Analyze parabolic flight: compute range, maximum height, time of flight, landing speed & angle. Drag-free model (vacuum) with adjustable gravity and launch height.
Projectile motion describes the curved path of an object launched into the air, subject only to gravity (and no aerodynamic drag in this ideal model). This calculator solves the fundamental equations derived from Newton's second law: horizontal motion constant, vertical motion uniformly accelerated. The result is a parabolic trajectory, foundational in ballistics, sports, and aerospace engineering.
$$ Range R = \frac{v₀² \sin(2θ)}{g} (when y₀ = 0) $$
$$ Max height H = \frac{(v₀ \sin θ)²}{2g} + y₀ $$
$$ Time of flight T = \frac{v₀ \sin θ + \sqrt{(v₀ \sin θ)² + 2 g y₀}}{g} $$
The equations of motion: \( x(t) = v_0 \cos\theta \cdot t \), \( y(t) = y_0 + v_0 \sin\theta \cdot t - \frac{1}{2} g t^2 \). Solving for the time when y(t)=0 gives the total flight time. The horizontal range is simply \( R = v_0 \cos\theta \cdot T \). The apex occurs when vertical velocity becomes zero: \( t_{peak} = \frac{v_0 \sin\theta}{g} \), and maximum height = \( y_0 + \frac{(v_0 \sin\theta)^2}{2g} \). Impact velocity components: \( v_x = v_0\cos\theta \), \( v_y = - (v_0\sin\theta - g T) \) (negative downward). These formulas assume constant g and no air resistance; they are extensively used in introductory university physics (Halliday & Resnick) and advanced trajectory analysis.
| Scenario | v₀ (m/s) | θ (°) | y₀ (m) | g (m/s²) | Range (m) | Max Height (m) | Time (s) |
|---|---|---|---|---|---|---|---|
| Standard 45° flat | 30 | 45 | 0 | 9.8 | 91.74 | 22.96 | 4.33 |
| Low angle golf | 45 | 12 | 0 | 9.8 | 170.76 | 5.02 | 3.90 |
| Elevated launch | 15 | 30 | 5 | 9.8 | 30.51 | 7.87 | 2.35 |
| Lunar projectile | 25 | 40 | 0 | 1.62 | 386.31 | 128.9 | 20.2 |
Historically, gunners used projectile theory to maximize range. For flat terrain and no air resistance, the optimum angle is 45°. However, for elevated cannons (y₀ > 0), the optimum angle slightly decreases. Our calculator allows engineers to test such scenarios: enter v₀ = 150 m/s, y₀ = 15 m, and compare range at 44° vs 45° — the difference can be dozens of meters. Moreover, military applications often include wind corrections, but the ideal drag-free model remains the baseline for fire control tables.