Rocket Equation Calculator (Tsiolkovsky)
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Calculates the change in velocity (delta-v) a rocket can achieve based on propellant mass and exhaust velocity.
Results
Delta-V (m/s)
557.86m/s
Propellant Mass (kg)
200kg
Inputs
kg
kg
m/s
Calculates the change in velocity (delta-v) a rocket can achieve based on propellant mass and exhaust velocity.
Delta-V (m/s)
Propellant Mass (kg)