Payload and fuel
750kg (1,654 lbs)
Max. flight time
15 hrs
Max. airspeed
222km/h (119 kn)
Operating ceiling: (max. density altitude)
4,000 m (13,123 ft)
ANAVIA focuses on one key objective: ensuring customer satisfaction through innovative and reliable aircraft. With its endurance, cargo capacity and long range, the HT-750 stands as the world’s leading heavy-lift unmanned VTOL system – ready for every mission, in every deployment.
For more details:
KEY FEATURES:
ADVANCED POWER SYSTEMS
- Hybrid Assistant System (HAS) ensures safety during turbine power loss
- Autonomous electric rotor power
- Gas turboshaft engine
- 250 SHP take-off power
- 230 SHP max continuous power
ONBOARD AVIONICS
- Custom-built avionics
- Safe and precise operations
- Integrated GPS/inertial navigation
- Real-time diagnostics and autopilot capabilities
MARITIME READY
- Fully autonomous deck landing system
- Harpoon landing (NATO Grid)
- Optional emergency floatation devices
SAFETY
- Redundancy (GPS; DATA-Link; DAAS; ADS-B; key sensorics, as in manned aviation)
- Anti-jamming GPS protection
- Radar altimeter
ROTOR EFFICIENCY
- Semi-rigid 4-blade bearing-less rotor system
- Optimised for performance and durability
- Low maintenance service costs
PAYLOAD SUPPORT
- Manned-aviation grade sensors
- Cargo compartments
- Medical evacuation equipment
- Troop insertion
DATA COMMUNICATION
- Data link up to 200 km
- Limitless SATCOM
- Dual MIMO radios (up to 100 Mbps data rate and AES256 encryption)
SWISS QUALITY
- Durable lightweight materials
- Reliability, performance
- Low maintenance costs
- Customer support services
SPECIFICATIONS
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 weigh | 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) |