Calculate pressure, temperature, density, and speed of sound for any altitude using International Standard Atmosphere (ISA) model.
The atmosphere is a layered envelope of gases surrounding Earth. Pressure, temperature, and density decrease with altitude, but the rate of change depends on the layer.
Key Variables:
| Layer | Altitude Range (km) | Temperature Gradient |
|---|---|---|
| Troposphere | 0 – 11 | −6.5 °C/km |
| Stratosphere (lower) | 11 – 20 | Isothermal (216.65 K) |
| Stratosphere (upper) | 20 – 32 | +1.0 °C/km (approx) |
This calculator uses the ISA model for 0–20 km: troposphere lapse rate 6.5 K/km, then isothermal at 216.65 K up to 20 km.