x = v₀cosθ · t
y = y₀ + v₀sinθ · t − ½gt²
v_x = v₀cosθ — constant
v_y = v₀sinθ − gt — changing
g = 9.8 m/s² — always down
Inputs
Components
v_x = v₀cosθ
— m/s
v_y₀ = v₀sinθ
— m/s
Outputs
t_flight
— s
t_peak
— s
max height
— m
range
— m
v at landing
— m/s
v_x constant throughout
v_y = 0 at peak
max range at θ = 45°
symmetric when y₀ = 0