The ANAVIA HT-100 Naval unmanned helicopter brings all the performance, endurance and efficiency advantages of the HT-100 but with a configuration for the unique conditions of maritime deployment. Ruggedised with corrosion protection and equipped with a fully autonomous, state-of-art deck landing system.
By combining the most advanced sensor technologies with a heavy payload capacity, we offer a safe, reliable solution that can outperform manned rotary-winged aircraft in sea conditions that are often harsh and complex.
With the cell and rotor blades constructed of innovative lightweight carbon, and incorporating decades of aerospace and motorsport technologies, the HT-100 Naval sets new benchmarks for autonomous flying, with a 15 kW turbine engine, flight time of 360 minutes, and air load of up to 60 kg.
Advanced technology systems include dual inter-meshing Flettner main rotors that support large payloads and flight stability, a powerful reliable 15 kW backup electric drive, and an intelligent redundancy system for uncompromising safety.
- Fully autonomous landing system
- Equipped with Harpoon, Floats, ELT
- Efficient dual inter-meshing Flettner main rotors (no tail rotor, less vibration)
- Full high-tech carbon composite structure for longevity and high-performance
- Diverse digital data link options: terrestrial (up to 200km) / optional LTE / Satcom
- Flight control redundancy with four actuators
- Autonomous deck-landing system
- Corrosion protection
- Low maintenance, high reliability
- Turbine JET A-1 powered engine
- Autorotation capability
- ITAR free
TECHNICAL DATA
| Turbine | 15 kW shaft turbine |
| Rotor | Flettner double rotor system |
| Typical empty weight | 66 kg (145 lbs) |
| Tank capacity | 60 liters (15.8 gallons) |
| Fuel types | Jet A1 – other fuel types on demand (JP-8, JP-5) |
| Fuel consumption | 9 l/h |
| Data link type | Fully encrypted MESH IP (SATCOM and LTE on demand) |
| Data link range | Radio and antenna configuration up to 200 km (depending on terrain topography and national regulations) |
| Operating temperature | -25 °C to +55 °C, -13 °F to +131 °F |
| Max. wind speed | 45 km/h (25 kn) |
| Start and landing | Fully autonomous |
PERFORMANCE
| Max. payload and fuel | 60 kg (132 lbs) |
| Max. flight time | 360 minutes |
| Max. airspeed | 120 km/h (65 kn) |
| Max. flight mission/ payload weight | 1 hrs / 43 kg, 2 hrs / 35 kg, 4 hrs / 22 kg, 6 hrs / 9 kg |
| Max. take-off weight | 120 kg (264 lbs) |
| Operating ceiling | (max. density altitude) 4,000 m (13,123 ft) |
DIMENSIONS
| Rotor diameter | 3.75 m (12.00 ft) |
| Dimensions (excluding rotors) L / W / H | 2.82 m (9.25 ft) x 0.72 m (2.36 ft) x 1.00 m (3.28 ft) |