Gravitational fields
Gravitational field strength, Newton's law of gravitation, g = GM/r², gravitational potential and potential energy, circular orbits, Kepler's third law from first principles, and geostationary satellites.
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In 30 seconds
- A gravitational field is a region where a mass feels a force. Field strength g = F/m (force per unit mass).
- Newton's law: F = GMm/r² between point masses; outside a uniform sphere, treat its mass as concentrated at the centre.
- Potential φ = −GM/r is the work done per unit mass bringing a small mass from infinity to that point. It is negative because gravity is attractive.
- Orbits: gravity provides the centripetal force: GMm/r² = mv²/r, so v² = GM/r and T² = (4π²/GM)r³.
By the end you can
- Understand the gravitational field and field lines, and define field strength g = F/m.
- Recall and use F = GMm/r² and g = GM/r².
- Define and use gravitational potential φ = −GM/r and potential energy EP = −GMm/r.
- Analyse circular orbits, including geostationary orbits, using gravity as the centripetal force.
1Field and force
Field strength
Gravitational field strength — the gravitational force per unit mass at a point: g = F/m.
Calculate g at the Earth's surface (M = 5.97 × 10²⁴ kg, R = 6.37 × 10⁶ m).
- g = GM/R² = 6.67 × 10⁻¹¹ × 5.97 × 10²⁴/(6.37 × 10⁶)² C1
- g = 9.81 N kg⁻¹ A1
2Potential
φ = −GM/r
Gravitational potential — the work done per unit mass in bringing a small test mass from infinity to the point.
- Why negative? Potential is zero at infinity, and work is done by the field as a mass falls in, so potential is lower (more negative) closer in.
- mgh only works where g is constant (near the surface). Over large distances use Δφ.
Find the energy needed to raise a 1000 kg satellite from the Earth's surface to a point at r = 2R.
- Δφ = GM/R − GM/(2R) = GM/(2R) = 3.13 × 10⁷ J kg⁻¹ C1 C1
- ΔE = mΔφ = 3.1 × 10¹⁰ J A1
3Orbits
Circular orbits
A satellite orbits at r = 7.0 × 10⁶ m. Find its speed and period.
- v = √(GM/r) = √(6.67 × 10⁻¹¹ × 5.97 × 10²⁴/7.0 × 10⁶) = 7.5 km s⁻¹ C1 A1
- T = 2πr/v = 5.8 × 10³ s (about 97 min) A1
Geostationary satellites
- Three conditions: period 24 hours, orbit above the equator, moving in the same direction as the Earth rotates (west to east). It stays above one point, so dishes don't need to track it.
Show that the radius of a geostationary orbit is about 4.2 × 10⁷ m.
- r³ = GMT²/(4π²) with T = 86 400 s C1
- r = (6.67 × 10⁻¹¹ × 5.97 × 10²⁴ × 86 400²/4π²)1/3 = 4.22 × 10⁷ m A1 (height ≈ 3.6 × 10⁷ m)
Test yourself — cover the answers first
Quick check
- Define gravitational field strength.
- Why is gravitational potential negative?
- How does g vary with r outside a planet?
- State the period of a geostationary satellite.
- Does the orbital speed depend on the satellite's mass?
Exam-style
- At what height above the surface is g a quarter of its surface value?
- Show that T² ∝ r³ for circular orbits.
- The Moon's mass is 7.35 × 10²² kg and radius 1.74 × 10⁶ m. Find g on its surface.
Show answers
- force per unit mass
- it is zero at infinity and work is done by the field as masses come together
- g ∝ 1/r²
- 24 hours
- no
- r = 2R, so h = R = 6.37 × 10⁶ m
- GMm/r² = m(2πr/T)²/r ⇒ T² = (4π²/GM)r³
- g = GM/R² = 1.62 N kg⁻¹
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