The ANAVIA HT-100 is a long-range, heavy-lift unmanned aerial vehicle (UAV) designed for autonomous flight operations across multiple industries. As a VTOL aircraft with an intermeshing rotor system, it offers exceptional stability, efficiency, and modularity, making it the ideal UAV for intelligence, surveillance, and reconnaissance (ISR), commercial logistics, search & rescue, infrastructure inspection, and photometry.
Replacing Manned Helicopters with Unmatched Efficiency
Built to take over missions traditionally flown by manned helicopters, the HT-100 delivers the same grade of ISR equipment, cargo capacity, and multi-mission payloads—but at a fraction of the cost.
- Swiss-engineered 15 kW turbine engine consumes just 9 l/h of JET A-1, JP-5, or JP-8 fuel, ensuring operational efficiency.
- Endurance of up to 6 hours per mission with a maximum payload of 60 kg.
- Cruise speed of 100 km/h, maintaining performance in extreme weather.
- 600 km maximum range while still carrying a 23 kg payload, making it the market leader in sensor payload capacity.
- Modular ‘plug & play’ avionics ensure seamless sensor and equipment integration for any mission.
The ANAVIA HT-100 sets a new benchmark for autonomous UAV operations, combining power, endurance, and adaptability to redefine unmanned aerial missions.
- 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
- 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 | 65 kg (143 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. flight time | 360 minutes |
| Max. airspeed | 120 km/h (65 kn) |
| Max. flight mission/ payload weight | 1 hrs / 51 kg, 2 hrs / 43 kg, 4 hrs / 28 kg, 6 hrs / 14 kg |
| Max. take-off weight | 120 kg (264 lbs) |
| Max. payload and fuel | 55 kg (121 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) |