Skip to main content
JEE · NEET Physics

Class 11 · Chapter 8

Gravitation

Overview, notes, short notes, formula sheet, daily practice problems, previous year questions, and videos for this chapter — all in one place.

Gravitation Formula Sheet

10 formulas across 3 topics in Gravitation.

1 min read

Updated 2026-07-03 · v1.0.1

Newton's Law of Gravitation & Field

Every mass attracts every other mass. The inverse-square law plus superposition is the entire foundation of this chapter.

F = G m₁m₂ / r²

Newton's law of gravitation

EasyAsked very oftenJEE MainNEETMHT-CETBoards
Variables used in this formula, with units and dimensions
SymbolMeaningUnitDimension
Guniversal gravitational constantG = 6.67 × 10⁻¹¹ N·m²/kg²N·m²/kg²[M⁻¹L³T⁻²]
m₁, m₂the two point masseskg[M]
rseparation between their centresm[L]

Valid when

  • Point masses, or spheres with uniform (radial) density measured centre-to-centre

Common mistakes

  • Gravitational force is ALWAYS attractive — no gravitational shielding exists

g = GM / R²

Acceleration due to gravity at a planet's surface

EasyAsked very oftenJEE MainNEETMHT-CETBoards

mg = GMm/R² on a surface mass

Variables used in this formula, with units and dimensions
SymbolMeaningUnitDimension
Mmass of the planetkg[M]
Rradius of the planetm[L]

Common mistakes

  • g is independent of the falling body's mass — that is the equivalence of inertial and gravitational mass

g(h) = g (1 − 2h/R) for h ≪ R; g(h) = gR²/(R+h)² exactly

Variation of g with height

EasyAsked very oftenJEE MainNEETMHT-CETBoards

Binomial expansion of gR²/(R+h)² for small h/R

Variables used in this formula, with units and dimensions
SymbolMeaningUnitDimension
hheight above the surfacem[L]
Rplanet radiusm[L]

Valid when

  • The (1 − 2h/R) form is an approximation valid only for h ≪ R

Common mistakes

  • Depth variation is DIFFERENT: g(d) = g(1 − d/R) — factor 1, not 2; g falls linearly to zero at the centre

Worth remembering

  • Inside a uniform spherical SHELL, the gravitational field is exactly zero everywhere
  • At depth d, only the inner sphere of radius (R − d) attracts — the outer shell contributes nothing

Gravitational Potential & Energy

With the zero of potential energy at infinity, all bound systems have negative energy — the sign carries the physics.

U = − G M m / r

Gravitational potential energy (zero at infinity)

EasyAsked very oftenJEE MainJEE AdvNEETMHT-CETBoards

Work done by gravity bringing m from infinity to r

Variables used in this formula, with units and dimensions
SymbolMeaningUnitDimension
Upotential energy of the pairJ[ML²T⁻²]
rcentre-to-centre separationm[L]

Valid when

  • U = mgh is this formula's near-surface approximation for the CHANGE in U

Common mistakes

  • U is negative and INCREASES (toward zero) as r increases — 'less negative' means higher energy

V = − G M / r

Gravitational potential

MediumAsked oftenJEE MainNEETMHT-CET
Variables used in this formula, with units and dimensions
SymbolMeaningUnitDimension
Vpotential (PE per unit mass)J/kg[L²T⁻²]

Valid when

  • Inside a uniform solid sphere the potential at the CENTRE is −3GM/2R (1.5× the surface value)

v(e) = √(2GM/R) = √(2gR)

Escape velocity

EasyAsked very oftenJEE MainJEE AdvNEETMHT-CETBoards

Total energy zero at launch: ½mv² − GMm/R = 0

Variables used in this formula, with units and dimensions
SymbolMeaningUnitDimension
v(e)escape speed from the surface11.2 km/s for Earthm/s[LT⁻¹]

Valid when

  • Independent of the projectile's mass AND of launch direction (ignoring rotation and atmosphere)

Common mistakes

  • v(e) = √2 × v(orbital, low orbit) — remember the √2 bridge between the two speeds

Worth remembering

  • Total energy decides fate: E < 0 bound (ellipse/circle), E = 0 parabola (barely escapes), E > 0 hyperbola

Satellites & Kepler's Laws

A satellite is perpetual free fall — gravity supplies exactly the centripetal force. Every orbital formula falls out of that single equation.

v(o) = √(GM/r); near surface v(o) = √(gR) ≈ 7.9 km/s

Orbital velocity

EasyAsked very oftenJEE MainJEE AdvNEETMHT-CETBoards

Gravity as centripetal force: GMm/r² = mv²/r

Variables used in this formula, with units and dimensions
SymbolMeaningUnitDimension
v(o)orbital speed for a circular orbit of radius rm/s[LT⁻¹]
rorbit radius from the planet's CENTRE (r = R + h)m[L]

Valid when

  • Circular orbit
  • Higher orbit → SLOWER speed

Common mistakes

  • r is measured from the planet's centre, not from the surface — forgetting to add R to the height is the classic slip

T = 2π √(r³/GM)

Time period of a satellite

EasyAsked very oftenJEE MainNEETMHT-CETBoards

T = 2πr / v(o)

Variables used in this formula, with units and dimensions
SymbolMeaningUnitDimension
Torbital periods[T]

Valid when

  • This IS Kepler's third law: T² ∝ r³
  • Geostationary orbit: T = 24 h, r ≈ 42000 km, equatorial plane, west-to-east

E = −GMm/2r; K = +GMm/2r; U = −GMm/r

Energies of an orbiting satellite

MediumAsked very oftenJEE MainJEE AdvNEETMHT-CET

K = ½mv(o)² with v(o)² = GM/r; E = K + U

Variables used in this formula, with units and dimensions
SymbolMeaningUnitDimension
Etotal mechanical energy of the orbitJ[ML²T⁻²]

Valid when

  • The memory pattern: U = 2E, K = −E, |U| = 2K

Common mistakes

  • Binding energy = +GMm/2r — the energy you must SUPPLY to free the satellite

T² ∝ a³ (a = semi-major axis)

Kepler's three laws

EasyAsked oftenJEE MainNEETMHT-CETBoards
Variables used in this formula, with units and dimensions
SymbolMeaningUnitDimension
asemi-major axis of the elliptical orbitm[L]

Valid when

  • 1st law: orbits are ellipses with the Sun at one focus
  • 2nd law: equal areas in equal times (angular momentum conservation)
  • 3rd law: T² ∝ a³

Common mistakes

  • 2nd law consequence: a planet moves FASTEST at perihelion (closest approach), slowest at aphelion

Worth remembering

  • A satellite needs no fuel to stay in orbit but plenty to CHANGE orbit — raising the orbit costs energy even though the speed decreases
  • Weightlessness in orbit is free fall, not absence of gravity — g at ISS altitude is still ≈ 90% of surface g

NEET repeats escape/orbital velocity ratios yearly; JEE Advanced uses elliptical orbits where only L and E are conserved — apply both at perigee and apogee.

Stuck on a concept in Gravitation?

Message Ajay Sir directly on WhatsApp for doubt support on this chapter.