A.3.14—Fuel energy density

Syllabus
First assessment 2025
Objective
Level
SL

Compare Fuel Energy Density

Energy per volume

For the current IB Physics definition, fuel energy density uu is the transferable energy per unit volume:

u=EVu=\frac{E}{V}

Its SI unit is Jm3\mathrm{J\,m^{-3}}. This lets fuels be compared when storage volume is the constraint.

Connect it to a fuel flow

If fuel flows at volume rate V˙\dot V, its input power is Pin=uV˙P_{in}=u\dot V. Apply efficiency only after finding the input energy or power.

Worked example from local Question Bank row 36970

An engine produces 20kW20\,\mathrm{kW} useful power at 50%50\% efficiency while consuming 1.0×105m3s11.0\times10^{-5}\,\mathrm{m^3\,s^{-1}} of fuel.

Pin=20kW0.50=40kWP_{in}=\frac{20\,\mathrm{kW}}{0.50}=40\,\mathrm{kW}
u=PinV˙=4.0×1041.0×105=4.0×109Jm3=4.0GJm3u=\frac{P_{in}}{\dot V}=\frac{4.0\times10^4}{1.0\times10^{-5}}=4.0\times10^9\,\mathrm{J\,m^{-3}}=4.0\,\mathrm{GJ\,m^{-3}}

Common trap

Specific energy is energy per unit mass, measured in Jkg1\mathrm{J\,kg^{-1}}. Some sources use the words loosely, so let the stated definition and units determine whether to divide by volume or mass.

A.3.14 Exam Analysis

Assessment in practice

2–4 marks
How it is assessed

The evidence asks for fuel volume for a rocket manoeuvre and for energy density from useful engine power and fuel consumption rate.

Command terms

Estimate / Calculate

What earns marks

Use the fuel energy density with the fuel volume to find input energy, then apply efficiency and any time or kinetic-energy relation. Keep volume units in m³ when the density is given in J m⁻³.

Watch for

Using mass-specific energy when volume-specific energy is given, or omitting efficiency before comparing useful output.

Representative question

Question 1

[Maximum number: 2]

At the end of the 30-day period, rockets are fired to bring the ISS back to its initial height. The energy density of liquid hydrogen rocket fuel is 8.5×103MJm38.5 \times 10^{3} \mathrm{MJ} \mathrm{m}^{-3}.

Estimate the volume of fuel needed.