TAS Calculator
Enter flight parameters to calculate True Airspeed
Flight Parameters
KT
°C
Altitude
ft
Or use Altitude + QNH
ft
hPa
Result
True Airspeed
95.66
knots
Note: This calculator uses the International Standard Atmosphere (ISA) model for pressure calculations and accounts for actual temperature to determine air density. You can either enter pressure altitude directly or provide altitude + QNH to calculate it automatically.