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IB Physics HL B.1 Thermal Energy Transfers Question Bank

Practise IB Physics HL B.1 by combining molecular energy models with quantitative heat transfer, phase-change, conduction and stellar-radiation calculations.

Syllabus
First assessment 2025
Course
Physics HL
Level
HL

Exam points

  • Relate molecular kinetic and potential energy to temperature, density and internal-energy changes.
  • Solve multi-stage heating and phase-change problems using specific heat and latent heat evidence.
  • Apply conduction-rate, Stefan–Boltzmann, inverse-square brightness and Wien-law relationships to extended data.

B.1 Thermal energy transfers question 1

[Maximum number: 9]

Ceres is a dwarf planet in the asteroid belt. The following data are available.

 Mean distance of Ceres from the Sun =4.4×1011 m Mean power output of the Sun =3.8×1026 W\begin{array}{ll} \text { Mean distance of Ceres from the Sun } & =4.4 \times 10^{11} \mathrm{~m} \\ \text { Mean power output of the Sun } & =3.8 \times 10^{26} \mathrm{~W} \end{array}

Question (a)

(a)

Determine the mean temperature of Ceres assuming that it acts as a black-body radiator.

[ 3 ]

Question (b)

(b)

Ceres has a solid rocky core covered with solid ice. The mean temperature is higher than your answer in (a)(i) because radioactive nuclei in the centre of Ceres are decaying. Outline how the energy from the radioactive decay reaches the surface.

[ 2 ]

Question (c)

(c)

At low temperatures such as the mean temperature of Ceres, water undergoes a phase change directly from solid to gas.

[ 4 ]

Question (i)

(i)

Compare the molecular conditions of the solid phase and the gas phase at the same temperature.

[ 3 ]

Question (ii)

(ii)

The maximum surface temperature of Ceres is 38C-38^{\circ} \mathrm{C}. Observations show that significant quantities of water vapour are released from the surface of Ceres every second when the temperature is at this maximum. Calculate the mean kinetic energy of a molecule of water vapour at this temperature.

[ 1 ]

B.1 Thermal energy transfers question 2

[Maximum number: 3]

Question (a)

(a)

A cylindrical spacecraft of cross-sectional area S moves with velocity v. The spacecraft enters a region of dust of density ρ\rho. All the dust that comes into contact with the forward cross-sectional area of the spacecraft sticks to the spacecraft increasing its mass.

Figure for Question (a) — IB Physics HL
[ 1 ]

Question (i)

(i)

Show that in time Δt\Delta t the mass of the spacecraft will increase by an amount ρSvΔt\rho \operatorname{Sv} \Delta t.

[ 1 ]

Question (b)

(b)

The graph shows the variation with time of the height of the International Space Station (ISS) during a 30-day period.

Figure for Question (b) — IB Physics HL

The following data are available:

 Mass of Earth =5.98×1024 kg Mass of the ISS =4.20×105 kg Radius of the Earth =6.38×106 m\begin{aligned} \text { Mass of Earth } & =5.98 \times 10^{24} \mathrm{~kg} \\ \text { Mass of the ISS } & =4.20 \times 10^{5} \mathrm{~kg} \\ \text { Radius of the Earth } & =6.38 \times 10^{6} \mathrm{~m} \end{aligned}

For the 30-day period indicated in the graph the loss of total energy of the ISS is 4.5×109 J4.5 \times 10^{9} \mathrm{~J}.

[ 2 ]

Question (i)

(i)

Estimate the increase in the temperature of the ISS assuming all the lost energy went into thermal energy of the ISS. Take the specific heat capacity of the ISS to be 500Jkg1 K1500 \mathrm{Jkg}^{-1} \mathrm{~K}^{-1}.

[ 2 ]

B.1 Thermal energy transfers question 3

[Maximum number: 1]

Which of the following is equivalent to a temperature of 100C-100^{\circ} \mathrm{C} ?

A

-373 K

B

-173 K

C

173 K

D

373 K373 \mathrm{~K}

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