is calculated

Worked example, using the default values

  1. ISA Temperature
    T = 15°C − 2°C × (Alt ÷ 1000 ft)
    15 − 2 × (10,000 ÷ 1000) = -4.8°C (23.3°F)
  2. Atmospheric Pressure
    P = P₀ × (T/T₀)^(g/LR)
    101325 × (268.3 / 288.15)^5.256 = 696.8 hPa (20.58 inHg)
  3. Air Density
    ρ = P / (R × T)
    69682 / (287.05 × 268.3) = 0.9046 kg/m³ (σ = 0.7385)
  4. Speed of Sound
    a = 38.967 × √(T in Kelvin)
    38.967 × √268.3 = 638 kt

The questions that sit next to this one — chosen by subject, including calculators filed under a different category.

More in Aviation, Marine & Transport.