The Tsiolkovsky rocket equation shows that reaching a given velocity needs a propellant mass fraction that grows exponentially with the target delta-v — doubling the required velocity change can multiply the fuel needed several times over, not just double it.
Δv = v_e × ln(m₀/m_f) means the ratio of starting mass to final mass matters exponentially, not linearly — it’s exactly why multi-stage rockets exist: dropping empty fuel tanks partway up avoids carrying their dead weight through the entire burn.
The rocket equation assumes no external forces, so it ignores gravity losses and drag, which together can add 1.5–2 km/s to what a launch really needs. It also assumes one stage: staging throws away dry mass mid-flight and beats the single-stage number the equation gives.
Estimate with the rule, then check it against the calculator that models it properly.
Open Rocket Equation & Delta-v Budget →