Close the Book. Start the Clock.

Sections 1 to 11 and 13 taught you this chapter — Kepler's three laws, the universal law and superposition, both shell theorems, gg and the three ways it varies, potential energy and potential, escape speed, orbital speed and period, the energy of a bound orbit, geostationary and polar satellites, weightlessness, forty-odd worked problems and two exam-specific toolkits. This section asks one different question: can you use any of it with a timer running?

There is no new theory below. There are 30 single-correct questions built to the exam pattern, and a marking scheme designed to punish the two habits this chapter rewards most cruelly — reaching for a formula before checking which radius it wants, and writing a potential where a potential energy belongs.

The rules of engagement

Key Point: This is not a reading exercise. Blank sheet, pen, timer. Attempt all 30 questions in one unbroken sitting, and do not open a single explanation until the last answer is written.

The setup What it is
Number of questions 30, single correct option
Marking scheme +4+4 correct, 1-1 incorrect, 00 unattempted
Maximum score 30×4=12030 \times 4 = 120 marks
Minimum possible score 30×(1)=3030 \times (-1) = -30 marks
Suggested time limit 45 minutes (a shade under a minute and a half per question)
Take gg as 9.8 m/s2^2 throughout. No question here uses 10
Allowed rough sheet, your own head
Not allowed calculator, formula sheet, a glance back at the earlier sections

The constants sheet

Every question that needs a number uses these and no others. Copy them to the top of your sheet before you start.

Quantity Value
Gravitational constant GG 6.67×10116.67 \times 10^{-11} N m2^2/kg2^2
Earth's radius RER_E 6.4×1066.4 \times 10^{6} m, i.e. 6400 km
Surface gravity gg 9.8 m/s2^2
GME=gRE2GM_E = gR_E^2 4.01×10144.01 \times 10^{14} m3^3/s2^2
Escape speed from the surface vev_e 11.2 km/s
Orbital speed of a surface-skimming satellite vov_o 7.9 km/s
Gravitational potential at the surface 6.27×107-6.27 \times 10^{7} J/kg
Radius of the geostationary orbit 4.2×1074.2 \times 10^{7} m
Useful roots 2=1.41\sqrt{2} = 1.41, 3=1.73\sqrt{3} = 1.73, π=3.14\pi = 3.14

Those numbers are internally consistent: 2gRE=2(9.8)(6.4×106)=11200\sqrt{2gR_E} = \sqrt{2(9.8)(6.4\times10^6)} = 11\,200 m/s exactly, and 11.22=7.9\frac{11.2}{\sqrt{2}} = 7.9 km/s. Never mix 9.8 and 10 inside one problem — the 2% difference is enough to move you between two adjacent options.

[Exam Tip] That 1-1 is not decoration. Four wild guesses that land one lucky hit earn 43=+14 - 3 = +1 mark for four minutes of work — a terrible trade. But a question narrowed to two options returns 412=+1.5\frac{4 - 1}{2} = +1.5 marks on average, which is a very good one. Narrow first, then commit. Leave blank only what you could not narrow at all.

What this set covers

Topic map, marking scheme and constants sheet for the 30-question drill

Topic Questions How many
Kepler's three laws, ellipse geometry, the area law Q1 to Q3 3
The universal law, superposition and the shell theorems Q4 to Q7 4
gg at the surface and its variation with altitude, depth and rotation Q8 to Q12 5
Gravitational potential energy and gravitational potential Q13 to Q17 5
Escape speed Q18 to Q20 3
Orbital speed and time period Q21 to Q23 3
Satellite energetics and binding energy Q24 to Q27 4
Geostationary and polar satellites, weightlessness Q28 to Q30 3

That spread mirrors how the paper actually samples this chapter. Potential and the variation of gg are 10 of the 30, because between them they carry the most marks here — and they are the two places where a confident wrong answer is easiest to produce. A potential quoted where a potential energy was wanted; 2hRE\frac{2h}{R_E} used at a height where the binomial has long stopped being honest; RER_E written where RE+hR_E + h belonged.

The difficulty mix is roughly 20% easy, 45% medium and 35% hard. A handful will feel brutal. They are meant to.

[Exam Tip] Before you start, write four lines at the top of your sheet: which radius — RER_E, RE+hR_E + h, or REdR_E - d?, is this UU or VV?, what is the sign?, and is anything conserved here? Those four questions decide the method for almost every problem below, and choosing the method is where the marks in this chapter are actually won.

Scoring Yourself Honestly

Mark your sheet with the real scheme — +4+4, 1-1, 00 — and total it. No half marks for "I knew that one really". The number you get is the number that matters.

Four score bands and the expected marks from a narrowed guess

The bands

Your score (out of 120) Verdict What to do next
96 to 120 Exam ready. 80% or more on a hard set, inside the time. Move on. This chapter will not cost you marks. Revisit only the specific items you missed.
72 to 95 Solid, but leaking marks. Almost always slips rather than gaps — a lost minus sign, a 12\frac{1}{2} dropped from GMm2r\frac{GMm}{2r}, RER_E used where RE+hR_E+h belonged. Redo every wrong question without the explanation first.
42 to 71 Shaky. The ideas are there; the execution is not. For each wrong answer go back to the section that owns it (use the topic map above) and rework its solved examples before re-attempting.
Below 42 Start again. Work Sections 1 to 9 properly, then Section 10's worked problems, then Section 11 or 13. Re-attempting this set now teaches you nothing but the answer key.

Read your own answer sheet

Before you touch a single explanation, sort your mistakes into three piles. This is the most valuable ten minutes in the whole section.

  1. Method errors — you used mghmgh where the height was comparable with RER_E, or conserved energy across a manoeuvre in which a rocket did work. You treated the field inside a shell as zero and concluded the potential was zero too. You applied the depth formula gd=g(1dRE)g_d = g\left(1 - \frac{d}{R_E}\right) to a height. These are the expensive ones, because the whole solution is wrong from line one.
  2. Execution errors — right method, wrong arithmetic. The classic three in this chapter: forgetting to add RER_E to a height quoted above the surface, losing the factor 2 between GMmr\frac{GMm}{r} and GMm2r\frac{GMm}{2r}, and dropping a minus sign so that a bound orbit comes out with positive total energy.
  3. Reading errors — the question asked for the potential, not the potential energy; for the speed at aphelion, not perihelion; for the binding energy, not the total energy; for a depth, not a height.

Key Point: In this chapter pile 3 is dominated by four traps: UU or VV, which radius, what sign, and above or below the surface. Check which of the four caught you, every single time.

The eight habits this set is drilling

  • Name the radius before you name the formula. RER_E is the surface, RE+hR_E + h is a point above it, REdR_E - d is a point below it, and rr in an orbital formula is measured from the centre of the Earth, never from the ground.
  • UU and VV are different quantities. VV is measured in J/kg and belongs to the point; U=mVU = mV is measured in joules and belongs to the body you put there. A question that gives you a mass wants UU; a question that does not wants VV.
  • A zero field does not mean a zero potential. Inside a shell the field vanishes everywhere and the potential is a perfectly definite GMR-\frac{GM}{R}. At the null point between two masses the field cancels and the potential does not.
  • Every UU and every VV in this chapter is negative, with the zero taken at infinity. A bound orbit has E<0E < 0. Binding energy is E-E, and it is positive. If a sign comes out the other way, you have made an error, not a discovery.
  • mghmgh is a near-surface approximation. It is the first term of GMEmhRE(RE+h)\frac{GM_Em h}{R_E(R_E+h)}, and it is honest only while hREh \ll R_E. The moment a question says "at a height equal to the Earth's radius", mghmgh is finished.
  • In a circular orbit, K=EK = -E and U=2EU = 2E. Learn the triple once and half the energy questions in this chapter become one line.
  • Kepler's third law needs the semi-major axis, not the perigee distance. For a circle they coincide; for an ellipse they do not, and the question that hands you a perigee and an apogee is testing exactly that.
  • Check the size of the answer. A satellite cannot orbit faster than 7.9 km/s. Nothing launched from the surface at less than 11.2 km/s gets away. The period of any Earth satellite is at least 84.6 minutes.

[Exam Tip] Every explanation below is a full step-by-step solution, so this set doubles as revision. Read the explanation even for the questions you got right — several of these have a two-line route and a two-page route, and it is the two-line route you will need in the hall.