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- Daher EcoPulse
Daher EcoPulse
- Battery Capacity: 350 kW
- Propulsion System: Hybrid configuration combining a turboprop engine, turbogenerator, and distributed electric thrusters
- Service Ceiling (Max Altitude):
- Takeoff / Landing Type: Conventional runway operation
PROS
- Pioneering Hybrid Technology: First distributed-propulsion hybrid-electric aircraft demonstrator in its class.
- Reduced Emissions: Combines conventional fuel with electric thrust to cut COâ‚‚ output significantly.
- Noise Reduction: Distributed e-propellers and synchrophasing greatly lower cabin and external noise.
- Collaborative Innovation: Joint development by Daher, Airbus, and Safran—leaders in aviation technology.
- Scalable Concept: Research supports future hybrid and fully electric commercial aircraft designs.
CONS
- Prototype Only: Not available for commercial or passenger use.
- Limited Endurance: Less than 1 hour on electric power—unsuitable for long missions.
- Incomplete Specs: Many operational and weight details remain undisclosed.
- Charging Details Unknown: Real-world recharging and energy recovery data not public.
- Complexity: Hybrid systems add significant engineering and maintenance challenges.
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Full Specifications
Overview Electric Flying Vehicle
| Model | Daher EcoPulse |
| Manufacturer | Daher (in collaboration with Airbus & Safran) |
| Announced | 2019 |
| launched | November 29, 2023 |
| Base Price | 4950000 |
Electric Flying Vehicle Dimensions & Build
| Aircraft Type | Hybrid-electric distributed-propulsion demonstrator (based on Daher TBM platform) |
| Length | 10.7 m (based on TBM 900) |
| Wingspan / Rotor Diameter | 12.8 m |
| Height | 4.4 m |
| Passenger Capacity | 4–6 |
| Landing Gear Type | Retractable tricycle gear |
Power & Propulsion
| Battery Type | High-voltage Lithium-ion (800 V DC system) |
| Battery Capacity | 350 kW |
| Battery Brand | Airbus |
| Solar / Hybrid Assist | Hybrid system (conventional turboprop + electric motors) |
| Motor | Six wing-mounted Safran electric propellers (e-propulsion units) |
| Total Power Output | 350 kW combined |
| Propulsion System | Hybrid configuration combining a turboprop engine, turbogenerator, and distributed electric thrusters |
| transmission | Direct-drive electric motors (no gearbox) |
Electric Flying Vehicle Performance
| Top Speed | Estimated around 290 km/h (180 mph) |
| Endurance (Flight Time) | Less than 1 hour on battery power alone |
| Takeoff / Landing Type | Conventional runway operation |
| Noise Level (dB) | Significantly reduced |
| Flight Modes | Hybrid electric and distributed propulsion modes |
Safety & Systems
| Avionics | Modified Daher TBM avionics with Airbus-developed distributed propulsion management |
| Flight Control | Custom software enabling differential thrust for roll and yaw control |
| Safety Features |
High-voltage battery management Synchronization of propellers (noise and vibration reduction) Redundant power systems |
| Certifications | Demonstrator only (not yet certified for production use) |
Interior & Comfort
| Seating Layout | 4–6 seats |
| Cabin Type | Pressurized light aircraft cabin |
| Other Features | Advanced power distribution, hybrid control interface |
Capacities
| Passenger Capacity | 4–6 |
Reviews
Disclaimer Note
We can not guarantee that the information on this page is 100% correct
