617.6193
km/s
0.00206
c
274.0328
m/s²
55.214
×
2.953845
km
235,625.080285
×
617.6193
km/s
0.00206
c
274.0328
m/s²
55.214
×
2.953845
km
235,625.080285
×
The Escape Velocity Calculator computes the minimum speed needed to escape the gravitational field of a body without further propulsion. Escape velocity is one of the most important concepts in spaceflight, planetary science, and astrophysics, governing everything from rocket design to whether a planet can retain an atmosphere.
Escape velocity is derived from energy conservation: the kinetic energy of a projectile at the surface (1/2 mv^2) must equal or exceed the gravitational potential energy it needs to overcome (GMm/r). Setting these equal and solving for v gives: v_esc = sqrt(2GM/r). This is independent of the mass of the escaping object and the direction of launch (assuming straight-line escape from the surface).
Earth's escape velocity is about 11.19 km/s (about 40,280 km/h). The Moon's is about 2.38 km/s — which is why the lunar module could achieve lunar orbit and return with a much smaller rocket than required to escape Earth. Jupiter's escape velocity is about 59.5 km/s, which is why it has retained its entire primordial hydrogen-helium envelope since formation.
Atmospheric retention is governed by the relationship between escape velocity and atmospheric gas velocity. Gas molecules with thermal velocities exceeding about 1/6 of escape velocity will gradually escape (Jeans escape). This explains why small, hot bodies like Mercury and the Moon lack significant atmospheres, while large, massive planets retain even light gases like hydrogen and helium.
When v_esc = c, the escape velocity equals the speed of light — the object is at its Schwarzschild radius and has become a black hole. This relationship connects escape velocity directly to black hole physics.
Escape velocity: v_esc = sqrt(2GM/r), where G = 6.674x10-11 N m² kg-2, M is mass in kg, r is radius in meters. Result in m/s, divided by 1000 for km/s. Fraction of light speed = v_esc / c, where c = 2.998x10^8 m/s. Ratio to Earth escape velocity: v_esc / 11,186 m/s. Surface gravity g = GM/r².
Escape velocity below 1 km/s (like asteroids and small moons): very easy to escape, bodies cannot retain any atmosphere. 2-5 km/s (Moon, Mars): can retain CO2 and heavier gases but not hydrogen. 10-15 km/s (Earth, Venus): can retain N2, O2, CO2 atmospheres but loses hydrogen over geological time. Above 50 km/s (gas giants): retains even hydrogen and helium.
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Earth's escape velocity is 11.19 km/s (about 40,300 km/h). Rockets must reach this speed to leave Earth's gravitational influence permanently (not counting air resistance).
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A 1.4 solar mass neutron star with 11 km radius has an escape velocity of 63% the speed of light — deep in the relativistic regime. Surface gravity is about 1.5 trillion times Earth's.
Escape velocity is the minimum speed required for an object to escape a gravitational field without any additional propulsion, assuming no atmosphere. It is derived from energy conservation: the kinetic energy at launch must equal the gravitational potential energy to infinity. v_esc = sqrt(2GM/r).
In theory, escape velocity is independent of launch direction (straight up, at an angle, or even horizontal) if there is no atmosphere. What matters is the total kinetic energy, which depends only on the speed. In practice, launching horizontally places you in orbit below escape velocity, and launching upward (or at any angle) allows you to reach escape velocity with the same speed.
Circular orbital velocity at the surface is v_orb = sqrt(GM/r) = v_esc / sqrt(2). Orbital velocity is about 0.707 times escape velocity. To leave the orbit and escape, you need to increase your speed by a factor of sqrt(2) — about 41% more. For Earth, orbital velocity at the surface (ignoring atmosphere) would be 7.91 km/s, while escape velocity is 11.19 km/s.
Gas molecules in a planet's upper atmosphere have a Maxwell-Boltzmann distribution of speeds. Molecules moving faster than about 1/6 of the escape velocity at the exosphere can escape — a process called Jeans escape. For this reason, hydrogen (lightest gas, highest thermal velocity) escapes most easily. Earth retains N2 and O2 but has lost most primordial hydrogen and helium over geological time.
From Earth's surface, escaping the Solar System requires overcoming both Earth's gravity and the Sun's gravity. The combined escape speed is about 42.1 km/s from Earth's orbit — but starting from Earth's surface you need to reach 16.6 km/s (the hyperbolic excess speed) after escaping Earth's gravity. The Voyager probes exceeded this speed using gravity assists from Jupiter and Saturn.
The cosmic velocities are defined as: first (7.91 km/s) — circular orbit at Earth's surface; second (11.19 km/s) — escape from Earth; third (16.6 km/s) — escape from the Solar System from Earth's orbit; fourth — escape from the Milky Way. Rocket missions to the outer planets and beyond must exceed the third cosmic velocity.
The formula v_esc = c coincidentally gives the correct radius for a black hole (the Schwarzschild radius), but this is a coincidence. In Newtonian mechanics, light is not affected by gravity in the same way, and the concept of a black hole does not follow consistently from Newtonian physics. The correct treatment requires general relativity, where the event horizon is a geometric feature of curved spacetime, not a classical velocity barrier.
Rocket designers must account for escape velocity when designing launch vehicles. The delta-v (change in velocity) budget for a mission begins with the surface escape velocity. For Mars missions, the lower Martian gravity (escape velocity 5.03 km/s) makes launch from the surface much easier than from Earth. This is why a Mars sample return mission can use a much smaller rocket than Earth-based launches.
The escape velocity from the Milky Way depends on position and the total (including dark matter) mass distribution. From the Sun's location (about 8.5 kpc from the Galactic center), the escape velocity is roughly 550 km/s. Stars moving faster than this are hypervelocity stars that have been ejected, often by gravitational interactions with the central supermassive black hole.
Voyager 1, launched in 1977, was given enough velocity to escape the Solar System through a combination of launch speed and gravity assists from Jupiter and Saturn. It passed the solar escape velocity long ago and is now traveling at about 17 km/s (about 3.6 AU/year) in interstellar space. Its heliocentric speed exceeds the local solar escape velocity, confirming it is on a hyperbolic escape trajectory.
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