

Fuel Consumption
9 l/h
Payload and fuel
60 kg (132 lbs)
Tank Capacity
60 litres (15.8 gallons
Max. flight time
6 hrs
ANAVIA focuses on one key objective: ensuring customer satisfaction through innovative and reliable aircraft. With its endurance, versatility and long range, the HT-100 stands as the best unmanned VTOL system worldwide – ready for
every mission, in every deployment.
For more details:
KEY FEATURES
UNCOMPROMISING SAFETY
- Pre-programmed autorotation with automatic back-up safety eMotor.
- Flight control redundancy with four actuator.
- ADS-B mode S transponder and FLARM system.
- All airframe parachute system and ELT.
- Detect and avoid system.
- Terrain following.
- Front and bottom view FPV cameras.
- Automated RTH and GNSS loss / denied redundancy.
CAREFREE MAINTENANCE AND TRAINING
- All-inclusive maintenance plans structured for fixed price, ease of maintenance – ensures maximum uptime
with parts provided before they are required. - AMMs and all technical documentation written to a manned aircraft certification standard.
- Customer tailored flight and maintenance training and services.
EFFICIENT FLETTNER ROTOR SYSTEM
- Highest efficiency with no tail rotor compensation.
- 30% energy saved for heavy payloads or longer flight missions.
- Highest stability in demanding flight conditions.
- No mechanical parts in tail boom, removable for easy transport and deck storage.
PERFORMANCE 15 KW TURBINE ENGINE
- High-performance Swiss designed and built helicopter grade turbine engine.
- Long endurance with 9 liter per flight hour Jet-A1, JP-5, JP-8.
- Lowest vibration especially when compared to wankel / piston engines.
- Low maintenance given circumferential lubrication and high reliability with a 1,000 FH TBO.
SPECIFICATIONS
Turbine | 15 kw shaft turbine |
Rotor | Flettner double rotor system |
Typical empty weight | 60kg (132 lbs) |
Tank Capacity | 60 litres (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 | 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 | 60 kg (132 lbs) |
Max. flight time | 6 hrs |
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) |
Operating ceiling (max. density altitude) | 4,000 m (13,123 ft) |
DIMENSIONS
Rotor diameter | 3,75 m (12,3 ft) |
Dimensions L/W/H (excluding rotors) | 2.82 m x 0.72 m x 1.00 m (9.25 ft x 2.36 ft x 3.28 ft) |
HT-100 Video
