A-Level Physics — 8) Gravitational Fields (IP-Friendly Guide)
Download printable cheat-sheet (CC-BY 4.0)14 Jul 2025, 00:00 Z
TL;DR
Newton's inverse-square law is the only new “tool” in this topic; every other result (\(g\), \(\varphi\), \(U_G\), escape speed, orbit radius) is crafted by algebra and energy bookkeeping that you already know from mechanics. Nail those derivations once, and the WA1-to-A-Level questions collapse into four recurring templates.
1 Newton's law of gravitation
Isaac Newton modelled gravity as a mutual, attractive, central force:
\[ F = G \frac{m_1 m_2}{r^2}. \]
- Proportional to mass product: doubling either mass doubles the force.
- Inverse-square with separation: the force drops by \(4\) x when distance doubles — the geometry of spreading field lines over a sphere.
- Universal constant \(G\): \(6.67 \times 10^{-11} \space \pu{N.m^2.kg^{-2}}\), first measured by Cavendish in 1798.
1.1 IP exam cue
List all three features (“attractive”, “inverse-square”, “proportional to masses”) for a 2-mark definition: one IP tuition classic.
2 Gravitational field strength \(g\)
Field strength is force per unit mass: \(g = F/m\). Combining with Newton's law gives
\[ g = \frac{GM}{r^2}. \tag{1} \]
Near Earth's surface, \(r\) ≈ Earth's radius, so \(g ≈ 9.81 \space \pu{m.s-2}\) and is directionally “down”.
Parent insight: “Why is \(g\) 'constant'?” — because \(r\) changes by < 0.1 % across school-lab altitudes, giving < 0.3 % drift in \(g\).
3 Gravitational potential \(\varphi\)
Definition: work done per unit mass by an external agent in bringing a small test mass from infinity to the point.
For a point mass \(M\):
\[ \varphi = -\frac{GM}{r}. \tag{2} \]
The negative sign encodes that gravity is attractive; zero potential is set at infinity.
Gradient link: \(g = -\dfrac{\mathrm{d}\varphi}{\mathrm{d}r}\) — differentiating Eq. (2) regenerates Eq. (1).
4 Gravitational potential energy \(U_G\)
For two point masses \(M\) and \(m\):
\[ U_G = -\frac{GMm}{r}. \tag{3} \]
Think of \(U_G\) as the shared energy store of the pair; separating them to infinity requires positive work equal to \(|U_G|\).
5 Escape velocity
Set “initial kinetic energy + potential energy = 0 at infinity”:
\[ \frac12 m v_e^2 - \frac{GMm}{r} = 0 \quad \Rightarrow \quad v_e = \sqrt{\frac{2GM}{r}}. \tag{4} \]
At Earth's surface \(v_e ≈ 11.2 \space \pu{km.s-1}\) — 34 x the expressway speed limit!
6 Circular orbits & centripetal acceleration
Equate gravitational force to the required centripetal force \(m v^2 / r\):
\[ \frac{GMm}{r^2} = \frac{m v^2}{r} \quad \Rightarrow \quad v = \sqrt{\frac{GM}{r}}. \tag{5} \]
Key takeaway: orbital speed halves when radius quadruples — a fast elimination step in MCQs.
7 Geostationary satellites
A geostationary satellite has
- Orbital period = 24 h (synchronised with Earth's spin),
- Zero inclination & eccentricity (lies above the equator),
- Altitude ≈ 35 786 km.
Applications span weather monitoring, TV broadcast and VSAT internet.
7.1 Deriving the GEO radius
Set centripetal period \(T = 2 \pi r / v\) and combine with Eq. (5):
\[ r = \sqrt[3]{\frac{GMT^2}{4\pi^2}} ≈ 4.22 \times 10^4 \space \pu{km}. \tag{6} \]
8 Negative potential gradient shortcut
Many WA problems ask for \(g\) at a point off-axis or between bodies. Instead of re-drawing vectors, evaluate \(\varphi\) and differentiate — one line, fewer sign errors.
9 WA timing hacks (tested on IP papers)
- Derivations first: write Eqs. (4)-(6) from memory, circle any required answer — anchors marks early.
- Unit tagging: copy SI units alongside numbers before punching the calculator.
- Escape-vs-orbit confusion check: escape needs \(\sqrt{2}\) factor; circular orbit does not.
10 Why parents should care
An early mastery of gravitational fields lets students pre-learn circular motion and satellite communication, compounding advantage in Term 3. We schedule a 60-min clinic right after the Topic 8 lecture — seats fill fast each semester.
11 Mini-drill (do now!)
Find the minimum launch speed for a probe released from a 400 km-high ISS-style orbit so that it never falls back to Earth.
Hint: subtract the orbital kinetic energy at 400 km from the escape kinetic energy at the same altitude.
12 Further reading
Last updated 14 Jul 2025. We will refresh the guide once the 2027 draft syllabus lands.