Engines

UTG-20N

POWER, CAPABILITY AND CONFIDENCE The UTG-20 is a 20cc single cylinder engine with high power density and minimal maintenance requirements. The engine has excellent reliability and the EFI system maintains optimum engine operating parameters in all regimes of flight. This avoids common flaws of carbureted engines such as icing, top-of-climb engine stalls and incorrect fuel-air ratios. The engine has passed two 150 hour endurance tests (based on the US Federal Aviation Regulation Part 33) without the need for a major overhaul. One of the major advantages with a UTG engine is that it can be supplied as a turnkey system including a generator, isolation mount, low noise exhaust and standard harnesses. The UTG-20 engine is recommended for aircraft with a maximum take-off weight of approx 18kg. The UTG-20 EFI provides drones with increased reliability and power while addressing the shortcomings commonly found in two-stroke engines. The newly designed fuel pump, with self-priming capability, a reliable mechanical fuel pressure regulator precisely controls the fuel pressure. The UTG-20 EFI incorporates the latest engine technology from UTG EFI. Provide RS232 and CANBUS communication protocol to obtain engine running data in real time.

Part Number: UTG-20G
Engine Type: 2-Stroke Single Cylinder Displacement: 20cc
Weight: 1.8kg (engine, generator, integrated exhaust, vibration mount, EFI, Pump and Harness)
Fuel type: Regular Gasoline, Premium Gasoline, Avgas 100LL
Fuel Consumption: 450 g/kWh at cruise Power: 2.1kW (2.8HP) / 9600 RPM

Static Thrust: 6.3kg/100 Meters Altitude Static Thrust: 5.0kg/2000 Meters Altitude Static Bench Propeller: 14×10, 15×8, 16×6,
16×8, 17×6
Lubrication Ratio: 40:1 Temperature Range: -20° to 50°C

 

INCLUSIONS IN THE ENGINE PACKAGE

  • Base engine
  • Custom induction system with manifold and throttle body
  • Miniature Engine Control Unit (ECU)
  • Wiring Harness
  • Self priming fuel pump
  • Atomising fuel injector
  • CDI Ignition
  • Manifold and Cylinder head temperature sensors
  • Generator
  • Engine Isolation Mount
  • Operation and service and ICD manuals

Low Noise, aerodynamically integrated Exhaust

UTG-30N

POWER, CAPABILITY AND CONFIDENCE The UTG-30 is a 30cc single cylinder engine with high power density and minimal maintenance requirements. The engine has excellent reliability and the EFI system maintains optimum engine operating parameters in all regimes of flight. This avoids common flaws of carbureted engines such as icing, top-of-climb engine stalls and incorrect fuel-air ratios. The engine has passed two 150 hour endurance tests (based on the US Federal Aviation Regulation Part 33) without the need for a major overhaul. One of the major advantages with a UTG engine is that it can be supplied as a turnkey system including a generator, isolation mount, low noise exhaust and standard harnesses. The UTG-30 engine is recommended for aircraft with a maximum take-off weight of approx 25kg. The UTG-30 EFI provides drones with increased reliability and power while addressing the shortcomings commonly found in two-stroke engines. The newly designed fuel pump, with self-priming capability, a reliable mechanical fuel pressure regulator precisely controls the fuel pressure. The UTG-30 EFI incorporates the latest engine technology from UTG EFI. Provide RS232 and CANBUS communication protocol to obtain engine running data in real time.

Part Number: UTG-30G

Engine Type: 2-Stroke Single Cylinder Displacement: 30cc

Weight: 2.5kg (engine, generator, integrated exhaust, vibration mount, EFI, Pump and Harness)

Fuel type: Regular Gasoline, Premium Gasoline, Avgas 100LL

Fuel Consumption: 450 g/kWh at cruise Power: 2.8kW (3.8HP) / 8500 RPM

Static Thrust: 8.4kg/100 Meters Altitude Static Thrust: 7.4kg/2000 Meters Altitude Static Bench Propeller: 16×10,17×8,17×10,18×8,18×10

Lubrication Ratio: 40:1 Temperature Range: -20° to 50°

 

INCLUSIONS IN THE ENGINE PACKAGE

  • Base DLE-20
  • Custom induction system with manifold and throttle body
  • Miniature Engine Control Unit (ECU)
  • Wiring Harness
  • Self priming fuel pump
  • Atomising fuel injector
  • CDI Ignition
  • Manifold and Cylinder head temperature sensors
  • Generator
  • Engine Isolation Mount
  • Operation and service and ICD manuals

Low Noise, aerodynamically integrated Exhaust

UTG-55N

POWER, CAPABILITY AND CONFIDENCE The UTG-55 is a 55cc single cylinder engine with high power density and minimal maintenance requirements. The engine has excellent reliability and the EFI system maintains optimum engine operating parameters in all regimes of flight. This avoids common flaws of carbureted engines such as icing, top-of-climb engine stalls and incorrect fuel-air ratios. The engine has passed two 150 hour endurance tests (based on the US Federal Aviation Regulation Part 33) without the need for a major overhaul. One of the major advantages with a UTG engine is that it can be supplied as a turnkey system including a generator, isolation mount, low noise exhaust and standard harnesses. The UTG-55 engine is recommended for aircraft with a maximum take-off weight of approx 40kg. The UTG-55 EFI provides drones with increased reliability and power while addressing the shortcomings commonly found in two-stroke engines. The newly designed fuel pump, with self-priming capability, a reliable mechanical fuel pressure regulator precisely controls the fuel pressure. The UTG-55 EFI incorporates the latest engine technology from UTG EFI. Provide RS232 and CANBUS communication protocol to obtain engine running data in real time.

Part Number: UTG-55G

Engine Type: 2-Stroke Single Cylinder Displacement: 55cc

Weight: 4.1kg (engine, generator, integrated exhaust, vibration mount, EFI, Pump and Harness)

Fuel type: Regular Gasoline, Premium Gasoline, Avgas 100LL

Fuel Consumption: 450 g/kWh at cruise Power: 4.7kW (6.3HP) / 7700 RPM

 

Static Thrust: 8.4kg/100 Meters Altitude Static Thrust: 7.4kg/2000 Meters Altitude Static Bench Propeller: 22×8, 22×10, 23×8, 23×10

Lubrication Ratio: 40:1 Temperature Range: -20° to 50°C

INCLUSIONS IN THE ENGINE PACKAGE

  • Base
  • Custom induction system with manifold and throttle body
  • Miniature Engine Control Unit (ECU)
  • Wiring Harness
  • Self priming fuel pump
  • Atomising fuel injector
  • CDI Ignition
  • Manifold and Cylinder head temperature sensors
  • Generator
  • Engine Isolation Mount
  • Operation and service and ICD manuals

Low Noise, aerodynamically integrated Exhaust

UTG-85N

POWER, CAPABILITY AND CONFIDENCE The UTG-85 is a 85cc single cylinder engine with high power density and minimal maintenance requirements. The engine has excellent reliability and the EFI system maintains optimum engine operating parameters in all regimes of flight. This avoids common flaws of carbureted engines such as icing, top-of-climb engine stalls and incorrect fuel-air ratios. The engine has passed two 150 hour endurance tests (based on the US Federal Aviation Regulation Part 33) without the need for a major overhaul. One of the major advantages with a UTG engine is that it can be supplied as a turnkey system including a generator, isolation mount, low noise exhaust and standard harnesses. The UTG-85 engine is recommended for aircraft with a maximum take-off weight of approx 65kg. The UTG-85 EFI provides drones with increased reliability and power while addressing the shortcomings commonly found in two-stroke engines. The newly designed fuel pump, with self-priming capability, a reliable mechanical fuel pressure regulator precisely controls the fuel pressure. The UTG-85 EFI incorporates the latest engine technology from UTG EFI. Provide RS232 and CANBUS communication protocol to obtain engine running data in real time.

Part Number: UTG-85G

Engine Type: 2-Stroke Single Cylinder Displacement: 85cc

Weight: 5.8kg (engine, generator, integrated exhaust, vibration mount, EFI, Pump and Harness)

Fuel type: Regular Gasoline, Premium Gasoline, Avgas 100LL

Fuel Consumption: 450 g/kWh at cruise Power: 6.6kW (8.9HP) / 7200 RPM

Static Thrust: 12.9kg/100 Meters Altitude Static Thrust: 10.2kg/2000 Meters Altitude Static Bench Propeller: 25×10, 26×9, 27×8

Lubrication Ratio: 40:1 Temperature Range: -20° to 50°C

INCLUSIONS IN THE ENGINE PACKAGE

  • Base
  • Custom induction system with manifold and throttle body
  • Miniature Engine Control Unit (ECU)
  • Wiring Harness
  • Self priming fuel pump
  • Atomising fuel injector
  • CDI Ignition
  • Manifold and Cylinder head temperature sensors
  • Generator
  • Engine Isolation Mount
  • Operation and service and ICD manuals

Low Noise, aerodynamically integrated Exhaust

Scroll to Top