FOA 660 SDI

FOUR CYLINDER
ENDURANCE
HEAVY FUEL POWER

50 – 57 hp UAV engine, 660 cc four-opposed two-stroke, air-cooled.
Designed for large UAV platforms requiring continuous heavy-fuel performance.

SWISS MADE
*under development juli 2026

The FOA 660-SDI marks Suter’s entry into the large UAV propulsion class.
With a four-cylinder opposed design, it delivers smooth, vibration-free performance and outstanding fuel efficiency, all within a compact and lightweight configuration.
Its heavy-fuel capability (kerosene based fuels like Jet-A1 / JP-5 / JP-8) and Swiss-engineered precision make it a proven solution for long-endurance, high-payload missions.


Civil Applications: Long-endurance surveillance UAVs, mapping platforms, twin-engine VTOL platforms.
Dual-Use Applications: Tactical and logistics UAV’s operating on Kerosine based fuels like Jet-A1 / JP-5 / JP-8 class.

KEY FEATURES

  • Four-Cylinder Architecture
  • Balanced operation with minimal vibration and long service intervals.
  • Heavy-Fuel Operation
  • Runs on gasoline and kerosene-based fuels such as Jet-A1, JP-5, JP-8 for unified logistics.
  • Liquid-Cooled Design
  • Stable power delivery under continuous or high-altitude load
  • Swiss Engineering
  • Casted aluminium block, Nikasil cylinder coating, validated endurance performance.

TECHNICAL SPECIFICATIONS

FOA 660-SDI (Heavy Fuel, Liquid-Cooled)

Parameter Value
Fuel Efficiency 305 g/kWh (BSFC)
Service Ceiling 20,000 ft (6,100 m)
Displacement 660 cc
Configuration Four Opposed, Two-Stroke
Power Output 37,0 – 42,0 kW (50,3 – 57,1 hp) at 6’750 rpm (HF – GAS)
55,0 – 63,5 Nm at 6’000 rpm (HF – GAS)
Weight 16,7 kg engine*
2,4 kg exhaust & silencer
1,5 kg 1 kW/28VDC regulator
1,5 kg Generator 1 kW
Cooling Air cooled
Fuel gasoline and kerosine based fuels line Jet A-1, JP-5/JP-8
Management & Control ECU / 12V system, automatic
Ignition System CDI (Capacitor Discharge Ignition)
Mixture Direct Oil Injection, 2-stroke oil API TC
Dimensions 429 x 422 x 252 mm (L x W x H)

POSITIONING

Purpose-built for the heavy-UAV segment. The FOA 660-SDI features a four-cylinder opposed design with proven heavy-fuel capability. It supports larger airframes, greater payload capacity, and long-endurance mission performance.

 UAV PROPULSION
ENGINEERING SOLUTIONS

Every engine has different integration needs to suit your aircraft. We offer integration engineering support for our engine packages. In addition to standard solutions we offer support to complete your firewall forward installation.

From servo controlled airducts, to keep engine temperature in the preferred range, or tailor-made engine mounts and optimized reduction drives, our engineers will support your demands. The package will be topped with our titanium exhaust systems, where engineering meets art.

Different aircraft and mission profiles and their specific mission profile eventually need an optimization of the engine fuel and ignition map, especially when the fuel varies from international standard specifications.