An H2 tank is too large and too heavy for long-haul and ultra-long-haul flights
Law presents other possible scenarios, such as distributing the fuel among several small tanks or combining a larger, comparatively low-pressure H2 storage tank with a smaller high-pressure tank. The latter solution is worth considering for hydrogen direct combustion, since the engines require hydrogen pressures of 60 bar for this. “As a rule, however, several small hydrogen tanks will always be heavier than one or a few large tanks.” For this reason, he expects the second option to become the future standard. However, when it comes to long-haul and ultra-long-haul flights, he points out that just a single tank—even one made as usual of lightweight aluminum—would be so large and heavy that liquid hydrogen is no longer economically viable. “To put it bluntly, the tank would take up all the space, with none left for passengers,” Law says. That’s why MTU believes that long-haul aircraft will be powered by drop-in sustainable aviation fuels (SAFs).
Apart from the challenge of integrating the liquid hydrogen tanks, designing aircraft with fuel cells as the primary propulsion system begs the question as to the best location for the cells. “There are two alternatives,” says Jochen Kaiser, Head of Visionary Aircraft Concepts at the Munich aviation research institution, Bauhaus Luftfahrt. “The fuel cells can be placed either in the fuselage, as close as possible to the hydrogen, or in the nacelle, as close as possible to the electric motor,” he says. Locating them in the fuselage offers the advantage of short hydrogen pipelines to the fuel cells. The downside: longer cables have to be laid to the electric motors. These advantages and disadvantages are reversed in the nacelle, with shorter electric cables and longer H2 pipelines. In Kaiser’s view, the latest research indicates that placing them near the electric motors offers additional benefits. first, it is easier to dissipate the waste heat from the fuel-cell stacks if they are in the nacelle; second, conventional cable technology would be sufficient.