Cutting-Edge Propulsion Systems for Mission-Critical UAVs & Advanced Unmanned Technology
TOA 330 / TOA 330 SDI Twin opposed-piston air-cooled 330 cc UAV engine with gasoline & heavy fuel options
TOA 330 / TOA 330 SDI

Twin opposed-piston air-cooled 330 cc UAV engine with gasoline & heavy fuel options

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TOA 330 / TOA 330 SDI

Suter's TOA 330 is a twin opposed-piston air-cooled engine designed for mid-sized UAV platforms. With low vibration and smooth operation, it offers excellent endurance and payload performance, and is available in gasoline and heavy fuel variants.

The TOA 330 family is easy to integrate and features ECU-managed fuel injection and ignition with built-in altitude compensation, cold start support and over-temperature protection. It is ideal for civilian fixed-wing mapping and surveying UAVs, as well as for long-endurance tactical and security platforms.

Specifications:

TOA 330

TOA 330 SDI

Dimensions (L x W x H):

253 × 453 × 285 mm

Weight:

8.5 kg engine

+ 1.8 kg exhaust & silencer

+ 1.5 kg 1 kW / 28 VDC regulator

+ 1.5 kg generator 1 kW

8.8 kg engine

+ 1.8 kg exhaust & silencer

+ 1.5 kg 1 kW / 28 VDC regulator

+ 1.5 kg generator 1 kW

Power Output:

21.5 kW at 6,750 rpm (29.2 hp)

33.4 Nm at 6,000 rpm

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)

Fuel Efficiency:

325 g/kWh BSFC

305 g/kWh BSFC

Service Ceiling:

20,000 ft (6,100 m)

Fuel:

Min. 95RON (91 MON MOGAS) or AVGAS LL100

All kerosene-based fuels e.g Jet-A1, JP-5, JP-8

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