Can We Keep Flying Without Fossil Fuels?

A drop-in hydrocarbon can be assembled from water, electricity, and captured carbon. The chemistry is known. The hard part is paying for every conversion while keeping the whole factory busy.

Last updated September 2026
Figure 2 · Follow one unit through the stack

A fuel plant is a chain of conversions

Select a layer. The retained-energy ranges are an engineering frame, not a promise for a particular plant.

Layer 1 of 7

Clean electricity

Energy state
100 units in
Product
Electricity
Operating measure
$/MWh · carbon intensity · hourly match
Where energy goes
Curtailment, transmission, and an under-used connection

Binding constraint: The fuel plant needs low-carbon power at the same hours it needs utilization.

The ranges summarize the architecture of power-to-liquids. A defensible project model must replace them with measured unit operations, an hourly power profile, recycle streams, and product yields.

What the record shows

  • A litre of jet-range fuel stores roughly 9.5 kWh, while representative power-to-liquid designs require far more electrical input after hydrogen, syngas, synthesis, and upgrading losses.
  • Stoichiometry alone requires about 0.429 kg of H₂ and 3.14 kg of CO₂ for one kilogram of idealized –CH₂– hydrocarbon; real plants need recycle and make off-products.
  • Cheap intermittent power can raise rather than lower fuel cost when electrolysers and synthesis trains recover capital across too few operating hours.
  • The EU requires synthetic aviation fuels to reach 1.2% of fuel supplied at covered airports in 2030 and 35% in 2050, creating demand before a mature cost curve exists.

Mass balances below are derived. Mandates are policy. Announced plants and nameplate tonnes are not counted as operating output.

Part I: Reverse combustion

Build the molecule that an engine takes apart

Combustion combines a hydrocarbon with oxygen and releases heat, CO₂, and water. Power-to-liquids pays energy to reverse that direction: split water, recover carbon, create carbon monoxide, form longer chains, and refine them into a specification.

Clean electricity + H₂O→H₂ + captured CO₂→Drop-in hydrocarbon + O₂

The product's advantage is compatibility. Dense liquid fuel can use aircraft, engines, tanks, pipelines, and logistics built around hydrocarbons. Its disadvantage is the same fact viewed thermodynamically: electricity is converted into a molecule and later converted again into motion, losing useful energy at both stages.

Compatibility is what the losses buy

44 MJ/kgRegulatory energy-content value for Fischer–Tropsch jet fuel.
1.2%EU synthetic-aviation-fuel minimum share from 2030.
35%EU synthetic share required in 2050 under ReFuelEU Aviation.

Those percentages are demand obligations, not evidence that production has reached scale. EASA's 2026 market report said no large synthetic-fuel facility had yet reached final investment decision in its assessed EU pipeline.

Part II: The material floor

The atoms set a lower bound

An idealized hydrocarbon repeat unit, CH₂, has one carbon atom and two hydrogen atoms. Molar mass makes the minimum feed transparent before conversion losses enter.

3.14 kgStoichiometric CO₂ per kilogram of idealized CH₂ hydrocarbon.
0.429 kgStoichiometric H₂ feed per kilogram before process losses and upgrading; 0.143 kg is the hydrogen contained in the product.
~2.5–4 kg/LPractical modeling range for CO₂ input once density, selectivity, and yield enter.

Not all captured carbon reaches saleable jet fuel. Fischer–Tropsch synthesis produces a distribution of chain lengths. Gas and light fractions may be recycled or used for heat; heavy waxes are hydrocracked; oxygenates and water are separated. A plant should report carbon efficiency to each product, not only conversion inside one reactor.

Part III: Compounded conversion

Every individually reasonable step takes a cut

Electrolysis, compression, reverse water-gas shift, synthesis, separation, and upgrading multiply rather than add their efficiencies.

A 70%-efficient electrolyser followed by an 80%-efficient synthesis and upgrading chain retains only 56% before balance-of-plant loads. Real system comparison must include capture energy, compression, recycle, heat integration, auxiliaries, and the fuel fraction that meets the target specification.

LayerMain measureFailure mode
ElectricityHourly $/MWh and carbon intensityCheap hours leave capital idle
HydrogenkWh/kg, stack life, utilizationReplacement and compression erase gains
CarbonOrigin, purity, $/t, capture energyCheap fossil CO₂ does not close the loop
SynthesisCarbon efficiency and target yieldOff-products dilute saleable output
UpgradingCertified litres per feed tonneFuel misses freezing, density, or blending rules
Figure 3 · Interactive production-floor model

Cheap electricity is not the same as cheap fuel

Change power price and plant utilization together. The model exposes electricity, carbon feedstock, and capital recovery for a nominal 100,000-litre-per-day plant; it is not a delivered-fuel quote.

Firm clean power$3.22/L

Exposed production burden

Electricity
$0.77/L
CO₂ feedstock
$0.32/L
Capital + fixed
$2.13/L
Electricity input
21.9 kWh/L
Implied power-to-liquid
43%

A litre of jet-range hydrocarbon contains roughly 9.5 kWh of lower-heating-value energy. The model's implied efficiency divides that by electrolyser plus selected process electricity; it therefore excludes upstream generation and downstream engine losses.

Calculation and boundaries

Electricity cost = (hydrogen input × electrolyser kWh/kg + other process kWh) × $/kWh. Carbon cost = kg CO₂/L × $/kg. Capital + fixed cost = installed capital × annual charge rate ÷ (100,000 L/day × 365 × utilization).

Excluded: water, catalysts, replacement stacks, oxygen or heat credits, carbon-capture energy if not included in CO₂ price, product yield outside the selected inputs, storage, blending, transport, taxes, margin, and financing beyond the annual charge. Installed capital is deliberately user-set; no single public number describes projects with different boundaries.

In the intermittent scenario, a lower power tariff is overwhelmed by capital spread across fewer litres. This is the central e-fuel trade: the cheapest hour can be an expensive factory schedule.
Part IV: The factory clock

The cheapest electron can make expensive fuel

A synthesis plant sized for occasional surplus power earns revenue occasionally but carries capital continuously.

Hydrogen storage can decouple a flexible electrolyser from a steadier synthesis loop, but it adds compression, tanks or caverns, inventory, and another utilization problem. Firm clean electricity costs more per MWh but can lower capital cost per litre. The optimum depends on the joint hourly system, not an annual average power price.

Electrolysers can flex

Stacks can follow power more readily than a hot, pressurized chemical loop, though cycling can affect efficiency and life.

Synthesis prefers continuity

Catalysts, recycle ratios, separation columns, and heat integration work best near a designed operating state.

Storage buys coupling

Hydrogen or intermediate storage protects synthesis utilization while exposing capital, safety, and geography.

Contracts shape operation

Hourly clean-power rules, grid access, and product offtake determine whether an optimized plant is legally low-carbon and financially useful.

Part V: Carbon is a feedstock and a claim

The cheapest source may defeat the purpose

Concentrated industrial CO₂ is easier to purify than atmospheric CO₂, but carbon origin changes the lifecycle story.

Biogenic CO₂ and direct air capture can create a circular atmospheric carbon flow when powered cleanly. Fossil point-source CO₂ can reduce emissions relative to extracting fresh oil but still introduces geological carbon after combustion. A credible fuel certificate traces carbon origin, hydrogen electricity, process energy, transport, and co-product allocation.

Part VI: The hard-use test

Aviation pays for density and compatibility

Cars can use batteries directly. Long-haul aircraft carry their energy source, making mass, volume, freezing behavior, and global refuelling compatibility unusually valuable.

This makes aviation the strongest case for synthetic hydrocarbons, and a stringent test. Fuel must meet ASTM pathways and blend rules, contain appropriate aromatics or be paired with them, work at low temperature, and arrive at airports through certified custody. Policy can create initial demand; only operating plants reveal the eventual premium.

Who is building what

Direct electrochemical CO₂ reduction, reverse water-gas shift, Fischer-Tropsch catalytic synthesis, and high-temperature co-electrolysis construct drop-in hydrocarbon fuels. Search the record, or filter by synthesis pathway.

8 programmes
TwelveOpus CO2 Electrolysis & E-JetElectrochemical CO₂ reduction using proprietary membrane electrode assemblies (MEA) converting CO₂ and water directly into syngas, bypassing separate reverse water-gas shift
Reported evidence
Constructing commercial E-Jet manufacturing plant (AirPlant One) in Moses Lake, Washington; delivered certified synthetic SAF to commercial aviation partners.
Announced next step
Commercial volume production of drop-in aviation fuel with up to 90% lifecycle emissions reduction compared to fossil jet A-1.
Unresolved risk
Catalyst durability and selectivity against hydrogen evolution over thousands of operating hours in industrial CO₂ electrolyzer stacks.
HIF GlobalHaru Oni Demonstration & MatagordaPairing high-capacity wind power in southern Chile with Siemens alkaline electrolyzers, direct air capture, and methanol-to-gasoline (MTG) catalytic synthesis
Reported evidence
Haru Oni operational in Magallanes, Chile, producing certified e-gasoline shipped to Porsche for test fleets; developing commercial e-fuel plant in Texas.
Announced next step
Commercial export facilities producing millions of liters of carbon-neutral gasoline and e-methanol annually for automotive and marine offtake.
Unresolved risk
Very high capital investment per barrel of delivered fuel, long marine shipping distances, and low overall round-trip energy efficiency (~45%).
Norsk e-FuelMosjøen Power-to-LiquidIntegrating solid oxide co-electrolysis with direct air capture and Fischer-Tropsch synthesis to produce synthetic paraffinic kerosene (e-SAF)
Reported evidence
Secured industrial site in Mosjøen, Norway with access to clean hydropower; signed commercial SAF offtake agreements with Norwegian Air and Cargolux.
Announced next step
Commercial plant commissioning targeting 50 million liters of fossil-free aviation fuel annually by 2026–2028.
Unresolved risk
Power supply allocation constraints on local grids and high cost differential between e-SAF and fossil jet fuel requiring regulatory mandates.
InfiniumElectrofuels Facility (Pathfinder)Direct conversion of captured industrial CO₂ and green hydrogen into drop-in synthetic diesel and aviation fuel using proprietary catalysts
Reported evidence
Commissioned operational commercial e-fuels facility (Project Pathfinder) in Corpus Christi, Texas, delivering commercial synthetic fuel to Amazon's fleet.
Announced next step
Expanding commercial production facilities in Texas and France supplying drop-in electrofuels to global transport fleets.
Unresolved risk
Reliable long-term supply of pure biogenic or direct-air-captured CO₂ feedstock at predictable pricing.
Prometheus FuelsElectrochemical Carbon SeparationDirect electrochemical conversion of atmospheric CO₂ in water into ethanol and alcohols, separated via carbon nanotube membranes and catalytic oligomerization
Reported evidence
Demonstrated laboratory and pilot electrochemical cells producing automotive-grade gasoline; backed by BMW i Ventures and American Airlines.
Announced next step
Zero-carbon drop-in gasoline produced at standard retail pump price parity without government subsidies.
Unresolved risk
Membrane selective flux under high current densities and scaling nanoscale electrochemical reactors to industrial fuel volumes.
SunfireCo-Electrolysis (SOEC)High-temperature solid oxide electrolysis cells operating at ~800°C co-electrolyzing steam (H₂O) and CO₂ simultaneously into synthesis gas (CO + H₂)
Reported evidence
Multi-megawatt SOEC systems deployed in European industrial pilots; demonstrated significant electrical efficiency gains over low-temperature systems.
Announced next step
Direct coupling of high-temperature co-electrolysis to Fischer-Tropsch synthesis loops, recycling synthesis heat directly back to the electrolyzer.
Unresolved risk
Ceramic cell degradation under fluctuating carbon-monoxide chemical potentials, carbon coking on electrodes, and thermal cycling.
LanzaTech / LanzaJetFreedom Pines Fuels (Alcohol-to-Jet)Biological gas fermentation of industrial carbon monoxide off-gases into ethanol, followed by chemical Alcohol-to-Jet (ATJ) catalytic synthesis into SAF
Reported evidence
Inaugurated world's first commercial ATJ plant (LanzaJet Freedom Pines Fuels) in Soperton, Georgia, producing 10 million gallons/year of SAF and renewable diesel.
Announced next step
Deploying 1 billion gallons of annual SAF production capacity globally by 2030 across international aviation hubs.
Unresolved risk
Competition for commercial ethanol feedstocks from road transport blending and chemical industry applications.
ICAO / ReFuelEU AviationRegulatory Mandates & Book-and-ClaimEuropean Union and international aviation mandates legally requiring airlines to blend increasing percentages of synthetic e-kerosene (starting at 1.2% in 2030, rising to 35% in 2050)
Reported evidence
ReFuelEU Aviation regulation officially adopted into EU law, establishing guaranteed statutory demand for certified non-fossil synthetic fuels.
Announced next step
Establishing book-and-claim digital accounting systems allowing airlines to purchase e-SAF attributes without physically fueling at every airport.
Unresolved risk
Compliance penalty thresholds versus commercial fuel cost gaps, and potential airline route leakage to non-EU refueling hubs.

Overall electrical-to-fuel thermodynamic round-trip efficiency rarely exceeds 40–50%; e-fuel production requires ~20–25 kWh of zero-carbon electricity per liter of drop-in jet fuel.

An optimistic view, with conditions

Use synthetic fuel where the molecule earns its losses

The stack can improve through cheaper power, durable electrolysers, heat integration, higher selectivity, modular construction, and shared carbon infrastructure. It should compete first where direct electrification cannot deliver the same service.

Now

Prove full balances

Publish hourly electricity, net carbon intensity, utilization, carbon efficiency, target yield, and delivered litres.

First markets

Concentrate demand

Aviation mandates and durable offtake can support initial plants without pretending they match fossil price.

Scale test

Standardize trains

Repeatable electrolysis, synthesis, upgrading, and certification packages must turn projects into products.

How much fuel must the new system replace?

IATA estimates 1.9 million tonnes of sustainable aviation fuel in 2025, just 0.6% of global jet-fuel use. Most of that supply is biofuel from oils and fats, not synthetic fuel. In the EU, EASA’s 2026 review of 2025 reporting recorded 1.1 million tonnes of SAF, about 2.79% of reported supply, predominantly used-cooking-oil biofuel. It found no large synthetic-fuel facility in the assessed EU pipeline had reached final investment decision. The EU mandate rises to 6% total SAF in 2030, including 1.2% synthetic, and 70% total in 2050, including 35% synthetic.

The same EASA review gives a 2025 reference price of €640/t for conventional jet fuel and €1,925/t for bio-based SAF. Its synthetic-fuel reference of €7,520/t using industrial or biogenic CO₂ is a modeled production-cost estimate, not an observed transaction: EASA says real e-SAF price indexes were unavailable. This is a more useful price boundary than treating every SAF premium as an e-fuel price. EASA reference-price method and table.

For a scale check, IATA’s 1.9 Mt and 0.6% imply roughly 317 Mt of annual global jet fuel. Supplying 10% as synthetic fuel would mean about 32 Mt of fuel, at least 100 Mt of CO₂ feed from CH₂ stoichiometry, and around 790 TWh of clean electricity at an illustrative 20 kWh/L and 0.8 kg/L. Actual input rises with carbon and fuel yield losses. This is a derived scenario, not a forecast of future demand or plant output. If a synthesis train’s annual capital charge is unchanged, halving its utilization doubles that capital charge per litre; cheap, intermittent power only helps when the electricity savings exceed this penalty and any buffering cost.

Fuel carbon is also only part of aviation’s climate effect. EASA’s aviation non-CO₂ review identifies contrails, NOₓ and aerosols as material and uncertain warming terms. Cleaner fuel composition and targeted contrail avoidance are separate levers; a carbon-neutral molecule does not automatically cancel them. Battery-electric and hydrogen aircraft may serve some shorter routes, but the energy density and airport infrastructure needed for long-haul flight keep drop-in fuels central to that segment.

Efficiency helps, but the aircraft choice still depends on range

ICAO estimates aircraft built in the mid-2010s used about 80% less fuel per passenger-kilometre than 1960s aircraft, while anticipated efficiency gains of roughly 1–2% a year were slower than traffic growth in its cited outlook. This is a long-run aircraft comparison, not a measured 2026 fleet average. Airbus revised its ZEROe hydrogen roadmap in 2025 toward technology maturation; it did not announce an operating zero-emission airliner. Battery and hydrogen concepts may reduce fossil demand on shorter missions, while long-haul aircraft remain the main case for certified dense liquid fuel. Programme nameplate capacity below is not evidence of delivered e-SAF.

Sources, method, and boundaries

Stoichiometric figures are derived from molar mass; the calculator exposes assumptions rather than predicting market price. Policy shares are legal requirements. Announced capacity and targets are not operating production.