Lesson 11 of 11 · 15 min
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Must-know facts
16 facts
- 1F = G m₁ m₂ / r², with r measured between centres; G = 6.67 × 10⁻¹¹ N m² kg⁻².
- 2g = G M_E / R_E² ≈ 9.8 m/s² and is independent of the mass of the falling body.
- 3g(h) = g R_E²/(R_E + h)² exactly; ≈ g(1 − 2h/R_E) only for h ≪ R_E.
- 4g(d) = g(1 − d/R_E) for a uniform earth; zero at the centre.
- 5g is largest at the surface and decreases both above and below it.
- 6Shell outside → acts as a point at its centre; point inside a shell → zero net pull.
- 7Kepler: ellipse with the sun at a focus; equal areas in equal times; T² ∝ a³.
- 8Law of areas = conservation of angular momentum; holds for any central force.
- 9v_P r_P = v_A r_A: fastest at perihelion.
- 10U = −G M m / r, zero at infinity; mgh is its near-surface approximation.
- 11Escape speed vₑ = √(2gR_E) ≈ 11.2 km/s; independent of the body's mass and launch direction.
- 12Orbital speed near the surface v₀ = √(gR_E) ≈ 7.9 km/s; vₑ = √2 v₀.
- 13Orbital speed v = √(G M_E / r) falls with r; period T ∝ r^(3/2).
- 14Near-surface orbit period ≈ 85 min.
- 15Satellite: K = GMm/2r, U = −GMm/r, E = −GMm/2r = −K.
- 16Negative total energy = bound orbit; zero or positive = escape.
Common traps
Where marks are lost
Putting the height above the surface into F = G M m / r².
Using g(1 − 2h/R_E) for a height like R_E/2.
Thinking g keeps increasing as you go down a mine, because you are closer to the centre.
Believing a heavier body needs a bigger escape speed.
Thinking astronauts float because there is no gravity in orbit.
Giving a satellite a positive total energy because it is moving.
Saying the law of areas proves the inverse-square law.
Treating G and g as the same kind of constant.
Formulas
13 to know
Law of gravitation
F = G m₁ m₂ / r²
r between centres; attractive.
Kepler's third law
T² = (4π² / G M) a³
M is the central body; a is the semi-major axis (radius for a circle).
Law of areas
ΔA/Δt = L / 2m = constant
At the ends of the orbit: v_P r_P = v_A r_A.
Cavendish balance
G M m L / d² = τθ
τ is the restoring torque per unit twist.
g at the surface
g = G M_E / R_E²
Gives M_E = g R_E² / G.
g at height h
g(h) = g R_E² / (R_E + h)² ≈ g (1 − 2h/R_E)
Approximation only for h ≪ R_E.
g at depth d
g(d) = g (1 − d/R_E)
Uniform earth; zero at the centre.
Potential energy
U = −G m₁ m₂ / r
Zero at infinity; add over all pairs for a system.
Gravitational potential
V = −G M / r
Potential energy per unit mass.
Escape speed
vₑ = √(2 G M / R) = √(2 g R)
≈ 11.2 km/s for the earth.
Orbital speed
v = √(G M_E / (R_E + h)); v₀ = √(g R_E)
v₀ ≈ 7.9 km/s just above the surface.
Orbital period
T = 2π (R_E + h)^(3/2) / √(G M_E); T₀ = 2π √(R_E / g)
T₀ ≈ 85 min.
Satellite energies
K = G M m / 2r, U = −G M m / r, E = −G M m / 2r
r = R_E + h; E = −K = U/2.
Key terms
13 terms
- Geocentric model
- A picture of the heavens with the earth at the centre.
- Heliocentric model
- A picture with the sun at the centre and the planets going round it.
- Ellipse
- A closed curve on which the distances to two fixed foci always add to the same total.
- Perihelion
- The point of a planet's orbit nearest the sun.
- Aphelion
- The point of a planet's orbit farthest from the sun.
- Semi-major axis
- Half of the longest diameter of an ellipse.
- Central force
- A force always directed along the line joining the body to a fixed centre.
- Gravitational constant (G)
- The universal constant in Newton's law, 6.67 × 10⁻¹¹ N m² kg⁻².
- Acceleration due to gravity (g)
- The acceleration of a freely falling body near a planet; about 9.8 m/s² at the earth's surface.
- Gravitational potential
- Gravitational potential energy per unit mass at a point.
- Escape speed
- The least launch speed with which a body can reach infinity.
- Satellite
- A body that revolves around a planet.
- Bound system
- A system with negative total energy, whose orbit stays closed.