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JEE Main (Engineering) · Physics (JEE & NEET)

Gravitation

Universal law of gravitation, gravitational field and potential, escape and orbital velocity, and Keplers laws of planetary motion.

Nine concepts, and almost every one of them turns on a sign or a power of r. Gravitation is where marks are lost fastest by measuring from the wrong place — so every number below is worked from the centre outwards, and every negative sign is there on purpose.

  • JEE Main (Engineering)
  • Medium level
  • 9 concepts
  • 5 practice questions

1Newton's law of gravitation

Every particle attracts every other along the line joining them with F = Gm₁m₂/r², where G = 6.67 × 10⁻¹¹ N m² kg⁻². The force is always attractive, cannot be screened off, and acts equally on both bodies whatever their masses: the Earth pulls a falling apple exactly as hard as the apple pulls the Earth. Only the accelerations differ, and they differ by the mass ratio.

G is the smallest constant anybody measures, which is why gravitation is undetectable between laboratory objects and dominant between planets. Several masses acting at once add as a vector sum — each pull computed as though the others were not there.

Figure. The two nearest masses pull with equal force at right angles, so their resultant already lies along the diagonal; the far corner, at twice the distance squared, adds a third as much again in the same direction. The net pull is 1.91 Gm²/a² straight at the centre of the square, which is where symmetry says it must point.

Adding gravitational pulls

  1. One pair at a timeCompute each Gm₁m₂/r² as if the other masses were absent. Superposition here is exact, not an approximation.
  2. Draw the directionsEvery arrow points from the mass being pulled towards the mass doing the pulling. Attraction only, so there are no signs to guess.
  3. Add as vectorsResolve along convenient axes, or exploit symmetry — equal masses placed symmetrically usually cancel in pairs.

Four masses at the corners of a square

Four particles, each of mass m, sit at the corners of a square of side a. Find the net gravitational force on any one of them.

  • Two adjacent masses, distance a, at 90° to each other√2 Gm²/a² along the diagonal
  • Diagonal mass, distance a√2: Gm²/(a√2)²Gm²/2a², same direction
  • F = (√2 + ½)Gm²/a²1.91 Gm²/a², towards the centre

Pro tip. The half is the row people drop: the diagonal separation is a√2, so squaring it halves the force, it does not divide it by √2. Add the diagonal contribution last — it already points along the resultant of the other two, so no resolving is needed.

The Earth pulls a falling apple with a force F. The force the apple exerts on the Earth is
  1. Very much smaller than F, since the apple is tiny
  2. Exactly F, directed the other way
  3. Zero — the apple is in free fall

F = Gm₁m₂/r² is symmetric in the two masses, and Newton's third law says the same. What is not symmetric is the acceleration: a = F/m, so the Earth's response is smaller by the mass ratio, about 10²⁵.

2The field of a sphere

The gravitational field is force per unit mass, g = GM/r², directed inwards. What makes it usable is the shell theorem: a uniform spherical shell attracts an outside particle exactly as if all its mass sat at the centre, and exerts no force at all on a particle anywhere inside it. So outside the Earth g falls as 1/r² measured from the centre, and inside it only the mass in the sphere beneath you counts.

For a uniform sphere that enclosed mass is M(r/R)³, so g = GMr/R³ climbs linearly from zero at the centre to its maximum at the surface — which is the depth formula g_d = g(1 − d/R). Real Earth is not uniform; its core is far denser than its crust, so measured g actually rises a little for the first 2900 km down. Use g(1 − d/R) as the uniform-sphere result the exam asks for, and know why it is idealised.

Figure. Plotted for a sphere of uniform density: a straight rise from zero at the centre, a sharp corner at the surface, then a 1/r² tail. The peak is at r = R and nowhere else — g is smaller both above the surface and below it. At r = 2R the field is a quarter of surface g, and at r = 3R a ninth.

Why only the enclosed mass counts

  1. Split the body into shellsAny spherically symmetric body is a stack of thin uniform shells, one inside the next.
  2. Shells above you do nothingInside a shell the pulls from opposite sides cancel exactly: the far patch subtends the same cone, so its area grows as the square of its distance — and 1/r² cancels that square exactly.
  3. Shells below you act from the centreEach of those pulls as a point mass at the centre, so only the mass within radius r survives — hence g ∝ r inside a uniform sphere.

Weighing the Earth from g

Given g = 9.8 m s⁻², R = 6.4 × 10⁶ m and G = 6.67 × 10⁻¹¹ N m² kg⁻², find the Earth's mass and its mean density.

  • R² = (6.4 × 10⁶)²4.10 × 10¹³ m²
  • M = gR²/G = 9.8 × 4.10×10¹³ / 6.67×10⁻¹¹6.0 × 10²⁴ kg
  • Volume = (4/3)πR³1.10 × 10²¹ m³
  • Mean density = M/V5.5 × 10³ kg m⁻³

Pro tip. GM = gR² is the substitution that carries this whole chapter: it removes both G and M from any problem set near a planet whose surface g you know. The density is the bonus — 5.5 × 10³ kg m⁻³ is twice that of surface rock, which is how we know the Earth has a dense metallic core without ever drilling to it.

A tunnel is bored towards the centre of a planet of uniform density. Halfway down, the value of g is
  1. 4g, since g goes as 1/r²
  2. g/2
  3. g/4

Inside a uniform sphere only the enclosed mass acts, and it grows as r³ while 1/r² shrinks — the two combine to g ∝ r. At r = R/2 that is g/2. The 1/r² reflex belongs outside the surface, never inside it.

3g above the surface

Above the surface there is nothing left to enclose, so g simply obeys the inverse square measured from the centre: g_h = g(R/(R + h))². Expanding that for h ≪ R gives the familiar g_h ≈ g(1 − 2h/R). The 2 comes from the square, and the expression is the first two terms of a series, not an identity — it has an expiry date.

Compare the two directions from the surface. Rise a height h and g falls by roughly 2h/R; descend the same distance and it falls by only d/R. Near the surface, going up costs exactly twice as much as going down.

Figure. The dashed line is the tangent to the true curve at h = 0, which is exactly what a first-order expansion is. The two agree while h is a percent or two of R and then separate fast: by h = R/2 the straight line has run into the axis while the real g is still 0.44 of its surface value. The approximation always under-reads, never over-reads.

Up half a radius, and down half a radius

A satellite orbits at height h = R/2 above the Earth's surface. Find g there as a fraction of the surface value, and compare it with g at depth d = R/2.

  • Distance from the centre: r = R + R/23R/2
  • g_h = g(R/r)² = g(2/3)²0.444 g
  • Linear form g(1 − 2h/R) at h = R/20 — nonsense
  • At depth R/2: g_d = g(1 − d/R)0.5 g

Pro tip. The linear form is within about 1% up to h ≈ 350 km — it is still worth 1.2% of error at the space station's 400 km — and it is 100% wrong at h = R/2, where it predicts g = 0 instead of 0.44 g. The moment h is a noticeable fraction of R, go back to g(R/r)².

At a height equal to the Earth's radius above the surface, g becomes
  1. g/2
  2. g/4
  3. Zero, from the linear approximation

r = R + R = 2R, so g(R/2R)² = g/4. The third option is what the linear approximation is wrongly believed to return. Push g(1 − 2h/R) to h = R and it gives −g, a gravitational field pointing away from the Earth — the sign that the expansion has been taken far outside the h ≪ R it was derived for.

4Rotation and the g you actually measure

A weighing scale on the ground sits in a rotating frame. At latitude λ the ground travels a circle of radius R cos λ, so part of the true gravitational pull is spent supplying that circular motion and the scale reads less: g_eff = g − Rω²cos²λ.

The two cosines come from different places, and that is the whole subtlety. One is the radius of the circle you are carried round; the other is the projection of the resulting centripetal direction onto your local vertical. Hence cos²λ, not cos λ — the correction is largest at the equator and exactly zero at the poles, where you are not going round anything.

Figure. Because it is cos² and not cos, the correction is almost flat across the tropics — Mumbai at 19° keeps 89% of the full equatorial reduction — and then falls away fastest at 45°, reaching exactly zero at the poles. Plotted for ω = 7.27 × 10⁻⁵ rad s⁻¹ and R = 6.4 × 10⁶ m, so the left-hand end is 0.034 m s⁻².

Where the two cosines come from

  1. The radius of your circleAt latitude λ you are carried round a circle of radius R cos λ about the Earth's axis, not a circle of radius R.
  2. What that circle demandsIt needs a centripetal acceleration ω²R cos λ directed at the axis — which is not the same direction as the pull towards the centre, except at the equator.
  3. Project onto the verticalOnly the component along your local vertical shows up in the scale reading, and that costs a second cos λ. The leftover sideways part is real too: it tilts a plumb line by a few arcminutes at mid-latitudes.

How fast would the Earth have to spin?

Find the present rotational correction to g at the equator, and the spin rate at which a body at the equator would become weightless. Take R = 6.4 × 10⁶ m, g = 9.8 m s⁻².

  • Now: Rω² = 6.4×10⁶ × (7.27×10⁻⁵)²0.034 m s⁻²
  • Weightless needs Rω′² = g, so ω′ = √(g/R)1.24 × 10⁻³ rad s⁻¹
  • T′ = 2π/ω′5.08 × 10³ s ≈ 85 min
  • ω′/ω — how much faster than today≈ 17 ×

Pro tip. That 85-minute day is not a coincidence: ω′ = √(g/R) is exactly the angular velocity of a satellite skimming the surface, so a weightless equator simply means the ground is in orbit. Meanwhile 0.034 m s⁻² is only 0.35% of g. The measured pole-to-equator gap is about 0.052 m s⁻²; rotation supplies two-thirds of it and the Earth's equatorial bulge the rest.

The reduction in effective g caused by the Earth's rotation varies with latitude λ as
  1. cos λ
  2. cos²λ
  3. sin²λ

One cos λ sets the radius R cos λ of the circle traced; a second appears when the centripetal acceleration, which points at the axis, is resolved along the local vertical. At the poles cos λ = 0 and there is no correction at all.

5Potential and potential energy

Gravitational potential is the work done per unit mass in bringing a test mass in from infinity: V = −GM/r, with the zero deliberately placed at infinity rather than at the surface. It is negative everywhere because gravity does the work for you on the way in, so you must repay it to get back out. The energy of a pair of masses follows the same shape: U = −Gm₁m₂/r.

Field and potential are two views of the same thing, tied together by g = −dV/dr. Read that backwards and it says a region of constant V has zero field — which is exactly the inside of a spherical shell, where g = 0 but V holds its surface value −GM/R and does not drop to zero.

Figure. The whole curve lies below the dashed zero line and climbs towards it, never reaching it at any finite r. Its steepness is the field: the slope dV/dr at the surface is GM/R², which is g. A −1/r curve flattens far more slowly than the −1/r² field does, which is why potential still matters at distances where the field has become negligible.

Reading the minus signs

  1. Zero is at infinityEvery value of V and U is measured against a body infinitely far away and at rest. That choice, not the physics, is what makes them negative.
  2. Deeper means more negativeMoving in towards the mass lowers V; moving out raises it towards zero. 'Larger potential' means closer to zero, which is further out.
  3. Work is a differenceThe work you must supply is ΔU = U_final − U_initial, and near the surface that reduces to mgh only while h ≪ R.

Lifting a tonne to a height R

How much work is needed to raise a 1000 kg satellite from the Earth's surface to a height equal to one Earth radius? Take g = 9.8 m s⁻², R = 6.4 × 10⁶ m, and ignore the Earth's rotation.

  • U(R) = −GMm/R = −mgR = −1000 × 9.8 × 6.4×10⁶−6.27 × 10¹⁰ J
  • U(2R) = −GMm/2R−3.14 × 10¹⁰ J
  • W = ΔU = mgR/2+3.14 × 10¹⁰ J
  • Naive mgh with h = R would give mgR6.27 × 10¹⁰ J — twice too big

Pro tip. mgh is the straight-line approximation to a curve that bends away, so it always over-charges you — here by exactly a factor of two. The general result is worth carrying: lifting from R to nR costs mgR(1 − 1/n).

Inside a hollow uniform spherical shell of mass M and radius R the gravitational field is zero. The potential there is
  1. Also zero, since g = −dV/dr and g = 0
  2. Constant at −GM/R, the same as on the surface
  3. Constant at −3GM/2R

Zero field means V has zero gradient, so V is constant — not that it is zero. Its constant value is whatever it is at the surface, −GM/R. The third option is the centre of a solid sphere, a different body.

6Circular orbits: speed and period

A circular orbit is free fall that keeps missing. Gravity is the only force acting and it is exactly the centripetal force required, so GMm/r² = mv²/r, giving v_o = √(GM/r) and T = 2π√(r³/GM). Both depend on the orbital radius alone — the satellite's own mass cancels out, which is why a loose bolt and a space station in the same orbit drift along side by side.

Notice the direction of the dependence. A larger orbit is a slower orbit, v falling as 1/√r while T grows as √(r³). This is the opposite of the intuition that a higher orbit is a 'faster' one, and it is the single most reliable trap in the chapter.

Figure. Circular-orbit speed falls as 1/√r. The force is radial and the velocity tangential — perpendicular — so gravity turns the path without changing speed; the graph carries the r-dependence the undrawable circle would hide.

Setting up any orbit problem

  1. One force, one jobGravity supplies the entire centripetal requirement: GMm/r² = mv²/r. There is no second force to balance and nothing 'flinging the satellite outwards'.
  2. Measure r from the centrer = R + h, never h alone. This is the commonest arithmetic slip in the whole topic.
  3. Trade GM for gR²Whenever the surface g of the planet is known, substituting GM = gR² removes both G and M and keeps the numbers small.

From a skimming orbit to geostationary

Find the speed and period of a satellite circling just above the Earth's surface, then the radius of the orbit whose period is 24 hours. Take g = 9.8 m s⁻², R = 6.4 × 10⁶ m.

  • v_o = √(GM/R) = √(gR) = √(9.8 × 6.4×10⁶)7.92 × 10³ m s⁻¹
  • T = 2πR/v_o5.08 × 10³ s ≈ 85 min
  • r = (gR²T²/4π²)^⅓ with T = 86 400 s4.23 × 10⁷ m = 6.6 R
  • Check by ratio: (86 400/5077)² against 6.62³290 either way

Pro tip. The geostationary radius is 6.6 R, so the satellite hangs about 3.6 × 10⁴ km above the ground — five and a half Earth radii of empty space. The formula gives the radius but not the other two conditions the orbit must meet: it has to lie in the equatorial plane and run eastwards, or the satellite will not stay over one spot.

A satellite is transferred from a circular orbit of radius r to one of radius 2r. Its orbital speed
  1. Doubles
  2. Falls by a factor of √2
  3. Is unchanged, since the mass has not changed

v_o = √(GM/r) falls as 1/√r, so doubling the radius divides the speed by √2. Higher orbits are slower orbits, even though getting to them costs energy.

7Energy of a satellite

In a circular orbit K = ½mv_o² = GMm/2r while U = −GMm/r, so the total is E = −GMm/2r. Three statements fall out together and are best memorised as one line: E = −K, E = U/2, and E is negative — negative meaning bound. The binding energy, the extra energy needed to just barely escape from that orbit, is +GMm/2r.

Raising a satellite makes E less negative, which costs energy, and yet K falls while it happens. Fire the engine forwards and the satellite ends up in a higher and slower orbit. Total energy and speed move in opposite directions here, and examiners know it.

Figure. Three curves of the same 1/r shape. K sits above the dashed zero line, U twice as far below it, and E halfway between U and that line — so E is always the mirror image of K in it, which is the statement E = −K. All three climb towards zero as r grows: a distant orbit is a weakly bound one, and reaching E = 0 is escape.

The energy books for a one-tonne satellite

A 1000 kg satellite is in a circular orbit skimming the Earth's surface (r ≈ R = 6.4 × 10⁶ m, g = 9.8 m s⁻²). Find its potential, kinetic and total energy, and its binding energy.

  • U = −GMm/R = −mgR = −1000 × 9.8 × 6.4×10⁶−6.27 × 10¹⁰ J
  • K = ½mv_o² = ½mgR+3.14 × 10¹⁰ J
  • E = U + K = −GMm/2R−3.14 × 10¹⁰ J
  • Binding energy = 0 − E+3.14 × 10¹⁰ J

Pro tip. Look at the last two rows: for a surface-skimming orbit, the energy needed to put the satellite there from rest on the ground and the energy needed to then send it away for good are the same number. Getting into orbit really is halfway to leaving altogether — a useful sanity check whenever an energy answer comes out wildly asymmetric.

A satellite in a circular orbit has kinetic energy K. Its total mechanical energy is
  1. −K
  2. +K
  3. −2K

U = −2K for a circular orbit, so E = U + K = −K. The third option is U itself, and choosing it is the standard way to lose the mark.

8Escape velocity

Escaping means reaching infinity with nothing left over: ½mv_e² − GMm/R = 0, so v_e = √(2GM/R) = √(2gR). For the Earth that is 11.2 km s⁻¹, exactly √2 times the 7.9 km s⁻¹ needed to orbit at the surface.

Three things v_e does not depend on: the mass of the escaping body, the direction it is fired in (energy is a scalar — any direction that misses the ground will do), and the path it happens to take. It depends only on the mass and the radius of the body being left behind, which is why every planet and moon has its own fixed number.

Figure. At exactly v_e the speed decays as 1/√r and reaches zero only at infinity — the body slows forever and never turns round. Fired at 80% of v_e it stops dead at r = 2.8R, a height of just 1.8 R. Losing a fifth of the launch speed costs you the entire journey, which is the sense in which escape speed is a threshold rather than a target.

The energy argument in three lines

  1. Write the total energy½mv² − GMm/r is conserved for a body moving freely under gravity alone.
  2. Set the far end to zero'Just escapes' means v → 0 as r → ∞, and both terms vanish there — so the total energy is exactly zero throughout.
  3. Solve at the launch point½mv_e² = GMm/R gives v_e = √(2GM/R), and m has cancelled before you ever put a number in.

Why the Moon has no air

Compare the escape speeds of the Earth (g = 9.8 m s⁻², R = 6.4 × 10⁶ m) and the Moon (g = 1.62 m s⁻², R = 1.74 × 10⁶ m) with the r.m.s. speed of nitrogen molecules at 300 K.

  • Earth: v_e = √(2gR) = √(2 × 9.8 × 6.4×10⁶)1.12 × 10⁴ m s⁻¹
  • Moon: v_e = √(2 × 1.62 × 1.74×10⁶)2.37 × 10³ m s⁻¹
  • Nitrogen at 300 K: v_rms = √(3 × 8.31 × 300 / 0.028)5.2 × 10² m s⁻¹
  • v_e / v_rms, Earth against Moon22 against 4.6

Pro tip. A body holds on to a gas only while its escape speed is roughly six times the molecular r.m.s. speed, because the fast tail of the Maxwell distribution leaks away over geological time. The Earth clears that bar by a factor of nearly four; the Moon misses it, and has no atmosphere. Same physics, one ratio, two very different worlds.

A projectile is fired from the Earth's surface at exactly the escape speed, but at 45° to the vertical rather than straight up. Ignoring air resistance and the ground, it will
  1. Escape, exactly as a vertical launch would
  2. Fall back, since only the vertical component counts
  3. Escape only if it is fired eastwards

The condition is on total energy, which is ½mv² regardless of direction, so the angle never enters. Direction matters for where the body goes and whether it clears the ground, not for whether it is bound.

9Kepler's laws

Kepler's three laws were the observational summary that Newton's inverse square law later explained. First: each planet moves on an ellipse with the Sun at one focus — at a focus, not at the centre. Second: the radius vector sweeps out equal areas in equal times, so a planet is fastest at perihelion and slowest at aphelion. Third: T² = 4π²a³/GM, with a the semi-major axis, which for a circle is just the radius.

The second law is angular momentum conservation wearing different clothes, and it gives the familiar v_p r_p = v_a r_a — but only at perihelion and aphelion, where the velocity happens to be perpendicular to the radius. Everywhere else the conserved quantity is vr sin θ and the shortcut does not apply.

Figure. Real data for Mercury, Venus, Earth and Mars, plotted as T² against a³ rather than T against a. The four points are collinear to three decimal places and the line passes through the origin — which is the whole content of the third law, and the reason plotting the raw T against a would have shown nothing but a curve. The slope is 1 in these units by construction.

The three laws and what they really are
LawStatementThe physics underneath
FirstAn ellipse with the Sun at one focusThe closed-orbit shape peculiar to a 1/r² force
SecondEqual areas swept in equal timesAngular momentum conserved: the force is central
ThirdT² ∝ a³GMm/r² = mω²r, rearranged

Halley's comet

Halley's comet has a period of 76 years and comes within 0.586 AU of the Sun. Find its semi-major axis, its greatest distance, and the ratio of its fastest speed to its slowest.

  • In AU and years, T² = a³, so a = 76^(2/3)17.9 AU
  • Aphelion = 2a − r_p = 35.9 − 0.5935.3 AU
  • Equal areas: v_p/v_a = r_a/r_p = 35.3/0.5960

Pro tip. Working in astronomical units and years makes the constant in Kepler's third law exactly 1, so T² = a³ with no G, no solar mass and no powers of ten. Use the ratio form (T₁/T₂)² = (a₁/a₂)³ for any two bodies orbiting the same primary and the constant cancels regardless of units.

A satellite is moved to an orbit four times larger in radius. Its period becomes
  1. 4 times longer
  2. 8 times longer
  3. 16 times longer

T² ∝ r³, so the periods are in the ratio √(4³) = √64 = 8. Answering 4 forgets the cube and the square root; answering 16 squares the radius ratio instead of cubing it.

Notes

  • Newton's law of universal gravitation: Every particle attracts every other with a force F=\dfrac{Gm_1m_2}{r^2} directed along the line joining them, where G=6.67\times10^{-11}\text{ N m}^2/\text{kg}^2. The force is always attractive and obeys the inverse-square law.
  • Gravitational field and potential: The field is \vec{g}=-\dfrac{GM}{r^2}\hat{r} and the potential is V=-\dfrac{GM}{r} (taken zero at infinity). Potential energy of two masses is U=-\dfrac{Gm_1m_2}{r}, and \vec{g}=-\nabla V.
  • Variation of g: At height h, g_h=g\left(1-\dfrac{2h}{R}\right) for h\ll R; at depth d, g_d=g\left(1-\dfrac{d}{R}\right); and rotation reduces effective g at latitude \lambda by R\omega^2\cos^2\lambda.
  • Escape and orbital velocity: Escape speed from a body of mass M and radius R is v_e=\sqrt{\dfrac{2GM}{R}}; a circular orbit of radius r needs v_o=\sqrt{\dfrac{GM}{r}}, so v_e=\sqrt{2}\,v_o at the surface.
  • Kepler's laws: Planets move in ellipses with the Sun at one focus; the radius vector sweeps equal areas in equal times (conservation of angular momentum); and the square of the period is proportional to the cube of the semi-major axis, T^2\propto a^3.

Formulas

  • Force and field: F=\dfrac{Gm_1m_2}{r^2},\quad g_{surface}=\dfrac{GM}{R^2}
  • Potential and energy: V=-\dfrac{GM}{r},\quad U=-\dfrac{Gm_1m_2}{r}
  • Escape and orbital speed: v_e=\sqrt{\dfrac{2GM}{R}},\quad v_o=\sqrt{\dfrac{GM}{r}}
  • Satellite: T=2\pi\sqrt{\dfrac{r^3}{GM}},\quad E_{total}=-\dfrac{GMm}{2r}
  • Variation of g: g_h=g\left(1-\dfrac{2h}{R}\right),\quad g_d=g\left(1-\dfrac{d}{R}\right)
  • Kepler's third law: T^2=\dfrac{4\pi^2}{GM}a^3

Exam traps & shortcuts

  • For a satellite, total energy =-K=\tfrac12 U: it is negative, its magnitude equals the kinetic energy, and it is half the potential energy - handy for binding-energy questions.
  • Escape speed is \sqrt{2} times orbital speed at the surface, so v_e=\sqrt{2}\,v_o\approx11.2\text{ km/s} for Earth; memorise this to skip a full derivation.
  • Use Kepler's third law as a ratio \left(\tfrac{T_1}{T_2}\right)^2=\left(\tfrac{a_1}{a_2}\right)^3 so G and M cancel and you avoid large-number arithmetic.

Reference tables

Everything here should be reconstructible from the concept above it. The right-hand column is where the marks actually go.

Formula sheet
QuantityRelationWatch for
ForceF = Gm₁m₂/r²Attractive, along the line of centres, equal on both
Surface fieldg = GM/R², so GM = gR²The substitution that removes G and M
Heightg_h = g(R/(R+h))² ≈ g(1 − 2h/R)Linear form only while h ≪ R
Depthg_d = g(1 − d/R)Uniform sphere only; real Earth rises at first
Rotationg_eff = g − Rω²cos²λCos squared, not cos; zero at the poles
PotentialV = −GM/r, U = −Gm₁m₂/rZero at infinity, not at the surface
Field from potentialg = −dV/drg = 0 means V is constant there, not that V is zero
Orbital speedv_o = √(GM/r)Falls as 1/√r — a higher orbit is slower
PeriodT = 2π√(r³/GM)r from the centre: r = R + h
Satellite energyE = −GMm/2r = −K = U/2Binding energy is +GMm/2r
Escape speedv_e = √(2GM/R) = √(2gR) = √2 v_oIndependent of mass and of direction
Kepler IIIT² = 4π²a³/GMExactly 1 in AU and years — but only for the Sun

For a solid sphere of mass M and radius R with uniform density — the idealisation every exam question assumes unless it says otherwise.

Inside and outside a uniform sphere
QuantityOutside, r ≥ RInside, r ≤ R
Field gGM/r², falling as 1/r²GMr/R³, rising linearly from zero
Potential V−GM/r−GM(3R² − r²)/2R³
At the surface, r = RGM/R² and −GM/RThe same — the two forms agree there
At the centre, r = 0Does not applyg = 0, but V = −3GM/2R, its deepest value
Hollow shell insteadIdentical: GM/r² and −GM/rg = 0 everywhere, V constant at −GM/R

Recap

Read only this the night before.

Inverse square
F = Gm₁m₂/r², always attractive, and the two forces are equal whatever the masses. GM = gR² is the substitution that deletes G from the arithmetic.
Inside and out
Outside a sphere g ∝ 1/r² from the centre; inside a uniform one g ∝ r. Inside a hollow shell g = 0 but V = −GM/R, not zero.
Up and down
g(1 − 2h/R) going up, g(1 − d/R) going down — up costs twice as much. The linear form is for h ≪ R only; otherwise use g(R/r)².
Rotation
g_eff = g − Rω²cos²λ. Cos squared, 0.034 m s⁻² at the equator, nothing at the poles.
Signs
V = −GM/r and U = −GMm/r, zero at infinity, and most negative not at the surface but at the centre, where a uniform sphere reaches −3GM/2R. g = −dV/dr, so flat potential means no field.
Orbits
v_o = √(GM/r), T = 2π√(r³/GM), r measured from the centre. Higher orbit: slower satellite, larger total energy. Geostationary sits at 6.6 R.
The energy trio
E = −K = U/2. Binding energy GMm/2r, and escape speed is √2 times orbital speed — 11.2 km s⁻¹ against 7.9 km s⁻¹ for the Earth.
Kepler
Ellipse with the Sun at a focus; equal areas means angular momentum; T² ∝ a³. In AU and years, T² = a³ exactly.

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