Thrust-to-Weight Ratio Calculator computes the ratio of thrust to weight for an aircraft or engine, indicating its performance and ability to accelerate or overcome gravity.
It is widely used in aerospace engineering to evaluate the power-to-weight efficiency of aircraft, rockets, and engines.
Select an aircraft/engine (optional) or input custom values. The formula is:
Use the form above to input thrust and weight/mass with their respective units, and the calculator will provide the dimensionless TWR.
Example 1 (Airbus A380): Thrust = 1,392,000 N, Mass = 575,000 kg.
Calculation: \( TWR = \frac{1,392,000}{575,000 \cdot 9.81} \approx 0.247 \)
Example 2 (Merlin 1D): Thrust = 825,000 N, Mass = 467 kg.
Calculation: \( TWR = \frac{825,000}{467 \cdot 9.81} \approx 180.1 \)
Example 3 (Custom Input): Thrust = 50 kN (50,000 N), Mass = 2 t (2000 kg).
Calculation: \( TWR = \frac{50,000}{2000 \cdot 9.81} \approx 2.55 \)
Select a preset or enter custom values to verify.
1. What does the thrust-to-weight ratio measure?
The TWR measures an object’s ability to overcome gravity or accelerate, with values > 1 indicating vertical takeoff capability.
2. Why is TWR dimensionless?
It’s a ratio of thrust (force) to weight (force = mass × g), so units cancel out.
3. What is a good TWR?
TWR > 1 is ideal for rockets or fighter jets, while commercial aircraft typically have TWR < 1 (e.g., 0.2–0.3). Engines alone often have very high TWRs (e.g., 100+).
4. Can I use custom units?
Yes, select from available units (e.g., kN, lbf for thrust; kg, lb for mass), and the calculator converts them to SI units for computation.