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Free fall and projectile motion calculator

Fall time, range, maximum height and impact speed without air resistance, with editable g (Earth, Moon, Mars) and the worked calculation.

Parameters

0° = horizontal, 90° = straight up, negative = downward.
0 for a launch from the ground.
9.80665 = standard gravity. Moon: 1.62. Mars: 3.72.

Result

020400510range (m)height (m)
Range

40.79 m

Initial components
vx = 14.14 m/s; vy = 14.14 m/s
Calculation
t = (vy + √(vy² + 2·g·h₀)) ÷ g = (14.14 + √(14.14² + 2 × 9.807 × 0)) ÷ 9.807 = 2.884 s
Flight time
2.884 s
Maximum height
10.2 m
Impact speed
20 m/s, that is 72 km/h

Calculation, assumptions and sources

OverviewFree fall: time and impact speed from a height.

Free fall: time and impact speed from a height. Projectile motion: range, flight time, maximum height and impact speed, from the ground or from a height, angled up or down. Air resistance neglected; g editable, standard gravity by default.

Method & formulasfree fall: t = √(2h/g), v = g·t
free fall: t = √(2h/g), v = g·tcomponents: vx = v₀·cos θ, vy = v₀·sin θflight time: t = (vy + √(vy² + 2·g·h₀)) / grange: R = vx · tmaximum height: H = h₀ + vy² / 2gimpact speed: |v| = √(v₀² + 2·g·h₀)

Horizontally, v_x is constant; vertically, the acceleration is g downward, independent of the horizontal motion. The flight time is the positive root of y(t) = 0. The impact speed follows from energy conservation and depends only on v₀ and h₀, not on the launch angle.

Range (R)
horizontal distance between launch and return to the ground (zero altitude).
Maximum height (H)
height of the apex of the trajectory, where the vertical speed vanishes, measured from the ground.
Standard gravity (9.80665 m/s²)
exact conventional value, fixed by the 3rd CGPM (1901). Real gravity varies by about ±0.3% with latitude and altitude.
Validity domainAir resistance is neglected.

Air resistance is neglected. The approximation holds for a dense, compact object at moderate speed, not for a ping-pong ball, a shuttlecock or a fast projectile. The model also assumes uniform g (trajectories short compared with Earth’s radius) and a point mass without spin, hence no Magnus effect and no lift.

Maximum-range angleThe range is maximal at 45° when launching from the arrival altitude (h₀ = 0).

The range is maximal at 45° when launching from the arrival altitude (h₀ = 0). From a height, the optimal angle is less than 45° and depends on v₀ and h₀.