Higher Energy
Curriculum/Energy Forms Conversion
Energy Forms ConversionLayer 24 min

Energy Density and Transportation

A Boeing 787 carries about 100,000 kg of jet fuel for a transatlantic flight. To carry the same energy in lithium-ion batteries, you would need roughly 5,000,000 kg, about 20 times the aircraft's maximum takeoff weight of roughly 254,000 kg. No battery chemistry improvement on any credible roadmap closes a 20x gap. This is a physics constraint, not an engineering one.

Transportation is the sector where energy density matters most, because every kilogram of fuel displaces a kilogram of payload. The relevant metric shifts depending on the application. Short-range vehicles (city cars, delivery vans, buses) can tolerate low energy density because they recharge frequently and the weight penalty is manageable. Long-range, weight-sensitive applications (long-haul trucking, shipping, aviation) need high energy density because the fuel must travel with the vehicle.

This creates a natural technology map: batteries work for short-range surface transport, where efficiency compensates for low energy density. Liquid fuels (diesel, jet fuel, potentially hydrogen or ammonia) dominate long-range and heavy-duty applications where energy per kilogram is the binding constraint.

Worked Example

A container ship needs 200,000 MJ for a Pacific crossing. Compare heavy fuel oil (40 MJ/kg) versus ammonia (18.6 MJ/kg), a proposed zero-carbon shipping fuel.

  • Calculate fuel mass. HFO: 200,000 / 40 = 5,000 kg. Ammonia: 200,000 / 18.6 = 10,753 kg.

Ammonia requires 2.15x more mass for the same energy. What is the practical consequence?

Larger fuel tanks, reduced cargo capacity, and more frequent refueling. The ship's economics change: ammonia's lower energy density means higher fuel volume costs per voyage. This is why zero-carbon shipping fuels face an inherent penalty that no amount of engine efficiency can fully close.

Energy density determines which fuels are physically viable for which transport modes, independent of cost or carbon policy.


Question 1 of 2

Battery-electric aircraft are viable for short regional flights (~100 miles) but not for transatlantic routes primarily because:

At ~0.9 MJ/kg vs ~43 MJ/kg, the battery mass needed for a long flight exceeds the aircraft's structural limits. Short flights need less total energy, making the weight penalty manageable.

The answer is D

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