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ISA Atmosphere Properties Calculator

The complete standard-atmosphere row for any altitude: temperature, pressure, density, speed of sound and the δ/σ/θ ratios — troposphere and stratosphere both.

0
Temperature (°C)
0
Pressure (hPa)
0
Density (kg/m³)
0
Speed of sound (kt)
0
δ / σ / θ

Both layers modeled honestly: the linear-lapse troposphere to 11 km and the isothermal stratosphere above it with exponential pressure decay — the same two-regime model inside every air-data computer and performance code.

Formula

troposphere: T linear, p = p₀(T/T₀)^5.2559; stratosphere: T = 216.65 K, p exponential decay
References: ICAO Doc 7488/3, Manual of the ICAO Standard Atmosphere; NOAA/NASA/USAF, U.S. Standard Atmosphere 1976

⚠️ For planning and education only. Weight & balance must be computed from YOUR aircraft's actual empty weight, arm and current equipment list, and verified against the POH/AFM envelope before flight.

The complete standard-atmosphere row for any altitude: temperature, pressure, density, speed of sound and the δ/σ/θ ratios — troposphere and stratosphere both.

About ISA Atmosphere Properties Calculator

One altitude in, the whole standard-atmosphere row out: temperature, pressure in hectopascals, density in kg/m³, the local speed of sound, and the three normalized ratios engineers actually compute with. Unlike the simple troposphere-only formulas scattered online, this implements both ISA regimes — linear lapse to 11 km, then the isothermal stratosphere's exponential pressure decay — so FL450 queries return physics, not extrapolation error.

How to use ISA Atmosphere Properties Calculator

  1. 1Enter — sensible defaults are pre-filled so you see a worked result immediately.
  2. 2Read the live results: .
  3. 3Check the "With your numbers" line to see the formula troposphere: T linear, p = p₀(T/T₀)^5.2559; stratosphere: T = 216.65 K, p exponential decay substituted step by step.
  4. 4Adjust inputs (or flip the unit toggle) until the scenario matches yours, then copy or share the result.

Why use ISA Atmosphere Properties Calculator?

  • Instant, free and private — every calculation runs in your browser, nothing is uploaded
  • Built on the published formula troposphere: T linear, p = p₀(T/T₀)^5.2559; stratosphere: T = 216.65 K, p exponential decay with sources cited on the page
  • Both layers modeled honestly: the linear-lapse troposphere to 11 km and the isothermal stratosphere above it with exponential pressure decay — the same two-regime model inside every air-data computer and performance code.
  • Switch units, tweak any input and watch every result update live

Frequently asked questions

Why does the pressure formula change at 11 km?+

The hydrostatic equation integrates differently depending on the temperature profile: with T falling linearly (troposphere) it yields the power law (T/T₀)^5.2559; with T constant (stratosphere) it yields a pure exponential decay with a 6,340 m scale height. Same physics, two solutions — the kink at 36,089 ft is visible in every plotted sounding.

What fraction of the atmosphere is below an airliner?+

Pressure is the direct answer, since it measures the weight of air above: at FL300 the standard pressure is 300.9 hPa — 70% of the atmosphere's mass lies below you. At FL400 it's 81%. The 'thin air up there' is literal: cruise flight happens above two-thirds of all the air there is.

How accurate is ISA-1976 against the real atmosphere?+

As a climatological mid-latitude average, remarkably good: real monthly means deviate a few percent in density at most levels. Day to day, deviations of ±5% density and ±20 °C are routine — which is the point: ISA is the ruler, the deviation tools measure the day. For engineering (drag, performance, ballistics) ISA plus a deviation model covers nearly every use.

What's geopotential altitude in the input label?+

Altitude measured in gravity-adjusted metres — the variable the standard atmosphere's equations are actually written in. It differs from geometric (tape-measure) height by under 0.5% below 20 km, because g weakens slightly with height. Aviation altimetry, this calculator and ISA tables all speak geopotential; only space-adjacent work needs the distinction.

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