Tsiolkovsky Rocket Equation Formula

Equation for calculate tsiolkovsky rocket equation is,

$$\mathrm{\Delta _v}=\mathrm{v_e}\ln \frac{\mathrm{m₀}}{\mathrm{m_f}}$$

Δ_v (delta-v) = the maximum change of velocity of the vehicle.

m₀ = the initial total mass, including propellant.

m_f = the final total mass without propellant, also known as dry mass.

v_e = the effective exhaust velocity.

ln = refers to the natural logarithm function.