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| Price | $126,000.00 $280,000.00 |
| Our Rating | |
| Brand | XPeng Xpeng AeroHT |
| Category | Flying Vehicles Flying Vehicles |
| Model | XPeng AeroHT Voyager X2 Xpeng Land Aircraft Carrier (LAC) |
| Manufacturer | XPeng AeroHT Xpeng AeroHT (a subsidiary of XPENG Motors) |
| Announced |
2021 October 2023 |
| launched | 2024 November 2024 (first public flight demo), Prototype / Pre-production (mass production targeted for 2026) |
| Base Price | 126000 ¥2,000,000 (CNY) ≈ $280,000 USD |
| Aircraft Type | Electric eVTOL multicopter Modular two-part flying car (ground “mothership” + detachable air module) |
| Length | 5.17 m 5.5 m (ground vehicle), 2.0 m (ground vehicle) |
| Wingspan / Rotor Diameter | 5.12 m |
| Height | 1.36 m |
| Empty Weight | 560–680 kg (varies by source) |
| Maximum Takeoff Weight (MTOW) | 760 kg |
| Passenger Capacity | 2 Ground Module: 4 persons Air Module: 2 persons (pilot + passenger) |
| Cargo Capacity | 200 kg (combined payload) Large internal bay for air module and storage |
| Landing Gear Type | Fixed skid landing gear Retractable landing struts (air module) |
| Battery Type | Fully electric lithium-based pack 800-V high-voltage lithium-based system |
| Charging Input Voltage | 800 V |
| Charging Power | Fast charging (air module 30 % → 80 % in ~18 min via ground vehicle) |
| Charging Time | Fast – ~18 min |
| Solar / Hybrid Assist | None (pure electric) Ground module uses hybrid EREV (range-extender engine) |
| Motor |
8 electric motors (octocopter) Air module: 8 electric motors (6 rotors + 2 ducted fans) |
| Propulsion System | 8 individual propellers (direct-drive) Electric vertical take-off & landing (VTOL) + forward ducted-fan propulsion |
| transmission | Direct electric drive (no gearbox) Direct electric drive |
| Top Speed | 130 km/h |
| Maximum Range | Ground Module: ≈ 1,000 km (CLTC, hybrid system) Air Module: Supports 5 – 6 flights per full charge |
| Endurance (Flight Time) | 35 minutes |
| Service Ceiling (Max Altitude) | 1,000 m |
| Takeoff / Landing Type | Vertical Takeoff and Landing (VTOL) VTOL (vertical take-off & landing) |
| Flight Modes | Manual flight + Autonomous mode Manual / Autonomous hybrid control |
| Avionics | Basic navigation + autonomous systems (details not public) Multi-source navigation + electronic geofencing |
| Flight Control | Autopilot & manual control options Triple-redundant fly-by-wire system |
| Safety Features |
8-motor redundancy Emergency ballistic parachute Ground/environment sensing Real-time monitoring (4G/5G) Parachute recovery system (for up to 1,000 kg) Redundant motors (can sustain flight with 2 motors failed) Automated stability control |
| Emergency Landing System | Parachute-based system Integrated parachute + auto-hover descent |
| Certifications | Test-flight approvals in China (not yet commercially certified) Type certification process accepted by CAAC (China Civil Aviation Authority) |
| Seating Layout | 2 seats side-by-side Ground Module: 4 seats Air Module: 2 seats |
| Cabin Type | Fully enclosed cockpit Enclosed panoramic canopy (270° visibility) |
| Infotainment & Displays | Minimal controls, flight screens (limited details) Digital instrument panels |
| Storage Compartments | Small rear/luggage area Rear bay and roof mount for air module equipment |
| Other Features |
Aerodynamic teardrop body Foldable structure for easier storage/parking Automatic air module deployment via rear-loading system Sliding rail system and foldable rotor arms |
| Passenger Capacity | 2 Up to 6 (4 ground + 2 air) |
| Payload Capacity | 200 kg |
| Cargo Capacity | Large |
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We can not guarantee that the information on this page is 100% correct