The ANAVIA HT-750 redefines unmanned aerial operations with its unmatched endurance, heavy payload capacity, and long-range capabilities. Designed for missions traditionally flown by manned helicopters, this Swiss-engineered VTOL system delivers superior intelligence, surveillance, and reconnaissance (ISR), cargo transport, and multi-mission adaptability.
MTOW
1,150 kg
Endurance
15 hrs
Speed
Up to 222 km
Tank Capacity
900 litres
Unrivalled Heavy-Lift Capability
- Carries payloads up to 750 kg, setting a new benchmark in unmanned aviation.
- Long-range autonomous operations, ideal for ISR, logistics, and tactical deployments.
- Optimised for extreme conditions, ensuring mission success in demanding environments.
Next-Generation ISR & Mission Flexibility
- Advanced sensor integration: EO/IR, SAR, SIGINT, LiDAR, and hyperspectral imaging.
- Autonomous multi-role operations for defence, border security, disaster response, and more.
- High-performance Swiss engineering, ensuring reliability, precision, and efficiency.
Built for Global Deployments
- Designed and manufactured in Switzerland, with an uncompromising focus on quality.
- Robust airframe and rotor system, ensuring safety and stability in the toughest conditions.
- Multi-mission versatility, ready to excel in military, commercial, and humanitarian operations.
The HT-750 is the ultimate heavy-lift unmanned VTOL system, delivering next-level capability, endurance, and mission success—whenever and wherever it's needed.
FEATURES
- Advanced Power Systems
- Rotor Efficiency
- Onboard Avionics
- Payload Support
- Maritime Ready
- Data Communication
- Safety
- Swiss Quality
TECHNICAL DATA
| Turbine | Gas turbo-shaft engine |
| Rotor | Semi-rigid 4-blade bearing-less rotor system |
| Typical empty weight | XX |
| Tank Capacity | 900 litres (238 gallons) |
| Fuel Types | Jet A1 – other fuel types on demand (JP-8, JP-5) |
| Fuel Consumption | 60 l/h |
| Data link type | Fully encrypted MESH IP (limitless SATCOM, dual MIMO radios with up to 100 Mbps data rate and AES256 encryption) |
| Data link range | Dependant on terrain topography and national regulations - radio and antenna configuration up to 200 km |
| 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
| Payload and fuel | 750 kg (1,654 lbs) |
| Max. flight time | 15 hrs |
| Max. airspeed | 222 km/h (119 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 | 1,150 kg (2,536 lbs) |
| Operating ceiling (max. density altitude) | 4,000 m (13,123 ft) |
DIMENSIONS
| Rotor diameter | 7.50 m (24.06 ft) |
| Dimensions L/W/H (excluding rotors) | 6.88 m x 1.67 m x 3.35 m (22.57 ft x 5.47 ft x 10.99 ft) |