Single-Seat Amphibious Ultralight eVTOL with 6-Rotor Redundant Safety and Dual Refueling for Land & Water Operations
Product Details
| Capacity: | 1 Pilot Only | Empty Weight: | 115 Kg |
|---|---|---|---|
| Maximum Takeoff Weight: | 200 Kg | Max Useful Load: | 85 Kg |
| Maximum Flight Speed: | 100 Km/h | Airframe Material: | Aviation-grade Aluminum Alloy + Carbon Fiber Composite |
Product Description
| Specification | Details |
|---|---|
| Capacity | 1 pilot only |
| Empty Weight | 115 kg |
| Maximum Takeoff Weight (MTOW) | 200 kg |
| Max Useful Load | 85 kg (pilot + carry-on payload) |
| Layout | 6-rotor distributed electric propulsion configuration |
| Maximum Level Flight Speed | 100 km/h |
| Airframe Material | Aviation-grade aluminum alloy + carbon fiber composite |
| Flight Test Record | Over 500 cumulative flight hours; scheduled for formal delivery in 2027 |
| Regulatory Classification | Ultralight aircraft compliant with CCAR-91 |
| Overseas Price | Below USD 120,000 per unit |
Pure lithium battery fully electric power system supporting dual energy replenishment modes:
- Standard Mode: Onboard direct fast charging via charging port
- Commercial Operation Mode: Modular quick-detachable battery packs for hot swap - full battery replacement completed within 3 minutes
Positioned for short-duration low-altitude experience flights with endurance ranging from 5 to 30 minutes per full battery cycle.
- Six independent rotor-motor redundant propulsion system maintains stable controlled descent even with multiple motor failures
- Dual amphibious safety design with streamlined boat-shaped hull plus buoyancy pontoons for stable water operations
- Automatic righting mechanism prevents capsizing after ditching
- Fully enclosed crash-resistant cockpit with passive energy-absorbing structure
- Supports fully automatic vertical takeoff, landing and autonomous return-to-home flight
- Differentiated market positioning focusing on high-realization-value segments
- Ultra-low compliance threshold as ultralight aircraft
- High mobility & site adaptability with compact size for road transportation
- No large-scale dedicated heliport infrastructure required
- Flight control and power systems iterated from aerospace-grade technical architecture
- Intelligent assisted flight logic reduces training expenses
- Simple mechanical structure results in low failure rate and minimal maintenance
- Optimized for global export with completed certification layouts
- Tourism & Leisure: Scenic area aerial sightseeing, lake surface flight experience
- Government & Public Service: Water resource inspection, wildfire patrol, search and rescue
- Aviation Sports: Private recreational flight, flight school practical training
- Overseas Commercial Operation: Island sightseeing fleets for tourist destinations
- Single-seat layout cannot carry additional passengers
- Pure electric configuration limits flight endurance for short-distance flights only
- 100 km/h cruising speed not suitable for long-range intercity air commuting
6-rotor redundant safety | Charge & 3-min battery swap dual refueling | Land & water dual takeoff/landing | Ultralight easy certification | Ideal for sightseeing, patrol and emergency response operations
Product Highlights
Single-Seat Amphibious Ultralight eVTOL R1: 6-rotor redundant safety, dual refueling (charge & 3-min battery swap), land & water takeoff/landing. Ultralight classification enables easy certification. Ideal for sightseeing, patrol, and emergency response operations.
Single-Seat Amphibious Ultralight eVTOL with 6-Rotor Redundant Safety and Dual Refueling for Land & Water Operations
Single-Seat Amphibious Ultralight eVTOL R1: 6-rotor redundant safety, dual refueling (charge & 3-min battery swap), land & water takeoff/landing. Ultralight classification enables easy certification. Ideal for sightseeing, patrol, and emergency response operations.
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