Aviation Solutions

Home  /  Blog

Turbine Fuel Explained: The Specifications Jet Fuel Has to Meet

Key Takeaways

  • Turbine fuel is kerosene-type fuel for gas-turbine engines. It is defined by specifications (ASTM D1655, DEF STAN 91-91, GOST 10227 and CGSB-3.22), not by a fixed recipe. A batch qualifies by meeting limits.
  • The key limits include a maximum freezing point of -40°C for Jet A and -47°C for Jet A-1, a minimum flash point of 38°C, density of 775 to 840 kg/m³ and no more than 25% aromatics, as Chevron listed them in 2004.
  • Only approved additives, at parts-per-million levels, may go in. Jet A-1 contains a static dissipator, while US Jet A usually contains none or only an antioxidant.
  • Sustainable aviation fuel is blended, up to 50% for most pathways, because on its own it lacks the aromatics that keep seals sealed.

Most explanations of jet fuel list what’s in it. This one looks at what the fuel must do, and the limits that make it safe for a turbine engine at altitude. For the hydrocarbon breakdown, with a chart of Jet A samples, see our guide to what aviation fuel is.

What Is Turbine Fuel?

Turbine fuel, also called aviation turbine fuel, is the kerosene-type fuel burned by turbofans, turboprops and turboshaft helicopters. It isn’t one product. Four civil grades are widely specified, and each has limits it must meet. Chevron’s Aviation Fuels Technical Review summarises them:

PropertyJet AJet A-1TS-1Jet B
SpecificationASTM D1655DEF STAN 91-91GOST 10227CGSB-3.22
Freezing point, max (°C)-40-47-50 (chilling point)-51
Flash point, min (°C)383828None listed
Density (kg/m³)775 to 840775 to 840774 min at 20°C750 to 801
Aromatics, max25% vol25% vol22% mass25% vol
Smoke point, min (mm)18192520
Net heat of combustion, min (MJ/kg)42.842.842.942.8

That table reflects the specifications as Chevron wrote them in fall 2004, and specifications are revised over time. Chevron’s table lists each grade against one specification, but ASTM D1655 covers Jet A and Jet A-1 alike, so check the current edition before you rely on a figure.

Maximum Freezing Point by Turbine Fuel GradeMaximum freezing point in degrees Celsius: Jet A minus 40, Jet A-1 minus 47, TS-1 minus 50 (measured as a chilling point), Jet B minus 51. Bars lengthen as the limit gets colder. Source: Chevron Aviation Fuels Technical Review, Figure 3.3, specifications as of fall 2004.How Cold Each Grade Must Stay LiquidMaximum freezing point, °C (longer bar = colder limit)Jet A-40Jet A-1-47TS-1*-50Jet B-510-20-40-60degrees Celsius
Source: Chevron, Aviation Fuels Technical Review, Figure 3.3 (specifications as of fall 2004). *TS-1’s figure is a chilling point, a different test from freezing point. Bars are drawn to scale (6 px per degree).

Why Does Turbine Fuel Have So Many Limits?

Each limit guards against a specific failure, and they interact. Chevron notes that as total aromatics rise, density, final boiling point and freezing point rise too, while smoke point falls. That is why the specification caps several properties at once rather than naming ingredients.

  • Freezing point keeps the fuel liquid in the cold. ATSDR notes that Jet A-1’s lower limit suits long international flights, especially polar routes in winter.
  • Flash point limits how readily the fuel’s vapour ignites during handling. Chevron lists a 38°C minimum for Jet A and Jet A-1, and ATSDR notes that the carrier fuel JP-5 has a higher, 60°C flash point for safer handling aboard ships.
  • Aromatics, naphthalenes and smoke point are capped because these compounds form carbon particles in the combustor, which can disrupt airflow and cause visible smoke.
  • Thermal stability matters because the fuel acts as a heat sink for oil, hydraulic fluid and air conditioning, and poor stability leaves deposits.
  • Lubricity comes from trace oxygen, nitrogen and sulfur compounds, and refining that removes them can leave a fuel that needs a lubricity additive at around 10 ppm.

What Additives Can Go Into Turbine Fuel?

Only additives approved in the specification, in the stated amounts, which are measured in parts per million. Chevron says an additive must be tested at four times its maximum dose alongside other additives before approval. Its summary of civil grades:

AdditivePurposeJet AJet A-1
AntioxidantPrevents gums and peroxides forming in storageAllowedRequired in hydroprocessed fuel, otherwise optional
Static dissipatorSpeeds the dissipation of static chargeAllowedRequired
Metal deactivatorBlocks metal contamination that degrades stabilityAllowedAllowed
Corrosion inhibitor and lubricity improverProtects metal and adds lubricityBy agreementAllowed
Icing inhibitor (FSII)Stops ice crystals forming from dissolved waterBy agreementBy agreement
Thermal stability additiveRaises heat tolerance in military fuelNot allowedNot allowed

In practice, international Jet A-1 contains a static dissipator and may carry an antioxidant, while US Jet A usually contains no additives or only an antioxidant. Chevron adds that most commercial aircraft have filter heaters and that icing inhibitor isn’t used by large commercial carriers. Additive use is the main difference between commercial and military fuels.

How Does SAF Change the Picture?

Sustainable aviation fuel has to end up meeting the same specification. According to the IATA SAF Handbook, neat SAF already meets most requirements except its aromatic content and, in some cases, viscosity and density. So it’s blended with conventional fuel, up to 50% depending on the pathway, and then re-certified to ASTM D1655. Once blended, it is treated as ordinary Jet A or Jet A-1, as IATA’s technical certification fact sheet explains.

Aromatics are the reason. GreenAir News reported in 2022 that aromatics swell seal materials, and without them seals can shrink and leak in some older engines and fuelling equipment. Mixing a zero-aromatic component 50/50 with a conventional fuel at about 17% aromatics leaves at least 8%. Our SAF guide covers the pathways.

What Should Buyers Check?

Ask which grade and specification each batch meets and for the certificate to prove it, and confirm the grade your aircraft and airport need. Don’t assume additives: a Jet A uplift may carry none. Our UAE fuel supply guide covers certificates, audits and contract terms.

Frequently Asked Questions

What is turbine fuel?

Turbine fuel is kerosene-type fuel for gas-turbine engines such as turbofans, turboprops and turboshaft helicopters. It is defined by specifications, mainly ASTM D1655 and DEF STAN 91-91, rather than by a fixed recipe.

Is Jet A the same as turbine fuel?

Jet A is one kind of turbine fuel. Jet A-1, TS-1 and Jet B are others. Jet A has a maximum freezing point of -40°C and Jet A-1 -47°C, according to Chevron’s 2004 summary.

What additives are in jet fuel?

Only approved ones, in parts-per-million amounts. International Jet A-1 contains a static dissipator and may carry an antioxidant, while US Jet A usually contains none or only an antioxidant.

Why is SAF blended with conventional jet fuel?

Neat SAF lacks the aromatics that keep some seals swollen, so it’s blended, up to 50% depending on the pathway, and re-certified to ASTM D1655.

Read the Full Composition Guide

For the hydrocarbon classes in Jet A, the types of aviation fuel and which aircraft use which, see our main guide.

What Is Aviation Fuel?

LinkedIn
WhatsApp
Email

Planning a flight or a fuel uplift?

Tell us where you are flying and what you need. Our operations desk answers around the clock.

Scroll to Top