6-Passenger Compound Wing eVTOL Aircraft VE25-100 with 6-Seat Cabin, 235 km/h Cruising Speed, and 200-400 km Flight Range
Product Details
| Cabin Configuration: | 6 Seats (1 Pilot + 5 Passengers) | Fuselage Length: | 9.5 M |
|---|---|---|---|
| Wingspan: | 16.0 M | Maximum Take-off Weight: | 2,500 Kg |
| Maximum Payload: | 500 Kg | Cruising Speed: | 235 Km/h |
| Standard Flight Range: | 200-400 Km (nominal Range: 250 Km) | Service Ceiling: | 3,000 M |
| Power System: | 8 Distributed Permanent Magnet Motors (6 Lift Motors For Vertical Takeoff & Landing, 2 Thrust Motors For Cruising) With Triple-redundant Fly-by-wire Flight Control System | Battery Specification: | High-nickel Ternary Lithium Battery With An Energy Density Of 285 Wh/kg, Supporting 3C Fast Charging |
Product Description
| Parameter | Technical Data |
|---|---|
| Cabin Configuration | 6 seats (1 pilot + 5 passengers) |
| Fuselage Length | 9.5 m |
| Wingspan | 16.0 m |
| Maximum Take-off Weight | 2,500 kg |
| Maximum Payload | 500 kg |
| Cruising Speed | 235 km/h |
| Standard Flight Range | 200-400 km (nominal range: 250 km) |
| Service Ceiling | 3,000 m |
| Power System | 8 distributed permanent magnet motors (6 lift motors for vertical takeoff & landing, 2 thrust motors for cruising) with triple-redundant fly-by-wire flight control system |
| Battery Specification | High-nickel ternary lithium battery with an energy density of 285 Wh/kg, supporting 3C fast charging |
| Crosswind Resistance | 15 m/s |
| Safety Design Standard | Civil aviation-level failure probability of 10⁻⁹ |
| Energy Replenishment Mode | High-power DC fast charging as the primary solution; modular battery packs are detachable for maintenance-level replacement instead of rapid station swap for flight turnaround |
Eight independent motors operate separately. The aircraft can complete safe emergency landing even if a single propeller or motor malfunctions, fully complying with strict civil aviation airworthiness verification standards equivalent to trunk airliners.
Vertical lift is provided by multi-rotor units during takeoff and landing, while fixed wings generate aerodynamic lift in cruising phase. This design delivers outstanding crosswind resistance and stall prevention capability, enabling all-weather operation under complex meteorological conditions.
- Spacious 6-seat cabin with large payload capacity, accommodating medical stretchers for flexible switching among passenger transport, emergency rescue and light cargo delivery scenarios
- At a cruising speed of 235 km/h, covers 20 km within only 5 minutes, delivering 3 to 5 times higher travel efficiency than ground transportation
- Excellent aerodynamic efficiency significantly cuts energy consumption during fixed-wing cruising, achieving longer flight range than pure multi-rotor counterparts
The aircraft is applicable to diverse commercial and public service fields, including urban air mobility, intercity short-haul transportation, island shuttle services, low-altitude tourism, medical emergency rescue, forest fire prevention and light air logistics.
The fully electric propulsion system realizes zero local emissions. Flight noise is far lower than conventional helicopters, allowing compliant operation over urban core areas and residential zones.
- Matched with dedicated aviation fast chargers: battery can be charged to 85% capacity within 25 minutes and fully charged in 40 minutes
- Infrastructure investment is much lower than rapid battery swap stations, ideal for regular route operation at urban vertiports
This aircraft does not support minutes-level rapid battery swapping between consecutive flights. Battery pack disassembly and replacement belong to standard maintenance operations, mainly applied in two scenarios:
- Full battery replacement when the battery reaches its designed service life of around 1,000 charge-discharge cycles
- Replacement with high-energy-density customized battery packs to extend flight range for long-distance mission requirements
Average power consumption ranges from 75 kWh to 85 kWh per 100 kilometers:
- Off-peak industrial electricity price (0.4 USD/kWh equivalent): approx. USD 32 per 100 km
- Peak industrial electricity price (1.2 USD/kWh equivalent): approx. USD 96 per 100 km
The per-seat energy cost is merely 1/10 of the fuel expense of traditional helicopters.
The battery system accounts for roughly 30% of the total aircraft procurement cost. Under regular commercial operation with 3-4 flight segments daily, full battery replacement will be required every 3 years on average after around 1,000 charge cycles.
Regular monthly visual inspections, flight control calibration and motor insulation tests are mandatory. The overall mechanical maintenance cost is only 20% of that of conventional helicopters. Annual labor and spare parts maintenance expense accounts for 2.5% to 3.5% of the aircraft's total purchase price.
Major soft costs include professional pilots and certified maintenance technicians. Annual aviation liability insurance costs roughly 1.5%-2% of the aircraft value, alongside vertiport rent, charging facility maintenance and utility fees.
For large-scale fleet deployment, the comprehensive operating cost per seat per kilometer falls between USD 0.8 and USD 1.5. Economic analysis shows positive financial returns can be achieved with a daily flight duration of 4 hours or above.
- The all-electric design removes routine engine oil changes, piston overhauls and transmission maintenance
- Triple-redundant system and modular component design enable quick plug-and-play replacement of faulty units
- High component localization ensures competitive spare part pricing and short delivery lead times
Product Highlights
6-passenger compound wing eVTOL with 235 km/h cruising speed, 250 km range, and civil aviation-level safety. Features 8 redundant motors, triple-redundant flight control, and 350 kW DC fast charging. Offers low noise, zero emissions, and operating costs 1/10 of traditional helicopters for urban air mobility and emergency services.
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