TOA 288

COMPACT
FUEL EFFICIENT

Mid-range 16–24 hp UAV engine, twin-opposed two-stroke, air-cooled. Gasoline baseline of the 288 platform.

SWISS MADE

The TOA 288 is the starting point of the 288 platform family. Designed as a lightweight, compact gasoline engine, it delivers stable mid-range propulsion for civil UAVs. Its air-cooled twin-opposed design ensures simplicity and performance in fixed-wing applications.


Civil Applications: Survey drones, training UAVs, light mapping aircraft.
Dual-Use Applications: Entry-level sensor-based platforms and training drones (gasoline baseline version).

KEY FEATURES

  • Proven Baseline
  • Foundation of the 288 platform, extending to heavy-fuel and water-cooled variants.
  • Balanced Power
  • 16–24 hp output for medium UAV platforms requiring efficient cruise and endurance.
  • Lightweight Construction
  • Low engine mass supporting maximum payload efficiency and extended mission duration.
  • Air-Cooled Design
  • Air-cooled simplicity for fixed-wing and light UAVs

TECHNICAL SPECIFICATIONS

TOA 288 (Gasoline, Air-Cooled)

Parameter Value
Fuel Efficiency 325 g/kWh (BSFC)
Service Ceiling 20,000 ft (6,100 m)
Displacement 288 cc
Configuration Twin-opposed, two-stroke
Power Output 17.6 kW at 6,500 rpm (23,6 HP)
27.2 Nm Torque at 6,000 rpm
Weight 7.8 kg engine*
+ 1.8 kg exhaust
+ 1.5 kg 1 kW / 28 VDC regulator
+ 1.5 kg generator 1 kW
Cooling Air-cooled
Fuel Min. 95RON (91 MON MOGAS) or AVGAS LL100
Management & Control ECU / 12V system, automatic
Ignition System CDI (Capacitor Discharge Ignition)
Mixture 1:60 (1,6 %) 2-stroke oil API TC
Dimensions 253 × 239 × 285 mm (L × W × H)

POSITIONING

The TOA 288 is the lightweight entry into the 288 family optimized for civil UAVs needing reliable, most fuel efficient mid-range propulsion.

 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.