Found the below article useful as a primer:
https://www.energy.gov/eere/fuelcells/articles/fuel-cell-and...
Found the below article useful as a primer:
https://www.energy.gov/eere/fuelcells/articles/fuel-cell-and...
Making a methane-powered jetliner is far more practical than a hydrogen-powered one.
Edit: interesting to do the conversion and realize 700bar is just over 10k psi - misunderstood the parent comment regarding "700bar safe"
Edit2: further interesting to note how the 5k compression of the hydrogen has _higher_ Specific Energy density than 10k due to _decreased_ pressure vessel requirements
Cryogenic fuel looks great until you need to have it sit around unused. Embrittlement, volume, cost, and a rage of safety hazards make it unappealing for aircraft or ships.
So, my guess is the ideal long term solution barring “super batteries” is some sort of synthetic hydrocarbons that uses atmospheric CO2 but we are a long way from viability there.
However the latest generation of rockets seems to have moved away from hydrogen back to things like RP-1 (kerosene) and liquid methane. The high cost and difficulties of working with hydrogen is a factor in this.
Hydrogen may be a solution along with other hybrid approaches (WA state ferry electrification being relevant [1])
[1] https://wsdot.wa.gov/construction-planning/major-projects/fe...
For hydrogen storage, the DoE targets are truly sobering [1]. That whittles down hydrogen from roughly 100 times as dense as batteries to about 5. Throw a 50% thermodynamic efficiency (jet engines are not efficient!) on top of that and hydrogen still has an advantage, but it lags quite badly behind jet fuel. There have been four decades of intensive government-sponsored research effort into hydrogen storage materials, but all existing systems in practical use rely on fiber-composite tanks at 700 bar.
You get better results with an ammonia-burning jet engine. Here the tank weight is negligible and the hydrogen storage density is effectively 15% (after correcting for the enthalpy of formation). But ammonia still has just half the energy density of jet fuel, and it's rather unpleasant to work with. Plus, the existing production process of ammonia faces its own serious inefficiencies, and extensive investigation of more efficient ammonia production has been painstaking with only one Japanese startup [3] that is behind its timeline (probably a little COVID-influenced) and other contenders at lab stage.
With the direct ammonia fuel cell, the power density issue is even worse, but the energy density is very good. This technology competes well with fossil fuels for weight-sensitive applications that do not require high power (DARPA has been interested in a DAFC drone). But ammonia fuel cells are mostly at lab stage, partially because ammonia production remains disappointing (despite a theoretical energy cost of zero) despite considerable research effort.
1: https://www.energy.gov/eere/fuelcells/hydrogen-storage
2: https://www.google.com/search?client=firefox-b-1-lm&q=tsubam...
Liquid I suppose, temperature concern though.