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  1. Solar System Escape Velocity

    Solar System Escape Velocity: Escape Velocity from a Planet and the Solar System Calculator

    Escape velocity from the central body at the orbital distance; R converted from AU to m using 1 AU = 1.495978707e11 m.

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Results

Escape velocity from the body (surface)
11,186.32
m/s  =  11.186 km/s
Escape velocity from the Solar System (at the body's orbit)
42,122.87
m/s  =  42.123 km/s
Method Energy method: v = sqrt(2GM/d)
Surface escape (km/s) 11.186 km/s
Solar-System escape (km/s) 42.123 km/s

What is the Escape Velocity Calculator?

This calculator computes two related quantities using Newtonian gravitation. First, the surface escape velocity: the minimum speed an object needs at a body's surface to break free of that body's gravity. Second, the Solar-System escape velocity: the speed (relative to the Sun) needed to leave the Solar System starting from a body's orbital distance. Pick a preset (Sun through Neptune, plus the Moon and the asteroids Itokawa and Ceres) to auto-fill the physical values, or type your own. This is pure physics and applies universally.

How to use it

Select a body from the dropdown. Its mass M (kg), radius r (km), orbital semi-major axis R (AU) and central body mass Mc (kg) fill in automatically. You may edit any field. The gravitational constant G defaults to the CODATA value 6.67430e-11 and can be changed. Press calculate to see both escape velocities in m/s and km/s.

The formula explained

Setting total mechanical energy to zero gives \((1/2)v^2 = GM/d\), so \(v = \sqrt{2GM/d}\). For the surface case, \(d\) is the body's radius converted to metres (\(r \times 1000\)). For the Solar-System case, \(M\) becomes the central mass \(M_c\) and \(d\) is the orbital distance converted to metres (\(R \times 1.495978707 \times 10^{11}\) m per AU).

$$v_{esc} = \sqrt{\dfrac{2\,\text{G}\,\text{M}}{1000\cdot\text{r (km)}}}$$$$v_{solar} = \sqrt{\dfrac{2\,\text{G}\,\text{M}_c}{1.495978707\times 10^{11}\cdot\text{R (AU)}}}$$
Rocket leaving a planet surface along an upward trajectory, with radius marked from center to surface
Escape velocity is the minimum speed needed to break free from a body's gravity, depending on its mass M and radius d.

Worked example: Earth

With \(M = 5.97237 \times 10^{24}\) kg, \(r = 6371\) km, the surface escape velocity is $$\sqrt{2 \times 6.67430 \times 10^{-11} \times 5.97237 \times 10^{24} / 6.371 \times 10^{6}} \approx 11186 \text{ m/s} \approx 11.19 \text{ km/s}.$$ At Earth's orbit (\(R = 1\) AU, \(M_c = 1.9885 \times 10^{30}\) kg), the Solar-System escape velocity is $$\sqrt{2 \times 6.67430 \times 10^{-11} \times 1.9885 \times 10^{30} / 1.495978707 \times 10^{11}} \approx 42123 \text{ m/s} \approx 42.1 \text{ km/s}.$$

Bar comparison of escape velocity heights for Moon, Earth, a larger planet and the Sun
Larger, denser bodies require much higher escape velocities.

FAQ

Why is the Solar-System value N/A for the Sun? The Sun does not orbit another body, so its orbital radius is zero and that calculation is undefined.

Does escape velocity depend on launch direction? No. Because it comes from energy conservation, only speed matters, not direction (ignoring atmosphere and rotation).

Why is the Solar-System escape so much larger than Earth's surface escape? The Sun is vastly more massive than Earth, so escaping its gravity well requires much more speed even at 1 AU distance.

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