Calculate range, maximum height, and time of flight. Visualise the full trajectory arc.
Launch Parameters
Results
Trajectory
x(t) = v₀cos(θ)·t · y(t) = h₀ + v₀sin(θ)·t − ½gt² Range = v₀²sin(2θ)/g (from ground) · Max range at θ = 45°
📐 Accuracy Note: Results are calculated using standard formulas and are provided for educational and reference purposes. While we strive for accuracy, floating-point arithmetic and rounding may introduce small errors. Do not rely on this tool for safety-critical, professional, or high-precision applications without independent verification.