Thrust-to-Weight Ratio Calculator Formula
Understand the math behind the thrust-to-weight ratio calculator. Each variable explained with a worked example.
Formulas Used
Thrust-to-Weight Ratio
twr = thrust / (mass * gravity)Net Vertical Acceleration
net_accel = thrust / mass - gravityVariables
| Variable | Description | Default |
|---|---|---|
thrust | Thrust(N) | 7607000 |
mass | Total Mass(kg) | 549054 |
gravity | Surface Gravity(m/s2) | 9.80665 |
How It Works
Thrust-to-Weight Ratio
The TWR determines whether a vehicle can lift off and how quickly it accelerates.
Formula
TWR = F / (m * g)
TWR must exceed 1.0 for liftoff. Most launch vehicles aim for 1.2 to 1.8 at ignition.
Worked Example
Saturn V first stage: 7 607 000 N thrust, 549 054 kg.
thrust = 7607000mass = 549054gravity = 9.80665
- 01TWR = F / (m * g)
- 02Weight = 549054 * 9.80665 = 5 384 000 N
- 03TWR = 7607000 / 5384000
- 04TWR = 1.413
Ready to run the numbers?
Open Thrust-to-Weight Ratio Calculator