Terminal Velocity Calculator
Calculate terminal velocity for any object in air or fluid. Enter mass, drag coefficient, cross-sectional area, and fluid density. Includes skydiver cases, parachute, and time to reach terminal speed.
kg
m²
kg/m³
Terminal Velocity
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Terminal Velocity —
Terminal Velocity —
Extended More scenarios, charts & detailed breakdown ▾
kg
m²
Terminal Velocity (m/s)
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Terminal Velocity (mph) —
Time to ~95% Vt —
Professional Full parameters & maximum detail ▾
kg
m²
kg/m³
m/s²
Terminal Velocity
Terminal Velocity —
Terminal Velocity (mph) —
Drag Force at Vt —
Dynamics
Time Constant τ —
Time to 95% Vt (~5τ) —
Height Fallen by 95% Vt —
How to Use This Calculator
- Enter object mass in kg.
- Enter cross-sectional area perpendicular to motion (m²).
- Select or enter drag coefficient Cd.
- Set fluid density (air at sea level = 1.225 kg/m³).
- Results show terminal velocity in m/s, mph, and km/h. Use Extended tabs for skydiver cases and other fluids.
Formula
Vt = √(2mg / ρCdA)
m = mass (kg) | g = 9.81 m/s² | ρ = fluid density (kg/m³) | Cd = drag coefficient | A = cross-sectional area (m²)
Example
Example: 80 kg skydiver belly-to-earth, Cd=1.0, A=0.7 m², air at sea level → Vt = √(2×80×9.81/(1.225×1.0×0.7)) = 54 m/s (120 mph).
Frequently Asked Questions
- Terminal velocity is the constant speed reached when drag force equals gravitational force, giving zero net acceleration. An object stops accelerating when F_drag = mg. Formula: Vt = √(2mg / ρCdA).
- In belly-to-earth position (Cd≈1.0, A≈0.7 m²), a 80 kg skydiver reaches about 120 mph (54 m/s). Head-down (Cd≈0.7, A≈0.3 m²) gives about 200 mph. With an open parachute (Cd≈1.5, A≈40 m²), terminal velocity drops to about 15–20 mph.
- Common values: sphere 0.47, flat disk 1.17, streamlined body 0.04, human belly-to-earth ~1.0, human head-down ~0.7, open parachute ~1.3–1.5. The value depends on shape and Reynolds number.
- The time constant τ = Vt/g. An object reaches ~95% of terminal velocity after about 5τ. For a skydiver at 54 m/s, τ ≈ 5.5 s, so 95% Vt is reached in about 27 seconds of freefall (~700 m).
- Air density decreases with altitude. At 10,000 m, ρ ≈ 0.414 kg/m³ vs 1.225 at sea level. Since Vt ∝ 1/√ρ, terminal velocity at 10,000 m is about 72% higher than at sea level.
Related Calculators
Sources & References (5) ▾
- NASA Glenn Research Center – Terminal Velocity — NASA Glenn Research Center
- OpenStax University Physics Vol. 1 Chapter 6.4 – Drag Force and Terminal Speed — OpenStax
- HyperPhysics – Air Resistance and Terminal Velocity — HyperPhysics / Georgia State University
- USPA Skydiver's Information Manual — United States Parachute Association
- Hoerner S F — Fluid Dynamic Drag — Hoerner Fluid Dynamics