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Topic D.1 · SL and HL

Gravitational Fields: notes and practice questions

Summary
  • This topic describes gravitational fields, including Kepler's laws of orbital motion and Newton's law of universal gravitation.
  • Kepler's three laws describe the motion of planets around the Sun.
  • Newton's universal law of gravitation states that F=Gm1m2r2F = G\frac{m_1m_2}{r^2}.
  • Gravitational field strength gg is defined as the force per unit mass, g=Fm=GMr2g = \frac{F}{m} = G\frac{M}{r^2}.
  • Extended bodies can be treated as point masses for gravitational calculations under specific conditions.
  • Gravitational field lines are used to represent the direction and strength of a gravitational field.
  • Orbital motion problems at this level assume circular orbits.

How it is examined

Both papers, both levels. May 2025 Paper 2 TZ1 question 2 was common to SL and HL: calculate an orbital radius ratio using Kepler's third law from two orbital periods (2 marks), then explain how planetary observations let scientists determine the mass of the Sun (2 marks, "any 2 from" three marking points). HL got a third part using the potential gradient: estimate the average field strength from ΔV/Δr\Delta V/\Delta r (2 marks). That part is HL-only content and shows how the same stem is split across levels. Potential, potential energy, escape speed and equipotentials must never appear in an SL question.

Given in the booklet

SL: F=Gm1m2/r2F = Gm_1m_2/r^2, g=F/m=GM/r2g = F/m = GM/r^2, and the gravitational constant G. Kepler's three laws are statements, not booklet equations, and the third law in the form r3/T2=constantr^3/T^2 = \text{constant} has to be assembled by the student. HL adds EpE_\text{p}, VgV_\text{g}, the potential gradient, W=mΔVgW = m\Delta V_\text{g}, vescv_\text{esc} and vorbitalv_\text{orbital}.

Key ideas
  • Kepler's three laws of orbital motion
  • Newton's universal law of gravitation as given by F=Gm1m2r2F = G\dfrac{m_1 m_2}{r^2} for bodies treated as point masses
  • conditions under which extended bodies can be treated as point masses
  • that gravitational field strength g at a point is the force per unit mass experienced by a small point mass at that point, as given by g=Fm=GMr2g = \dfrac{F}{m} = G\dfrac{M}{r^2}
At HL
  • that the gravitational potential energy EpE_\text{p} of a system is the work done to assemble the system from infinite separation of its components
  • the gravitational potential energy for a two-body system as given by Ep=−Gm1m2rE_\text{p} = -G\dfrac{m_1 m_2}{r}, where r is the separation between the centres of mass of the two bodies
  • that the gravitational potential VgV_\text{g} at a point is the work done per unit mass in bringing a mass from infinity to that point, as given by Vg=−GMrV_\text{g} = -G\dfrac{M}{r}
  • the gravitational field strength g as the gravitational potential gradient, as given by g=−ΔVgΔrg = -\dfrac{\Delta V_\text{g}}{\Delta r}

Guiding questions

  • How are the properties of a gravitational field quantified?
  • How does an understanding of gravitational fields allow for humans to explore the solar system?

Linking questions

  • What measurements of a binary star system need to be made in order to determine the nature of the two stars?
  • How is uniform circular motion like and unlike real-life orbits?
  • How is the amount of fuel required to launch rockets into space determined by considering energy?
  • How can air resistance be used to alter the motion of a satellite orbiting Earth?
  • What are the benefits of using consistent terminology to describe different types of fields? (NOS)
  • How can the motion of electrons in the atom be modelled on planetary motion and in what ways does this model fail? (NOS)
  • Physics utilizes a number of constants such as G. What is the purpose of these constants and how are they determined? (NOS)

Practice questions

19 questions · 5 easy · 14 medium
Showing 19 of 19

Question 1

EasyPaper 1A · calculator1 mark

Two satellites, A and B, are in stable circular orbits around the Earth. The orbital period of satellite A is TAT_A and its orbital radius is RAR_A. The orbital period of satellite B is TBT_B and its orbital radius is RBR_B. Which expression correctly relates their periods and radii?

A. TATB=RARB\frac{T_A}{T_B} = \frac{R_A}{R_B}

B. TA2TB2=RB3RA3\frac{T_A^2}{T_B^2} = \frac{R_B^3}{R_A^3}

C. TA2TB2=RA3RB3\frac{T_A^2}{T_B^2} = \frac{R_A^3}{R_B^3}

D. TA3TB3=RA2RB2\frac{T_A^3}{T_B^3} = \frac{R_A^2}{R_B^2}

Question 2

MediumPaper 1A · calculator1 mark

In a simplified classical model of an atom, an electron orbits the nucleus in a circular path. Electron A orbits the nucleus at a radius RR. Electron B orbits the same nucleus at a radius 2R2R. Assume the only force acting on the electrons is the electrostatic force from the nucleus, which provides the centripetal force for the orbit. This electrostatic force follows an inverse square law with distance.

What is the ratio centripetal acceleration of electron Acentripetal acceleration of electron B\frac{\text{centripetal acceleration of electron A}}{\text{centripetal acceleration of electron B}}?

A. 14\frac{1}{4}

B. 12\frac{1}{2}

C. 2

D. 4

Question 3

EasyPaper 1A · calculator1 mark

Two artificial satellites, A and B, are in stable circular orbits around the Earth.

The orbital period of satellite A is TAT_A and its orbital radius is rAr_A. The orbital period of satellite B is TBT_B and its orbital radius is rBr_B.

What is the ratio rArB\frac{r_A}{r_B}?

A. (TATB)23\left(\frac{T_A}{T_B}\right)^{\frac{2}{3}}

B. (TATB)32\left(\frac{T_A}{T_B}\right)^{\frac{3}{2}}

C. (TBTA)23\left(\frac{T_B}{T_A}\right)^{\frac{2}{3}}

D. (TBTA)32\left(\frac{T_B}{T_A}\right)^{\frac{3}{2}}

Question 4

MediumPaper 1A · calculator1 mark

An exoplanet, Kepler-X, has a mass that is 8 times the mass of another exoplanet, Kepler-Y. The radius of Kepler-X is twice the radius of Kepler-Y.

The gravitational field strength at the surface of Kepler-Y is gg.

What is the gravitational field strength at the surface of Kepler-X?

A. 0.5g0.5g

B. 2g2g

C. 4g4g

D. 32g32g

Question 5

EasyPaper 1A · calculator1 mark

What is the primary application of the stellar parallax method in astronomy?

A. To determine the chemical composition of a star.

B. To measure the distance to nearby stars.

C. To calculate the surface temperature of a star.

D. To measure the recessional velocity of distant galaxies.

Question 6

MediumPaper 2 · calculator4 marks
(a)

A space probe, carrying a scientific instrument, lands on an exoplanet. The instrument has a weight of 750 N750\ \text{N} on the surface of Earth.

(a) Calculate the weight of the instrument on the exoplanet if the exoplanet has a radius that is one-third of Earth's radius and a density that is 1.51.5 times the density of Earth.

[2]
(b)

(b) Calculate the weight of the instrument on a different celestial body, Planet Y, if Planet Y has a radius that is 0.80.8 times Earth's radius and a mass that is 0.60.6 times Earth's mass.

[2]

Question 7

EasyPaper 1A · calculator1 mark

A communications satellite is in a stable elliptical orbit around the Earth. It is moving from its perigee (the point of closest approach) to its apogee (the point of furthest approach).

Which quantity is increasing during this part of the orbit?

A. The satellite's speed

B. The satellite's kinetic energy

C. The satellite's gravitational potential energy

D. The magnitude of the gravitational force on the satellite

Question 8

MediumPaper 2 · calculator5 marks
(a)

A geostationary communication satellite, with a mass of 2.5×103 kg2.5 \times 10^3\ \text{kg}, orbits the Earth at an altitude of 3.5786×107 m3.5786 \times 10^7\ \text{m} above the Earth's surface.

The mass of the Earth is 5.97×1024 kg5.97 \times 10^{24}\ \text{kg} and its radius is 6.371×106 m6.371 \times 10^6\ \text{m}.

(a) Calculate the magnitude of the gravitational force of attraction between the Earth and the satellite.

[2]
(b)

(b) According to Newton's first law of motion, a non-zero force should cause an object to accelerate. Explain how the force you calculated in (a) causes the satellite to accelerate while maintaining its orbit.

[3]

Question 9

EasyPaper 1A · calculator1 mark

Two satellites, S and T, orbit a planet in circular orbits. Satellite S has mass mm and orbital radius 2R2R. Satellite T has mass 4m4m and orbital radius RR.

What is the ratio centripetal force acting on Scentripetal force acting on T\frac{\text{centripetal force acting on S}}{\text{centripetal force acting on T}}?

A. 116\frac{1}{16}

B. 18\frac{1}{8}

C. 12\frac{1}{2}

D. 11

Question 10

MediumPaper 1A · calculator1 mark

A piece of space debris of mass mm is in a circular orbit of radius RR around Earth. Its orbital speed is vv. A second piece of space debris of mass 2m2m is in a circular orbit of radius 4R4R around Earth.

What is the orbital speed of the second piece of debris?

A. 14v\frac{1}{4}v

B. 12v\frac{1}{2}v

C. 2v2v

D. 4v4v

Question 11

MediumPaper 1A · calculator1 mark

An exoplanet A has a mass twice that of exoplanet B. The radius of exoplanet A is half that of exoplanet B.

The gravitational field strength at the surface of A is gg.

What is the gravitational field strength at the surface of B?

A. g8\frac{g}{8}

B. g4\frac{g}{4}

C. 4g4g

D. 8g8g

Question 12

MediumPaper 1A · calculator1 mark

What are the fundamental SI units of the universal gravitational constant GG?

A. kg−1m3s−2\text{kg}^{-1} \text{m}^3 \text{s}^{-2}

B. Nm2kg−2\text{N} \text{m}^2 \text{kg}^{-2}

C. kgm3s−2\text{kg} \text{m}^3 \text{s}^{-2}

D. kg−1m2s−2\text{kg}^{-1} \text{m}^2 \text{s}^{-2}

Question 13

MediumPaper 1A · calculator1 mark

A research satellite orbits a newly discovered exoplanet. At an altitude where its orbital radius from the center of the exoplanet is RR, the gravitational field strength experienced by the satellite is gRg_R. The satellite then adjusts its orbit to a new altitude where its orbital radius from the center of the exoplanet is 2R2R.

What is the difference in the magnitude of the gravitational field strengths experienced by the satellite between these two orbital radii?

A. gR2\frac{g_R}{2}

B. gR4\frac{g_R}{4}

C. 3gR4\frac{3g_R}{4}

D. gR8\frac{g_R}{8}

Question 14

MediumPaper 1A · calculator1 mark

A space probe is at a distance rr from the centre of a planet. The gravitational field strength at this point is g0g_0. The probe moves to a new position at a distance of 4r4r from the centre of the planet.

What is the magnitude of the change in the gravitational field strength experienced by the probe?

A. 1516g0\frac{15}{16}g_0

B. 116g0\frac{1}{16}g_0

C. 34g0\frac{3}{4}g_0

D. 14g0\frac{1}{4}g_0

Question 15

MediumPaper 1A · calculator1 mark

Two artificial satellites, P and Q, are in circular orbits around a planet. The orbital radius of satellite P is RR and the orbital radius of satellite Q is 4R4R. What is the ratio orbital period of Qorbital period of P\frac{\text{orbital period of Q}}{\text{orbital period of P}}?

A. 2

B. 4

C. 8

D. 16

Question 16

MediumPaper 1A · calculator1 mark

Star Alpha has luminosity LL and apparent brightness bb. Star Beta has luminosity 4L4L and apparent brightness 16b16b.

As viewed from Earth, what is parallax angle subtended by Alphaparallax angle subtended by Beta\frac{\text{parallax angle subtended by Alpha}}{\text{parallax angle subtended by Beta}}?

A. 14\frac{1}{4}

B. 12\frac{1}{2}

C. 22

D. 44

Question 17

MediumPaper 1A · calculator1 mark

A comet follows a highly elliptical orbit around a star. Which statement about the comet's motion is incorrect?

A. The speed of the comet is greatest when it is closest to the star.

B. The star is located at one of the foci of the comet's elliptical orbit.

C. The square of the comet's orbital period is proportional to the square of the semi-major axis of its orbit.

D. A line connecting the comet and the star sweeps out equal areas in equal time intervals.

Question 18

MediumPaper 1A · calculator1 mark

Two satellites, Alpha and Beta, orbit the Earth in circular paths.

The average orbital radius of satellite Alpha is four times greater than the average orbital radius of satellite Beta.

What is orbital period of satellite Alphaorbital period of satellite Beta\frac{\text{orbital period of satellite Alpha}}{\text{orbital period of satellite Beta}}?

A. 4\sqrt{4}

B. 424^2

C. 43\sqrt{4^3}

D. 434^3

Question 19

MediumPaper 1A · calculator1 mark

Two satellites, Alpha and Beta, are in circular orbits around a planet.

The orbital period of satellite Alpha is eight times greater than the orbital period of satellite Beta.

What is orbital radius of satellite Alphaorbital radius of satellite Beta\frac{\text{orbital radius of satellite Alpha}}{\text{orbital radius of satellite Beta}}?

A. 2

B. 4

C. 8

D. 64

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Where marks are lost

  • Stopping one step short of the conclusion. Two numbers and no sentence is two marks out of three.
  • Answering a procedure question with a platitude.
  • Losing precision in Paper 1B. Uniquely to this paper, quoting the right number badly loses marks.
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What does Gravitational Fields cover in IB Physics?

This topic describes gravitational fields, including Kepler's laws of orbital motion and Newton's law of universal gravitation. Kepler's three laws describe the motion of planets around the Sun. Newton's universal law of gravitation states that F = G(m_1m_2)/(r^2).

Is Gravitational Fields SL or HL?

Both. SL and HL students study Gravitational Fields, and HL goes further: that the gravitational potential energy E_p of a system is the work done to assemble the system from infinite separation of its components.

How do I revise Gravitational Fields for IB Physics?

Start from the core idea: this topic describes gravitational fields, including Kepler's laws of orbital motion and Newton's law of universal gravitation. In the exam: both papers, both levels. May 2025 Paper 2 TZ1 question 2 was common to SL and HL: calculate an orbital radius ratio using Kepler's third law from two orbital periods (2 marks), then explain how planetary observations let scientists determine the mass of the Sun (2 marks, "any 2 from" three marking points). Then practise exam-style questions, easiest first, writing out every step of your working before you check it.

How does FourtyFive help me practise Gravitational Fields?

FourtyFive has 19 Gravitational Fields questions. Every answer you write is marked mark by mark, IB-style, and you see where each mark was won or lost. Every part has a hint, the AI tutor helps you through the step you are stuck on, and your Study Profile picks what to practise next.

Is FourtyFive free for Gravitational Fields practice?

Yes. A free account gives you 50 marked answers a month, and you do not need a card to sign up.

Can I handwrite Gravitational Fields answers on an iPad?

Yes. In the FourtyFive iPad app you write your working by hand with Apple Pencil, the way you would on paper, and it is marked the same way.

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