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Rocket Equation Calculator
Calculate rocket velocity using the Tsiolkovsky rocket equation
📖 Rocket Equation
The Tsiolkovsky rocket equation relates the velocity change of a rocket to its exhaust velocity and the ratio of initial to final mass. It's fundamental to rocket propulsion and spaceflight.
📊 Result
💡 Tips & Information
- Delta V is measured in meters per second (m/s)
- Formula: Δv = ve × ln(m₀/mf) (Tsiolkovsky equation)
- Higher exhaust velocity and mass ratio = more delta V
- Mass ratio = initial mass / final mass
- This equation assumes no external forces (gravity, drag)