Technical description
Performance
- Endurance
- 8 hours with full ISR payloads
- Payloads
- Rapid role change, mult. payloads
- Maximum speed
- 185 km/h I 100kt
- Ceiling
- 6,000 m
Dimensions
- Length
- 6.2 m
- Height
- 2.28 m
- Main rotor diameter
- 7.2 m
Characteristics
- Propulsion
- Aviation-certified engine
- Propulsion
- Diesel fuel & jet fuel
- Maximum takeoff weight
- 760 kg
- Max wind for takeoff & landing
- 74 km/h I 40 Kt
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