True Airspeed Calculator
Enter your indicated airspeed and pressure altitude to estimate true airspeed with the well known 2 percent per 1000 feet rule of thumb. As you climb the air thins, so the aircraft slips through it faster than the airspeed indicator shows, and this tool returns both the estimated TAS and the exact percentage it added. It is a quick planning aid, not a substitute for a temperature-aware flight computer.
How to estimate true airspeed
- Type your indicated airspeed into the Indicated airspeed box, in knots.
- Type your pressure altitude into the Pressure altitude box, in feet.
- Read the True airspeed card for the estimate in knots.
- Check the Increase over IAS card for the percentage added by altitude.
- Click Copy to grab the TAS and percentage as a single line of text.
Examples
Light aircraft at 5000 ft
IAS 100 kt, 5000 ft
TAS 110 kt (+10%)
Cruise at 8000 ft
IAS 120 kt, 8000 ft
TAS 139.2 kt (+16%)
Turbine climb at 10000 ft
IAS 150 kt, 10000 ft
TAS 180 kt (+20%)
Frequently asked questions
What is the difference between indicated and true airspeed?
Indicated airspeed is what the airspeed indicator reads from dynamic pressure hitting the pitot tube. True airspeed is your actual speed through the surrounding air mass, which is higher at altitude because the thinner air produces less dynamic pressure for the same real speed.
What formula does this calculator use?
It applies the cockpit rule true airspeed = indicated airspeed times (1 + 0.02 times altitude in thousands of feet). That works out to about 2 percent added for every 1000 feet of pressure altitude, and the tool also reports that exact percentage.
How accurate is the 2 percent per 1000 feet rule?
It is a handy approximation that is close enough for rough flight planning at typical piston altitudes. Real true airspeed depends on air density, so both temperature and pressure matter. For dispatch-grade numbers use an E6B or an electronic flight computer that takes outside air temperature.
Does temperature change true airspeed?
Yes. Air that is warmer than the standard atmosphere is less dense and pushes true airspeed higher, while colder air makes it lower. This rule of thumb assumes a standard day and ignores temperature entirely, so on a hot day it will slightly underestimate your TAS.
What altitude should I enter?
Use pressure altitude, the reading you get with the altimeter set to 29.92 inches of mercury. It strips out local pressure variation, which keeps the estimate consistent regardless of the day's barometric setting.
What units does the result use?
The output matches whatever speed unit you enter. If you type knots you get knots, and the labels shown read kt. The math is a simple percentage increase, so it works the same for miles per hour or kilometers per hour if you enter those instead.
How is true airspeed different from groundspeed?
True airspeed is your speed relative to the air mass. Groundspeed is your speed over the terrain, which also depends on wind. A headwind lowers groundspeed below TAS and a tailwind raises it, so this tool gives TAS, not groundspeed.
Can I enter negative numbers or leave a box blank?
No. Both fields require a value, and neither the airspeed nor the altitude can be negative. If a box is empty or holds an invalid or negative number, the tool shows a short prompt instead of a result.
Is anything I type sent to a server?
No. The calculation runs entirely in your browser, so your airspeed and altitude entries never leave your device and nothing is stored between visits.
Learn more
- IAS, CAS and TAS: the airspeeds pilots use
How indicated, calibrated and true airspeed differ, why altitude and temperature drive the gap, and when the 2 percent rule is good enough.
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