UAV Engine

VRON‑66CC Twin‑Cylinder Two‑Stroke Engine

UAV Engine

nord defense

Technical Specifications

Configuration Project

Parameter

Output Power

8HP

Idle Speed

1500 rpm/min

Static Thrust (100m Altitude)

15.5kg

Static Thrust (1800m Altitude)

13.6kg

Recommended Propeller

22×10; 23×10; 24×8

Spark Plug Type

BM6A

Bore × Stroke

38mm × 30mm

Compression Ratio

7.6:1

Lubrication Ratio

30:1

Maximum Fuel Consumption

3L/h

Main Engine Weight

1520g

Exhaust Weight

90g

Ignition Weight

120g

Ignition Voltage

6V-14.4V

Overall Dimension (L×W×H)

220×165×190mm (±10mm)


label: Engine

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