HF TOA 330-SDI

HEAVY-FUEL TWIN
ENDURANCE-FOCUSED

24-29 hp UAV engine, twin-opposed two-stroke, air-cooled. Optimized for kerosene based fuels like Jet-A1 with JP-5 and JP-8 compatibility.

SWISS MADE

The TOA 330-SDI is Suter’s heavy-fuel twin engine for medium UAV platforms.
Its twin-opposed layout delivers smooth operation and low vibration, while the air-cooled architecture keeps the system light, efficient, and easy to maintain.
Designed for survey and mapping missions that demand reliable mid-range power and long-duration performance, the TOA 330 combines Swiss engineering precision with field-focused durability.
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Civil Applications: Fixed-wing UAVs for mapping, survey, and training operations.
Dual-Use Applications: Platform-ready heavy-fuel variant for extended-range and endurance-focused operations.

KEY FEATURES

  • Heavy-Fuel Advantage:
  • Optimized for kerosene based fuels like Jet-A1 with JP-5 and JP-8 compatibility.
  • Compact Twin Design:
  • Balanced two-cylinder architecture for low vibration and smooth operation.
  • High Power Density:
  • 24.6-29.2 output from a compact 330 cc displacement
  • ECU Integration:
  • ECU-managed fuel and ignition, cold start support, altitude compensation, EGT monitoring and over-temperature protection.

TECHNICAL SPECIFICATIONS

TOA 330-SDI (Heavy Fuel, Air-Cooled)

Parameter Value
Fuel Efficiency 305 g/kWh (BSFC)
Service Ceiling 20,000 ft (6,100 m)
Displacement 330 cc
Configuration Twin-opposed, two-stroke
Power Output 18.1 – 21.5 kW (24.6-29.2 hp) at 6,750 rpm (HF – GAS)
27.2 – 33.4 Nm at 6,000 rpm (HF – GAS)
Weight 8.8 kg engine*
+ 1.8 kg exhaust & silencer
+ 1.5 kg 1 kW / 28 VDC regulator
+ 1.5 kg generator 1 kW
Cooling Air-cooled
Fuel

Kerosine based fuels like 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 253 × 453 × 285 mm (L × W × H)

POSITIONING

The TOA 330-SDI combines compact size with high endurance. Its combination of altitude capability, fuel flexibility and high efficiency makes it well suited for UAV platforms requiring extended time on wing without compromise.

 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.