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Gravitation and Fields

Year 1 / ASYear 2 / A-Level AQA, Edexcel, OCR, WJEC/Eduqas, CCEA

A-Level Physics gravitation revision: field concept, Newton's law of gravitation, g field strength, gravitational potential with derivations, orbits, satellites, Kepler's laws and escape velocity - AQA 7408 3.7.2, OCR A H556 5.4, Edexcel 9PH0 Topic 12.

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๐ŸŽฏ Learning Objectives

๐Ÿ“‹ Key Definitions and Core Concepts

Force field: A region where a body experiences a non-contact force; a gravitational field acts on mass, an electric field on charge.
Newton's law of gravitation: F = GMm/r^2 - the attractive force between two point masses, an inverse-square law with G = 6.67 ร— 10^-11 N m^2 kg^-2.
Gravitational field strength (g): Force per unit mass, g = F/m = GM/r^2, in N/kg; 9.81 N/kg at Earth's surface.
Gravitational potential (V): Work done per unit mass bringing a mass from infinity to a point: V = -GM/r, always negative, zero at infinity.
Equipotential surface: A surface of constant potential; no work is done moving along one, and field lines cross them at right angles.
Geostationary satellite: A satellite with period 24 hours orbiting above the equator in the same direction as Earth's rotation, so it stays above a fixed point.
Escape velocity: The minimum launch speed for a body to just reach infinity with zero speed: v_esc = โˆš(2GM/R).
Inverse-square law: A law where the quantity falls as 1/r^2; doubling the distance quarters the force (flux spreading over a sphere of area 4ฯ€r^2).

๐Ÿ“Œ Key Points

Newton's law: F = GMm/r^2 - always attractive, inverse-square; G = 6.67 ร— 10^-11 N m^2 kg^-2.
Field strength: g = F/m = GM/r^2 (N/kg); uniform near Earth's surface (9.81 N/kg).
Potential: V = -GM/r (always negative, zero at infinity); ฮ”W = mฮ”V; field strength = potential gradient, g = -dV/dr.
Circular orbits: GMm/r^2 = mv^2/r gives v = โˆš(GM/r) and T^2 = 4ฯ€^2r^3/GM (Kepler: T^2 โˆ r^3).
Orbital kinetic energy = GMm/2r; total energy = -GMm/2r (negative - bound).
Escape velocity: v_esc = โˆš(2GM/R); independent of the launched mass.

Fields and Newton's law of gravitation

A force field is a region in which a body experiences a non-contact force - a useful bookkeeping idea that lets us assign a value (field strength) to every point in space (AQA 7408 3.7.1). Gravity is always attractive and acts on mass (AQA 7408 3.7.2.1; OCR A H556 5.4; Edexcel 9PH0 Topic 12).

Newton's law of gravitation: F = GMm/r^2 - the force between two point (or spherically symmetric) masses is proportional to each mass and to the inverse square of their separation. G = 6.67 ร— 10^-11 N m^2 kg^-2. Why inverse square? The field lines spread out radially, crossing spheres of area 4ฯ€r^2 - the same 'flux' crosses a sphere twice the radius, spread over four times the area, so the force per unit mass falls as 1/r^2. The same geometry underlies Coulomb's law and the intensity of light - a favourite comparison question.

Derivation of field strength: field strength is force per unit mass, g = F/m. Substitute Newton's law: g = GMm/r^2 รท m = GM/r^2 - independent of the test mass m, which is why all objects fall with the same acceleration in a vacuum. At Earth's surface (M = 5.97 ร— 10^24 kg, R = 6.37 ร— 10^6 m): g = 6.67 ร— 10^-11 ร— 5.97 ร— 10^24/(6.37 ร— 10^6)^2 = 9.81 N/kg. Higher altitude: g falls as 1/r^2 from the centre - at height h, use r = R + h.

Worked example: g at satellite height

Find g at the altitude of the ISS, 400 km above Earth's surface (M = 5.97 ร— 10^24 kg, R = 6.37 ร— 10^6 m).

Line 1: r = R + h = 6.37 ร— 10^6 + 4.0 ร— 10^5 = 6.77 ร— 10^6 m (M1: distance from the centre).

Line 2: g = GM/r^2 = (6.67 ร— 10^-11 ร— 5.97 ร— 10^24)/(6.77 ร— 10^6)^2 (M1 A1).

Line 3: g = 3.98 ร— 10^14/4.58 ร— 10^13 = 8.7 N/kg (A1) - only ~11% less than the surface value; astronauts float because they are in free fall, not because gravity is absent.

Gravitational potential and potential energy

Gravitational potential at a point is the work done per unit mass bringing a small mass from infinity to that point: V = -GM/r (AQA 7408 3.7.2.3). Negative because gravity attracts - you do negative work (the field does the work) moving a mass in from infinity; V = 0 at infinity, the zero of potential by convention. Gravitational potential energy of a mass m at that point: E_p = mV = -GMm/r.

Derivation of V = -GM/r: the work done moving mass m from radius r_1 to r_2 against the force F = GMm/r^2 is W = โˆซF dr = โˆซGMm/r^2 dr from r_1 to r_2 = GMm(1/r_1 - 1/r_2). Bringing the mass from infinity (r_1 = โˆž) to r (r_2 = r): W = -GMm/r - the potential energy. Per unit mass: V = -GM/r.

Field strength is the potential gradient: g = -dV/dr - the field points down the potential 'slope' (from high to low potential, i.e. towards the mass where V is more negative). Graphically, V against r for a point mass is a curve rising from -GM/r at small r towards zero; the gradient at any r gives -g. Moving between two points: ฮ”W = mฮ”V - work done equals mass times the change in potential. Equipotential surfaces are spheres of constant V: moving along one does no work (ฮ”V = 0), and field lines meet them at right angles - the two facts tested in diagram questions.

Worked example: work done lifting a satellite

Find the work done moving a 1000 kg satellite from Earth's surface to a 400 km orbit (M = 5.97 ร— 10^24 kg, R = 6.37 ร— 10^6 m).

Line 1: V_surface = -GM/R = -(6.67 ร— 10^-11 ร— 5.97 ร— 10^24)/6.37 ร— 10^6 = -6.25 ร— 10^7 J/kg (M1 A1).

Line 2: V_orbit = -GM/(R + h) = -3.98 ร— 10^14/6.77 ร— 10^6 = -5.88 ร— 10^7 J/kg (A1).

Line 3: ฮ”V = -5.88 ร— 10^7 - (-6.25 ร— 10^7) = +3.7 ร— 10^6 J/kg (M1: potential increases, less negative).

Line 4: W = mฮ”V = 1000 ร— 3.7 ร— 10^6 = 3.7 ร— 10^9 J (A1) - the minimum energy input (no kinetic energy included).

Orbits, satellites and Kepler's laws

For a circular orbit, gravity supplies the centripetal force (AQA 7408 3.7.2.4; OCR A H556 5.2/5.4):

Derivation of orbital speed: GMm/r^2 = mv^2/r. Cancel m and one r: v^2 = GM/r, so v = โˆš(GM/r) - orbital speed falls with orbit radius (outer satellites move slower). Orbital angular speed: v = ฯ‰r gives ฯ‰ = โˆš(GM/r^3).

Derivation of Kepler's third law: period T = 2ฯ€r/v = 2ฯ€r/โˆš(GM/r) = 2ฯ€โˆš(r^3/GM). Square: T^2 = 4ฯ€^2r^3/GM - T^2 โˆ r^3, so a log-log or T^2 against r^3 plot of planetary data gives a straight line - how Kepler's law is verified and G or the central mass found. The constant T^2/r^3 = 4ฯ€^2/GM is the same for all satellites of one central body.

Orbital energy: KE = ยฝmv^2 = GMm/2r (substituting v^2 = GM/r); PE = -GMm/r. Total energy = KE + PE = -GMm/2r - negative, meaning the satellite is bound to the planet; lower orbits are more strongly bound (more negative total energy, but faster and higher KE).

Geostationary satellites: period 24 hours, above the equator, same rotation direction - fixed above one point on the surface for communications. Derivation of the orbit radius: T^2 = 4ฯ€^2r^3/GM with T = 24 ร— 3600 = 86,400 s gives r = (GMT^2/4ฯ€^2)^(1/3) โ‰ˆ 4.23 ร— 10^7 m - about 36,000 km altitude (6.6 Earth radii). All geostationary satellites share this radius - a standard one-mark fact. Polar orbits (over the poles) scan the whole surface - used for weather and mapping.

Worked example: geostationary radius

Find the orbital radius of a geostationary satellite (M = 5.97 ร— 10^24 kg, T = 86,400 s).

Line 1: r^3 = GMT^2/4ฯ€^2 (M1: from T^2 = 4ฯ€^2r^3/GM).

Line 2: r^3 = (6.67 ร— 10^-11 ร— 5.97 ร— 10^24 ร— 86400^2)/(4ฯ€^2) = 7.54 ร— 10^22 m^3 (M1 A1).

Line 3: r = 4.23 ร— 10^7 m (A1) - altitude 4.23 ร— 10^7 - 6.37 ร— 10^6 โ‰ˆ 3.6 ร— 10^7 m above the surface.

Escape velocity and orbital analysis

Escape velocity is the minimum launch speed for a body to just reach infinity with zero speed (all KE spent against gravity).

Derivation: energy conservation. Launch from a planet's surface (radius R) with speed v: KE + PE = ยฝmv^2 - GMm/R. At infinity: KE = 0 and PE = 0. So ยฝmv^2 - GMm/R = 0, giving v_esc = โˆš(2GM/R) - independent of the launched mass. For Earth: v_esc = โˆš(2 ร— 6.67 ร— 10^-11 ร— 5.97 ร— 10^24/6.37 ร— 10^6) = 11.2 km/s. Comparison: v_esc = โˆš2 ร— v_orbit at the same radius (since v_orbit = โˆš(GM/r)) - a favourite link. Note also that escape velocity is independent of launch direction in the idealised model (energy, not vector direction, decides) - though launching eastward from the equator borrows Earth's rotation (~465 m/s), a small practical gain rockets exploit.

Energy changes in orbit: a satellite in a decaying orbit (drag from the thin upper atmosphere) loses total energy, so it moves to a lower orbit - where its speed is higher (v = โˆš(GM/r)) even though it lost energy. The apparent paradox resolves through the PE: the drop in PE (-GMm/r becomes more negative) exceeds the gain in KE (GMm/2r), with the difference dissipated as heat by drag. A satellite boosted to a higher orbit by a rocket burn gains PE and loses speed - the standard explanation question.

Analysing orbital data: planetary periods and radii: plot T^2 against r^3 - straight line through the origin with gradient 4ฯ€^2/GM, so the central mass M = 4ฯ€^2/(G ร— gradient). Satellite speed data against radius: v^2 against 1/r gives a straight line of gradient GM. This is how the mass of the Sun (from planetary data) or of a planet (from its moons) is found. Uncertainty practice: orbital radii and periods are large, well-measured quantities; the derived mass uncertainty is dominated by the scatter of the line fit and by G's precision; quote the percentage difference of the derived mass from the accepted value in the conclusion.

Worked example: escape velocity and orbital link

A planet has M = 6.4 ร— 10^23 kg and R = 3.4 ร— 10^6 m. Find v_esc and the orbital speed at the surface.

Line 1: v_esc = โˆš(2GM/R) = โˆš(2 ร— 6.67 ร— 10^-11 ร— 6.4 ร— 10^23/3.4 ร— 10^6) (M1 A1).

Line 2: v_esc = โˆš(2.51 ร— 10^7) = 5.0 km/s (A1).

Line 3: Orbital speed at the surface: v = โˆš(GM/R) = โˆš(1.25 ร— 10^7) = 3.5 km/s (M1 A1).

Line 4: Check: v_esc = โˆš2 ร— 3.5 = 5.0 km/s - consistent (A1).

Comparing gravitational and electric fields

The gravitational and electric field topics are deliberately parallel - exam boards set six-mark synthesis questions on the comparison, so learn the pairs (AQA 7408 3.7.1-3.7.3; OCR A H556 5.4/6.2; Edexcel 9PH0 Topics 7/12):

QuantityGravitationalElectric
SourceMass (always positive)Charge (ยฑ)
Force lawF = GMm/r^2F = q1q2/(4ฯ€ฮต0r^2)
Field strengthg = GM/r^2 (N/kg)E = Q/(4ฯ€ฮต0r^2) (V/m or N/C)
PotentialV = -GM/r (always negative)V = Q/(4ฯ€ฮต0r) (either sign)
Gradient relationg = -dV/drE = -dV/dr
EquipotentialsSpheres; no work along them; field โŠฅ to themSame geometry
AttractionAlways attractiveAttract or repel
ShieldingImpossibleConductors shield electric fields
Relative strengthWeak between particlesVastly stronger between particles (~10^36 times for two protons)

The pattern: every quantity maps one-to-one (source, force, field strength, potential, gradient, equipotentials), and the differences are exactly two - the sign of the source (making electric forces either attractive or repulsive, and electric potential either sign) and shielding. Both forces are inverse-square because field lines from a point source spread over spheres of area 4ฯ€r^2 - the same geometry argument serves both. Uniform versions also pair: a uniform gravitational field near Earth's surface (g constant) and a uniform electric field between parallel plates (E = V/d) - both give parabolic trajectories for projectiles and charged particles respectively, the deepest symmetry of the pair.

Worked example: relative strength

Compare the gravitational and electric forces between two protons 1.0 ร— 10^-10 m apart.

Line 1: Electric: F = e^2/(4ฯ€ฮต0r^2) = (1.60 ร— 10^-19)^2/(4ฯ€ ร— 8.85 ร— 10^-12 ร— (1.0 ร— 10^-10)^2) = 2.3 ร— 10^-8 N (M1 A1).

Line 2: Gravitational: F = Gm_p^2/r^2 = 6.67 ร— 10^-11 ร— (1.67 ร— 10^-27)^2/(1.0 ร— 10^-10)^2 = 1.9 ร— 10^-44 N (M1 A1).

Line 3: Ratio โ‰ˆ 1.2 ร— 10^36 - the electric force is enormously stronger; gravity only dominates for astronomical bodies because they are electrically neutral in bulk (A1: interpretation).

๐Ÿ’ก Worked Example

Exam-style: A satellite orbits Earth in a circular orbit of radius 8.0 ร— 10^6 m. Calculate its orbital speed and period. (M = 5.97 ร— 10^24 kg, G = 6.67 ร— 10^-11 N m^2 kg^-2) (AQA 7408-style, 6 marks)
Mark-scheme logic: Gravity provides the centripetal force: GMm/r^2 = mv^2/r (M1: force equation set equal to centripetal). Cancel m and r: v^2 = GM/r (M1 A1: algebra to v^2 = GM/r). v = โˆš(6.67 ร— 10^-11 ร— 5.97 ร— 10^24/8.0 ร— 10^6) = โˆš(4.98 ร— 10^7) = 7.1 ร— 10^3 m/s (A1). Period: T = 2ฯ€r/v = 2ฯ€ ร— 8.0 ร— 10^6/7.1 ร— 10^3 (M1) = 7.1 ร— 10^3 s โ‰ˆ 1.97 hours (A1).

โ“ Practice Questions & Mark Schemes

Calculate g at the altitude of the ISS, 400 km above Earth's surface (M = 5.97 ร— 10^24 kg, R = 6.37 ร— 10^6 m).
Answer: r = R + h = 6.77 ร— 10^6 m (M1: distance from centre, not altitude). g = GM/r^2 = 3.98 ร— 10^14/4.58 ร— 10^13 (M1 A1) = 8.7 N/kg (A1). Astronauts float due to free fall, not zero gravity.
Derive escape velocity from a planet of mass M and radius R, and calculate it for Earth.
Answer: Energy conservation: ยฝmv^2 - GMm/R = 0 at infinity (KE = 0, PE = 0) (M1: both energies set up). v^2 = 2GM/R, so v_esc = โˆš(2GM/R) (A1). Earth: โˆš(2 ร— 6.67 ร— 10^-11 ร— 5.97 ร— 10^24/6.37 ร— 10^6) = 11.2 km/s (A1).
Find the orbital radius of a geostationary satellite (T = 86,400 s, M = 5.97 ร— 10^24 kg) and state why it must orbit above the equator.
Answer: T^2 = 4ฯ€^2r^3/GM, so r^3 = GMT^2/4ฯ€^2 (M1) = 7.54 ร— 10^22 m^3 (M1 A1), r = 4.23 ร— 10^7 m (A1). Above the equator and moving with Earth's rotation so it stays fixed above one point - required for communications (A1).
A 1000 kg satellite is moved from Earth's surface to a 400 km orbit. Calculate the minimum work done (V_surface = -6.25 ร— 10^7 J/kg, V_orbit = -5.88 ร— 10^7 J/kg).
Answer: ฮ”V = -5.88 ร— 10^7 - (-6.25 ร— 10^7) = 3.7 ร— 10^6 J/kg (M1 A1: potential change from the two values). W = mฮ”V = 1000 ร— 3.7 ร— 10^6 = 3.7 ร— 10^9 J (A1). This excludes the kinetic energy of orbit - a full launch needs more.
Show that the orbital speed of a satellite is inversely proportional to โˆšr, and explain why outer planets move more slowly.
Answer: GMm/r^2 = mv^2/r gives v^2 = GM/r (M1 A1: centripetal argument), so v โˆ 1/โˆšr (A1). Outer planets are further from the central mass; gravity is weaker (inverse square) so less centripetal force is needed - slower speeds, longer periods (T^2 โˆ r^3) (A1).
Two planets orbit the same star: planet A at r = 1.0 ร— 10^11 m with T = 3.2 ร— 10^7 s. Find the star's mass.
Answer: T^2 = 4ฯ€^2r^3/GM, so M = 4ฯ€^2r^3/(GT^2) (M1: rearrangement). M = 4ฯ€^2 ร— (1.0 ร— 10^11)^3/(6.67 ร— 10^-11 ร— (3.2 ร— 10^7)^2) (M1 A1). M = 3.95 ร— 10^34/6.83 ร— 10^4 = 5.8 ร— 10^29 kg (A1).

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