Parameters

Initial Velocity (v₀)
50 m/s
Launch Angle (θ)
45°
Gravity (g)
9.81 m/s²
Moon (1.6)Earth (9.8)Jupiter (24.8)
Mass (m)
10 kg

Affects air resistance impact.

Air Resistance (Drag)
20%

Opposes motion direction.

Wind Velocity (-X)
0 m/s

Wind blowing left (needs air resistance).

Theoretical Models

Position over time
x =v₀ · cos(θ) · t
y =v₀ · sin(θ) · t − ½gt²
Max Range (R)
R =
v₀² · sin(2θ)
g
Max Height (H)
H =
(v₀ · sinθ
2g
Projectile Motion
t: 0.00s
Total Speed (|v|)

No experiments recorded yet.