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| Price | $495,000.00 $350,000.00 |
| Our Rating | |
| Brand | Daher Volocopter |
| Category | Flying Vehicles Flying Vehicles |
| Model | Daher EcoPulse VoloCity |
| Manufacturer | Daher (in collaboration with Airbus & Safran) Volocopter GmbH (Germany) |
| Announced | 2019 2019 |
| launched | November 29, 2023 Expected entry into service by 2025 (under certification) |
| Base Price | 4950000 $300,000–$350,000 |
| Aircraft Type | Hybrid-electric distributed-propulsion demonstrator (based on Daher TBM platform) Electric Vertical Take-Off and Landing (eVTOL) air taxi |
| Length | 10.7 m (based on TBM 900) ~9.3 m (30.5 ft) |
| Wingspan / Rotor Diameter | 12.8 m 18 rotors on a circular frame, ~9.3 m overall diameter |
| Height | 4.4 m ~2.5 m (8.2 ft) |
| Empty Weight | ~700 kg (1,543 lbs) |
| Maximum Takeoff Weight (MTOW) | 900 kg (1,984 lbs) |
| Passenger Capacity | 4–6 2 (including pilot, later autonomous) |
| Cargo Capacity | Small luggage compartment (~20–25 kg / 55 lbs) |
| Landing Gear Type | Retractable tricycle gear Fixed skid-type landing gear |
| Battery Type | High-voltage Lithium-ion (800 V DC system) Lithium-ion battery system |
| Battery Capacity | 350 kW ~35 kWh (modular packs) |
| Battery Brand | Airbus Custom aviation-grade packs (partnerships with multiple suppliers, undisclosed) |
| Charging Input Voltage | High-voltage DC charging infrastructure |
| Charging Power | Up to 100 kW (target) |
| Charging Time | Fast swap in minutes / ~60 minutes standard charge |
| Solar / Hybrid Assist | Hybrid system (conventional turboprop + electric motors) battery-electric only |
| Motor | Six wing-mounted Safran electric propellers (e-propulsion units) 18 electric motors (each with its own rotor) |
| Total Power Output | 350 kW combined ~100 kW peak combined |
| Propulsion System | Hybrid configuration combining a turboprop engine, turbogenerator, and distributed electric thrusters Distributed electric propulsion (DEP) with fixed-pitch propellers |
| transmission | Direct-drive electric motors (no gearbox) Direct drive (no mechanical transmission – each motor directly drives a rotor) |
| Cruising speed | ~90 km/h (56 mph) |
| Top Speed | Estimated around 290 km/h (180 mph) 110 km/h (68 mph) |
| Maximum Range | ~35 km (22 miles) |
| Endurance (Flight Time) | Less than 1 hour on battery power alone ~20 minutes (with reserves) |
| Climb Rate | ~6 m/s (1,180 ft/min) |
| Service Ceiling (Max Altitude) | ~2,000 m (6,560 ft) |
| Takeoff / Landing Type | Conventional runway operation Vertical takeoff and landing (VTOL) |
| Noise Level (dB) | Significantly reduced ~65 dB at 75 m (designed for urban low-noise operation) |
| Flight Modes | Hybrid electric and distributed propulsion modes Piloted, semi-autonomous, autonomous (future certification stages) |
| Avionics | Modified Daher TBM avionics with Airbus-developed distributed propulsion management Redundant fly-by-wire control, navigation, and flight management systems |
| Flight Control | Custom software enabling differential thrust for roll and yaw control Triple-redundant autonomous flight control with pilot interface |
| Safety Features |
High-voltage battery management Synchronization of propellers (noise and vibration reduction) Redundant power systems 18 independent motors (fault tolerance) Redundant power distribution Real-time diagnostics Low noise, low vibration design |
| Emergency Landing System | Parachute recovery system (airframe parachute) |
| Certifications | Demonstrator only (not yet certified for production use) Pursuing EASA SC-VTOL and FAA type certification |
| Seating Layout | 4–6 seats 2 seats (side-by-side pilot + passenger) |
| Cabin Type | Pressurized light aircraft cabin Enclosed cabin with wide windows for panoramic views |
| Infotainment & Displays | Minimalistic digital flight display, passenger information screen planned |
| Storage Compartments | Small rear luggage space for carry-on bags |
| Other Features |
Advanced power distribution, hybrid control interface
Climate control Lightweight, ergonomic seating Large windows for sightseeing |
| Passenger Capacity | 4–6 2 (1 pilot + 1 passenger) |
| Payload Capacity | ~200 kg (441 lbs, including passengers + luggage) |
| Cargo Capacity | ~20–25 kg luggage allowance |
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We can not guarantee that the information on this page is 100% correct