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IB Physics SL + HL · Theme D.1 · by Ahmed Gomaa

Gravitational Fields Field Guide

Pull two planets apart, walk a test mass away from a planet, draw the field lines of two masses, find where the pulls cancel, sweep equal areas on an ellipse, fire Newton’s cannon, compare orbits, float in a space station, climb out of a potential well, read the field from a V–r graph, move along equipotentials, slow a satellite with air and launch a probe to infinity.

Force, field strength Velocity, kinetic energy Energy, work Potential, field lines
Part 1Gravity and its fieldSections 01–04

01Two bodies pull each other: F = GMm/r²

← Back to the notes: Newton’s law of gravitation

Every two masses attract. The force on each body has the same size (Newton’s third law), F = GMm/r², with r measured between the centres. Double r and F falls to a quarter. Change M and both arrows change together. The small body accelerates more only because its mass is smaller.

force on each body—
acceleration of m—
acceleration of M—
F ÷ F(r = 3.8 × 10⁸ m)—

02Field strength: the force per unit mass

← Back to the notes: Gravitational field strength

Gravitational field strength is the force per unit mass experienced by a small point mass at that point. Walk the test mass away from the planet: g = GM/r² falls as 1/r². At r = 2R it is a quarter of the surface value. Choose another planet to see how M and R both matter.

r—
g = GM/r²—
g ÷ g(surface)—

03Field lines: always towards the mass

← Back to the notes: Field lines

Field lines show the direction of the force on a small mass. They point towards masses, never cross, and are closer together where the field is stronger. Around one sphere they are radial. With two masses the lines bend and there is a neutral point where none pass, closer to the smaller mass. Close to the surface of a planet the field is nearly uniform.

what to notice—

04Where the pulls cancel

← Back to the notes: Where the net field is zero

On the line between two masses each one pulls a test mass towards itself. The net field is zero where the pulls have the same size: GM/x² = Gm/(d − x)², so x/(d − x) = √(M/m). Move the probe and watch the two arrows. The zero point is always closer to the smaller mass. For the Earth and the Moon (M/m = 81) it is at 0.90 d.

field of M—
field of m—
net field—
zero point, x/d = √(M/m)/(1 + √(M/m))—
Part 2OrbitsSections 05–08

05Kepler’s first and second laws

← Back to the notes: Kepler’s three laws

A planet moves on an ellipse with the Sun at one focus (first law). The line from the Sun sweeps equal areas in equal times (second law): each shaded sector takes the same time, so the planet is fast near the Sun (short, wide sectors) and slow far away (long, thin ones). rPvP = rAvA.

r(A) ÷ r(P)—
speed at P ÷ speed at A—
speed now ÷ speed at A—

06Newton’s cannon: the total energy decides the path

← Back to the notes: Energy of an orbit

Fire a ball sideways from a mountain on the Earth (no air). The sign of its total energy ET = Ek + Ep decides the path. ET < 0: bound: it falls back to the ground, or moves in a circle (at the circle speed) or an ellipse, and we see it again. ET = 0 (at the escape speed for the mountain top): a parabola; it just escapes and never returns. ET > 0: a hyperbola; it escapes with speed to spare. Press “Show all five paths” to compare them.

launch speed—
total energy per kg, E_T—
path—
circle / escape speed here—

07Circular orbits: v = √(GM/r) and T² ∝ r³

← Back to the notes: Orbits: v = √(GM/r) and T² = 4π²r³/GM

Gravity provides the centripetal force: GMm/r² = mv²/r, so v = √(GM/r). With v = 2πr/T this gives T² = 4π²r³/(GM). Two satellites go round together: the outer one is slower and takes longer. Every satellite of the Earth sits on the same straight line of T² against r³, with gradient 4π²/GM.

v₁, T₁—
v₂, T₂—
T₂ ÷ T₁ and (r₂/r₁)^1.5—
T²/r³ (both)—

08Weightless, not without gravity

← Back to the notes: Weightlessness in orbit

In a space station 400 km up, g is still about 8.7 N kg⁻¹. The astronaut and the station fall around the Earth together, with the same acceleration, so the floor does not push on the astronaut: the scale reads zero and the astronaut feels weightless. Compare with standing on the ground, and with a lift falling freely.

g here—
weight of a 70 kg astronaut—
scale reading (normal force)—
Part 3 · HLPotential and energySections 09–13

09The potential well: why V is always negative

← Back to the notes: Why gravitational potential is always negative

Gravitational potential is the work done per unit mass in bringing a small mass from infinity to that point. Zero is at infinity. Gravity always attracts, so to take a mass from any point out to infinity we must do positive work on it: the mass starts below zero. V = −GM/r is negative everywhere and rises towards zero as r grows. Press “Bring it in from infinity”: gravity does the work, and the potential energy falls below zero.

V = −GM/r—
E_p = mV—
work needed to take it to infinity—

10Reading the field from a V–r graph

← Back to the notes: Field and potential: g = −ΔV/Δr

The field strength is minus the gradient of the V–r graph: g = −ΔV/Δr. Move the probe between a planet and its moon and watch the green tangent. Where the graph is steep the field is strong. At the top of the hump the tangent is horizontal: zero gradient, so the net field is zero, the same point as in section 04. The field always points “downhill”.

V—
gradient ΔV/Δx—
field g = −gradient—

11Equipotentials and the work done

← Back to the notes: Equipotential surfaces

The dashed circles are equipotentials drawn every 1 × 10⁷ J kg⁻¹. They cross the field lines at 90° and get further apart as the field weakens. Move a 100 kg probe from A to B. Work done against the field (by an external force) = mΔV. Work done by the field = −mΔV. Put A and B on the same equipotential: ΔV = 0, so no work is done.

V at A—
V at B—
work against the field, mΔV—
work done by the field—

12Energy of an orbit, and what drag does

← Back to the notes: Energy of an orbit

For a circular orbit Ek = GMm/2r, Ep = −GMm/r and the total ET = −GMm/2r. Press “Air resistance on”: drag takes energy, the total becomes more negative, so the orbit radius decreases and the speed increases. Ep falls twice as fast as Ek rises.

E_k (500 kg)—
E_p—
E_T—
orbital speed—

13Escape speed: a total energy of zero

← Back to the notes: Escape speed

Escape speed is the minimum speed a body must have at the surface to reach infinity, with no further energy supplied. It just escapes when its total energy is zero: ½mv² − GMm/R = 0, so vesc = √(2GM/R) = 11.2 km s⁻¹ for the Earth, whatever the mass. Launch below it and the probe stops and falls back.

total energy per kg—
highest point—
escape speed—

14Practice and self-check

← Back to the notes: Extra practice
Answers checked by calculation. Try each one before you open it.
1. Two moons of mass 5.0 × 10²⁴ kg and 2.0 × 10²² kg are 4.0 × 10⁸ m apart, centre to centre. Find the force between them.
F = GMm/r² = 6.67 × 10⁻¹¹ × 5.0 × 10²⁴ × 2.0 × 10²² / (4.0 × 10⁸)² = 4.2 × 10¹⁹ N, on each moon.
2. A planet has 4 times the Earth’s mass and twice its radius. Find g at its surface (Earth: 9.8 N kg⁻¹).
g = 9.8 × 4/2² = 9.8 N kg⁻¹: the same as on the Earth.
3. Find g at the height of the space station, 360 km above the Earth (GM = 4.0 × 10¹⁴ N m² kg⁻¹, R = 6.4 × 10⁶ m).
r = R + h = 6.76 × 10⁶ m; g = GM/r² = 8.8 N kg⁻¹. Remember to add R.
4. Mass M is 64 times mass m; their centres are 3.6 × 10⁸ m apart. How far from M is the net field zero?
x/(d − x) = √64 = 8, so 9x = 8d and x = 3.2 × 10⁸ m, closer to the small mass.
5. Show that the period of a satellite in a circular orbit of radius r is given by T² = 4π²r³/(GM).
Gravity provides the centripetal force: GMm/r² = mv²/r ✔; v = 2πr/T, so 4π²r²/T² = GM/r ✔; rearrange: T² = 4π²r³/(GM).
6. A satellite orbits at r = 7.0 × 10⁶ m. Find its speed and its period (GM = 4.0 × 10¹⁴ N m² kg⁻¹).
v = √(GM/r) = 7.6 × 10³ m s⁻¹; T = 2πr/v = 5.8 × 10³ s = 97 min.
7. Moon B orbits a planet at 1.5 times the radius of moon A, whose period is 2.0 days. Find the period of B.
T ∝ r^1.5: T_B = 2.0 × 1.5^1.5 = 3.7 days.
8. Explain why the gravitational potential near a planet is negative.
The potential is defined as zero at infinity ✔. Gravity is attractive, so positive work must be done on a mass to move it to infinity ✔: everywhere else the potential is less than zero.
9. A 250 kg probe is moved from r = 2R to r = 4R from the centre of the Earth. Find the work done against the field.
W = mΔV = 250 × (−GM/4R + GM/2R) = 250 × 1.56 × 10⁷ = 3.9 × 10⁹ J.
10. The potential at the surface of a planet is −5.0 × 10⁷ J kg⁻¹. Find the escape speed.
Total energy zero: ½v² + V = 0, so v = √(−2V) = √(1.0 × 10⁸) = 1.0 × 10⁴ m s⁻¹.
11. A 500 kg satellite orbits at r = 8.0 × 10⁶ m. Find its total energy. A small drag force acts: what happens to r and to v?
E_T = −GMm/2r = −1.25 × 10¹⁰ J. Drag lowers E_T, so r decreases and v = √(GM/r) increases.

Before the exam, can you…

  • state the definitions of gravitational field strength, gravitational potential and escape speed word for word?
  • use F = GMm/r² and g = GM/r² with r from the centre?
  • find where the net field is zero, from an equation and from a V–r graph?
  • state Kepler’s three laws with the words ellipse, focus, equal areas and cube?
  • derive T² = 4π²r³/(GM) and use it to find a mass or compare two orbits?
  • explain why V and E_p are always negative?
  • use W = mΔV, both as work against the field and as work done by the field?
  • derive the escape speed from energy and explain what drag does to an orbit?