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Escape Velocity Calculator

Calculate escape velocity v = sqrt(2GM/r) for any celestial body. Includes presets for Earth, Moon, Mars, Jupiter, Sun, and more.

v = √(2GM / r)

Escape Velocity

11.1857
km/s
m/s11,185.7265
km/h40,268.6154
Body Mass5.9720 × 1024 kg
Radius6.3710 × 106 m
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Quick Answer: What is escape velocity?

Escape velocity is the minimum speed needed to leave a celestial body's gravitational pull without additional thrust. For Earth, it is 11.19 km/s. For the Moon, just 2.38 km/s. Select a body from the presets above or enter custom mass and radius to calculate.

The Formula

ve = √(2GM / r)

G is the gravitational constant, M is the body's mass in kg, and r is the distance from the center of mass in meters. The escaping object's own mass does not appear in the formula.

Space Mission Scenarios

Apollo Lunar Return

  1. Moon escape velocity: 2.38 km/s.
  2. Ascent stage: The Lunar Module only needed to reach ~1.7 km/s to enter lunar orbit (not full escape).
  3. Trans-Earth injection: From lunar orbit, a burn of ~0.9 km/s pushed the spacecraft past escape velocity on a trajectory back to Earth.

Voyager 1 Leaving the Solar System

  1. Solar escape velocity at Earth orbit: 42.1 km/s.
  2. Strategy: Voyager used Jupiter's gravity assist to gain 16 km/s without burning fuel.
  3. Current speed: ~17 km/s relative to the Sun — well above solar escape velocity at its current distance.

Escape Velocities Across the Solar System

Body Escape Velocity Surface Gravity Atmosphere?
Moon2.38 km/s1.62 m/s²No (too slow to retain gas)
Mars5.03 km/s3.72 m/s²Thin CO&sub2; atmosphere
Earth11.19 km/s9.81 m/s²N&sub2;/O&sub2; atmosphere retained
Jupiter59.5 km/s24.8 m/s²Massive H&sub2;/He atmosphere
Sun617.5 km/s274 m/s²N/A (plasma)

Physics Tips

Do This

  • Measure r from the center of mass, not the surface. For a spacecraft in orbit, r is the orbital radius (surface radius + altitude). Escape velocity decreases with altitude, so it costs less delta-v to escape from higher orbits.
  • Remember: escape velocity = sqrt(2) × orbital velocity. If you know the circular orbital speed at a given altitude, multiply by 1.414 to get escape velocity. This is useful for quick mission planning estimates.

Avoid This

  • Don't forget atmospheric drag. The formula gives the theoretical minimum speed in vacuum. On Earth, a projectile launched at 11.19 km/s at sea level would lose most of its speed to air resistance. Real rockets reach escape velocity gradually as they climb above the atmosphere.
  • Don't confuse escape velocity with orbital insertion speed. You can orbit a body at any speed below escape velocity (at the correct altitude). Reaching orbit requires much less energy than escaping entirely — for Earth, orbital velocity is 7.9 km/s vs 11.2 km/s for escape.

Frequently Asked Questions

Does escape velocity depend on the mass of the escaping object?

No. The escaping object's mass cancels out in the derivation. A baseball and a spacecraft need the same speed to escape Earth's gravity. However, the energy required is proportional to mass, so launching a heavier object requires much more fuel.

Why doesn't the Moon have an atmosphere?

The Moon's escape velocity (2.38 km/s) is low enough that gas molecules at typical surface temperatures have thermal velocities approaching or exceeding escape speed. Over millions of years, the gas leaks away molecule by molecule — a process called Jeans escape. Earth's much higher escape velocity (11.19 km/s) keeps heavier gases like N2 and O2 permanently bound.

Can you escape a black hole?

No. Inside the event horizon of a black hole, the escape velocity exceeds the speed of light (c = 299,792 km/s). Since nothing can travel faster than light, nothing — not even photons — can escape. The event horizon is defined as the radius where escape velocity equals c.

What is a gravity assist and how does it help reach escape velocity?

A gravity assist (slingshot) trades a planet's orbital momentum for spacecraft speed. As the spacecraft swings behind a moving planet, the planet's gravity accelerates it. In the Sun's reference frame, the spacecraft gains speed equal to roughly twice the planet's orbital velocity. Voyager 1 gained about 16 km/s from Jupiter's gravity assist alone.

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