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  3. Escape Velocity

Gravitation · JEE & NEET Physics

Escape Velocity: notes and previous year questions

How fast to launch something so it never comes back: v_e = √(2GM/R) = √(2gR) ≈ 11.2 km/s, what it depends on, escape versus orbit, and why the Moon has no air.

Escape Velocity in short

  • Escape velocity is the least launch speed with which a body never returns.
  • It comes from energy: total energy zero at launch, ½mv_e² = GMm/R.
  • v_e = √(2GM/R) = √(2gR) ≈ 11.2 km/s for the Earth.
  • It depends only on the planet (v_e ∝ √(M/R)), not on the body's mass or the direction.

1Throw it harder

Throw a ball up and it comes back; throw it harder and it goes higher. Gravity weakens with height, so at one special speed the ball slows down forever but never stops, and never returns.

The escape velocity vev_e is the smallest launch speed with which a body never comes back: it just reaches infinity with no speed left. For the Earth, ve≈11.2v_e \approx 11.2 km/s, about 40,000 km/h.

2Where 11.2 km/s comes from

At the surface: KE=12mv2KE = \tfrac12 mv^2, U=−GMm/RU = -GMm/R. To just escape, the body arrives at infinity with KE=0KE = 0 and U=0U = 0, so its total energy must be zero:

12mve2−GMmR=0\tfrac12 m v_e^2 - \frac{GMm}{R} = 0
ve=2GMR=2gRv_e = \sqrt{\frac{2GM}{R}} = \sqrt{2gR}Using GM = gR². Earth: √(2 × 9.8 × 6.4 × 10⁶) ≈ 11,200 m/s.

With g=10g = 10 m/s² and R=6400R = 6400 km, ve=1.28×108≈11.3v_e = \sqrt{1.28\times10^8} \approx 11.3 km/s.

Since ve∝M/Rv_e \propto \sqrt{M/R}, a planet with 4 times the mass and 2 times the radius has ve=11.2×2≈15.8v_e = 11.2 \times \sqrt2 \approx 15.8 km/s. Shrinking the Earth to half its radius (same mass) also gives 2\sqrt2 times, 15.8 km/s, not double.

3What it depends on

  • Only the planet: its mass and radius.
  • Not the mass of the body: mm cancels, so a pebble and a spaceship need the same speed.
  • Not the direction: any direction works, as long as the path misses the ground; only the energy counts.

But the energy needed does grow with the mass: 12mve2=GMm/R=mgR\tfrac12 m v_e^2 = GMm/R = mgR. Each kilogram needs about 12×11,2002≈6.3×107\tfrac12 \times 11{,}200^2 \approx 6.3\times10^7 J; 1000 kg needs about 6.4×10106.4\times10^{10} J.

Bodyg (m/s²)R (km)v_e (km/s)
Earth9.86,40011.2
Moon1.61,7402.4
Mars3.73,4005.0
Jupiter2571,00060
Sun274696,000618

4Escape or orbit?

Launched sideways just above the ground, a body at the orbital speed circles the Earth:

vo=GM/R=gR≈7.9 km/s,ve=2 vov_o = \sqrt{GM/R} = \sqrt{gR} \approx 7.9\ \text{km/s},\qquad v_e = \sqrt2\,v_o
Launch speedTotal energyPath
7.9 km/sE<0E < 0circle (bound)
10 km/sE<0E < 0ellipse (bound)
11.2 km/sE=0E = 0parabola: just escapes
13 km/sE>0E > 0hyperbola: escapes with speed to spare

If the surface orbital speed is 5 km/s, the escape speed is 52≈7.075\sqrt2 \approx 7.07 km/s. A body launched at exactly vev_e has total energy zero.

5From a height, and with speed to spare

ve(h)=2GMR+h=veRR+hv_e(h) = \sqrt{\frac{2GM}{R+h}} = v_e\sqrt{\frac{R}{R+h}}From a space station 400 km up: 11.2 × √(6400/6800) ≈ 10.9 km/s.

Launched faster than vev_e, a body still has speed far away:

12mv2−GMmR=12mv∞2 ⇒ v∞=v2−ve2\tfrac12 mv^2 - \frac{GMm}{R} = \tfrac12 m v_\infty^2 \ \Rightarrow\ v_\infty = \sqrt{v^2 - v_e^2}

Launched at k vek\,v_e: v∞=vek2−1v_\infty = v_e\sqrt{k^2 - 1}. To keep 11.2 km/s far away, launch at 2×11.2≈15.8\sqrt2 \times 11.2 \approx 15.8 km/s.

Launched at exactly vev_e, the total energy stays zero, so at a distance rr: 12mv2=GMm/r\tfrac12 mv^2 = GMm/r and v=veR/rv = v_e\sqrt{R/r}. At r=4Rr = 4R it has slowed to ve/2=5.6v_e/2 = 5.6 km/s.

6Why the Moon has no air

vrms=3kT/mv_{rms} = \sqrt{3kT/m}Light, hot molecules move fastest.

A planet keeps a gas if its molecules' vrmsv_{rms} is below roughly ve/6v_e/6. Earth: ve/6≈1.9v_e/6 \approx 1.9 km/s; oxygen (about 0.48 km/s) and nitrogen (about 0.5 km/s) stay, but hydrogen (about 1.9 km/s) is at the limit, and the Earth has lost most of it. Moon: ve/6≈0.4v_e/6 \approx 0.4 km/s, so its gases escaped long ago. Jupiter, with ve≈60v_e \approx 60 km/s, keeps even hydrogen and helium.

Summary

Key ideas

  • Escape velocity is the least launch speed with which a body never returns.
  • It comes from energy: total energy zero at launch, ½mv_e² = GMm/R.
  • v_e = √(2GM/R) = √(2gR) ≈ 11.2 km/s for the Earth.
  • It depends only on the planet (v_e ∝ √(M/R)), not on the body's mass or the direction.
  • The energy needed, ½mv_e² = mgR, does grow with the mass.
  • v_e = √2 × the orbital speed at the same place (7.9 km/s at the Earth's surface).
  • E < 0 bound (circle, ellipse), E = 0 parabola, E > 0 hyperbola.
  • Escaping from a height is easier: v_e√(R/(R + h)).
  • Faster than v_e, the body keeps v∞ = √(v² − v_e²) far away.
  • A low escape speed lets gases leak away: the Moon has no air.

Every equation

Escape condition
12mve2=GMm/R\tfrac12 mv_e^2 = GMm/R
Escape velocity
ve=2GM/R=2gRv_e = \sqrt{2GM/R} = \sqrt{2gR}
Scaling
ve∝M/Rv_e \propto \sqrt{M/R}
Energy needed
E=GMm/R=mgRE = GMm/R = mgR
Orbital speed
vo=gRv_o = \sqrt{gR}
Escape and orbit
ve=2 vov_e = \sqrt2\,v_o
From height h
ve(h)=veR/(R+h)v_e(h) = v_e\sqrt{R/(R+h)}
Speed far away
v∞=v2−ve2v_\infty = \sqrt{v^2 - v_e^2}
Launched at k v_e
v∞=vek2−1v_\infty = v_e\sqrt{k^2 - 1}
On the way out at v_e
v=veR/rv = v_e\sqrt{R/r}
Gas speed
vrms=3kT/mv_{rms} = \sqrt{3kT/m}
Keeping a gas
vrms<ve/6v_{rms} < v_e/6

Previous year questions with solutions

Real JEE and NEET questions on escape velocity. Try each one before you open the solution.

Q1NEET 2026One correct option

Two planets P1P_{1} and P2P_{2} with equal mass have radii R1R_{1} and R2R_{2}, respectively, where R2=R12R_{2}=\frac{R_{1}}{2}. The escape speeds of P1P_{1} and P2P_{2} are v1v_{1} and v2v_{2}, respectively. Then v2v1\frac{v_{2}}{v_{1}} is:

  1. A2
  2. B12\frac{1}{\sqrt{2}}
  3. C1
  4. D2\sqrt{2}
Show answer and solution

Answer: Option D

ve=2GMRv_{e} = \sqrt{\dfrac{2GM}{R}}, and the masses are equal, so only the radii matter:

v2v1=R1R2=2\dfrac{v_{2}}{v_{1}} = \sqrt{\dfrac{R_{1}}{R_{2}}} = \sqrt{2}

which is D. The same mass squeezed into a smaller planet is harder to leave.

The trap is A, 22, which forgets the square root. B, 12\dfrac{1}{\sqrt{2}}, turns the ratio upside down, as if a smaller planet were easier to leave. C, 11, assumes equal masses mean equal escape velocities; the radius matters too.

Q2JEE Main 2026One correct option

The escape velocity from a spherical planet AA is 10km/s10 \mathrm{km}/s. The escape velocity from another planet BB whose density and radius are 10%10\% of those of planet AA, is ____\_\_\_\_ m/sm/s.

  1. A1000
  2. B2005200\sqrt{5}
  3. C100021000\sqrt{2}
  4. D10010100\sqrt{10}
Show answer and solution

Answer: Option D

ve=R8πGρ3v_{e} = R\sqrt{\dfrac{8\pi G\rho}{3}}, so ve∝Rρv_{e} \propto R\sqrt{\rho}. For planet BB:

vBvA=0.1×0.1=11010\dfrac{v_{B}}{v_{A}} = 0.1 \times \sqrt{0.1} = \dfrac{1}{10\sqrt{10}}

With vA=10 km/s=10 000 m/sv_{A} = 10\ \mathrm{km/s} = 10\,000\ \mathrm{m/s}:

vB=10 0001010=100010=10010≈316 m/sv_{B} = \dfrac{10\,000}{10\sqrt{10}} = \dfrac{1000}{\sqrt{10}} = 100\sqrt{10} \approx 316\ \mathrm{m/s}

which is D. The answer is asked in m/s\mathrm{m/s}, so convert the 10 km/s10\ \mathrm{km/s} first.

The trap is A, 10001000: it scales with the radius alone and forgets the density. B and C, 2005≈447200\sqrt{5} \approx 447 and 10002≈14141000\sqrt{2} \approx 1414, do not follow from RρR\sqrt{\rho} at all.

Q3JEE Advanced 2013One or more correct options

Two bodies, each of mass M, are kept fixed with a separation 2L2L. A particle of mass m is projected from

the midpoint of the line joining their centres, perpendicular to the line. The gravitational constant is G. The

correct statement(s) is (are)

  1. AThe minimum initial velocity of the mass m to escape the gravitational field of the two bodies is 4GML4\sqrt{\frac{GM}{L}}
  2. BThe minimum initial velocity of the mass m to escape the gravitational field of the two bodies is 2GML2\sqrt{\frac{GM}{L}}
  3. CThe minimum initial velocity of the mass m to escape the gravitational field of the two bodies is 2GML\sqrt{\frac{2GM}{L}}
  4. DThe energy of the mass m remains constant.
Show answer and solution

Answer: Options B, D

Each fixed body is a distance LL from the midpoint, so the potential there is −GML−GML=−2GML-\dfrac{GM}{L} - \dfrac{GM}{L} = -\dfrac{2GM}{L}. To escape from both,

12v2=2GML\dfrac{1}{2}v^{2} = \dfrac{2GM}{L}, so v=2GMLv = 2\sqrt{\dfrac{GM}{L}}

which is B. Firing it perpendicular to the line changes nothing: energy has no direction. And since the two bodies are fixed and gravity is conservative, the mechanical energy of mm, kinetic plus potential, stays the same as it flies off: D.

The trap is C, 2GML\sqrt{\dfrac{2GM}{L}}, which counts only one of the two bodies. A, 4GML4\sqrt{\dfrac{GM}{L}}, would need 12v2=8GML\dfrac{1}{2}v^{2} = \dfrac{8GM}{L}, four times the potential energy there is to pay back.

Practice questions, easy to hard

Three questions from the escape velocity practice ladder: one easy, one medium, one hard.

Q4One or more correct options

Watch the bottom line of h=Rk21−k2h = \dfrac{Rk^{2}}{1 - k^{2}} as the launch speed grows towards 2gR\sqrt{2gR}, that is as kk grows towards 11. It shrinks towards zero, and the height grows without any limit.

You met this speed before, from the other end: a body falling from rest very far away reaches the surface at exactly 2GMR=2gR\sqrt{\dfrac{2GM}{R}} = \sqrt{2gR}. For the Earth (g=9.8 m/s2g = 9.8\ \mathrm{m/s^{2}}, R=6.4×106 mR = 6.4 \times 10^{6}\ \mathrm{m}) it is about 11.2 km/s11.2\ \mathrm{km/s}. This speed is called the escape velocity, and the next rung is all about it.

Which statements are correct?

  1. AFor the Earth, 2gR≈11.2 km/s\sqrt{2gR} \approx 11.2\ \mathrm{km/s}
  2. BA heavier body must be launched faster than a lighter one to reach the same height
  3. CA rock falling onto the Earth from rest, starting very far away, arrives at about 11.2 km/s11.2\ \mathrm{km/s} if there is no air
  4. DDoubling a launch speed from the Earth, from 3 km/s3\ \mathrm{km/s} to 6 km/s6\ \mathrm{km/s}, makes the body rise more than four times as high
Show answer and solution

Answer: Options A, C, D

A: 2gR=2×9.8×6.4×106=1.2544×108 m2/s22gR = 2 \times 9.8 \times 6.4 \times 10^{6} = 1.2544 \times 10^{8}\ \mathrm{m^{2}/s^{2}}, and its square root is 1.12×104 m/s1.12 \times 10^{4}\ \mathrm{m/s}.

C: that is exactly the speed of arrival from rest at a great distance, 2GMR\sqrt{\dfrac{2GM}{R}}.

D: in h=Rv22gR−v2h = \dfrac{Rv^{2}}{2gR - v^{2}}, doubling vv makes the top four times larger, and the bottom smaller as well: 2gR−v22gR - v^{2} falls from 125.4−9=116.4125.4 - 9 = 116.4 to 125.4−36=89.4125.4 - 36 = 89.4 (in km2/s2\mathrm{km^{2}/s^{2}}). The height grows about 5.25.2 times.

B is the trap: mm cancels from the energy equation, so the height depends only on the launch speed, not on the mass. A heavier body needs more energy, but not more speed.

Q5One correct option

Nothing in the escape condition says the body must start on the surface. From any point a distance rr from the planet's centre, E=0E = 0 gives 12mv2−GMmr=0\dfrac{1}{2}mv^{2} - \dfrac{GMm}{r} = 0, so the least speed that escapes from there is

v=2GMrv = \sqrt{\dfrac{2GM}{r}}

It is smaller the further out the body starts, because it is already part of the way out of the planet's pull. Always measure rr from the centre: at a height hh above the surface, r=R+hr = R + h.

A probe is at rest at a height 8R8R above the surface of a planet whose surface escape velocity is vev_{e}. What is the least speed that lets it escape from there?

  1. Ave3\dfrac{v_{e}}{3}
  2. Bve9\dfrac{v_{e}}{9}
  3. Cve8\dfrac{v_{e}}{\sqrt{8}}
  4. Dve8\dfrac{v_{e}}{8}
Show answer and solution

Answer: Option A

The probe is r=R+8R=9Rr = R + 8R = 9R from the centre, so

v=2GM9R=132GMR=ve3v = \sqrt{\dfrac{2GM}{9R}} = \dfrac{1}{3}\sqrt{\dfrac{2GM}{R}} = \dfrac{v_{e}}{3}

which is A.

The trap is C, ve8\dfrac{v_{e}}{\sqrt{8}}, which uses the height 8R8R as the distance from the centre. B, ve9\dfrac{v_{e}}{9}, forgets the square root, and D makes both mistakes at once.

Q6Numerical answer

The density form ve=R8πGρ3v_{e} = R\sqrt{\dfrac{8\pi G\rho}{3}} says that small rocky bodies have tiny escape velocities. A person can jump upwards at about 3 m/s3\ \mathrm{m/s}.

A spherical asteroid is made of rock of density 3000 kg/m33000\ \mathrm{kg/m^{3}}. What is the largest radius it can have for a person to escape from it by jumping? Take G=6.67×10−11 N m2 kg−2G = 6.67 \times 10^{-11}\ \mathrm{N\,m^{2}\,kg^{-2}}. Give the answer in km\mathrm{km}, to one decimal place.

Show answer and solution

Answer: 2.3 km

8πGρ3=8×3.14×6.67×10−11×30003≈1.68×10−6 s−2\dfrac{8\pi G\rho}{3} = \dfrac{8 \times 3.14 \times 6.67 \times 10^{-11} \times 3000}{3} \approx 1.68 \times 10^{-6}\ \mathrm{s^{-2}}, whose square root is about 1.29×10−3 s−11.29 \times 10^{-3}\ \mathrm{s^{-1}}. Setting ve=3 m/sv_{e} = 3\ \mathrm{m/s}:

R=31.29×10−3≈2.3×103 m=2.3 kmR = \dfrac{3}{1.29 \times 10^{-3}} \approx 2.3 \times 10^{3}\ \mathrm{m} = 2.3\ \mathrm{km}

Any bigger, and the jumper comes back down. A good jump on a rock a few kilometres across is a trip to space.

The trap is forgetting the square root, which gives 31.68×10−6 m\dfrac{3}{1.68 \times 10^{-6}}\ \mathrm{m}, nearly two thousand kilometres.