- Home
- Electric Vehicles
- Compare
- Supernal S-A2 vs SkyDrive SD-05
Supernal S-A2 vs SkyDrive SD-05
Overview Electric Flying Vehicle
|
Model
|
Supernal S-A2
SD-05 |
|
Manufacturer
|
Supernal (Hyundai Motor Group)
SkyDrive Inc. (Japan) |
|
Announced
|
2024
2022 |
|
launched
|
Expo 2025 (public display & demo flights) |
|
Base Price
|
3000000
|
Electric Flying Vehicle Dimensions & Build
|
Aircraft Type
|
eVTOL (urban air mobility air taxi)
Passenger eVTOL (multicopter / flying car) |
|
Length
|
~11.5 m |
|
Wingspan / Rotor Diameter
|
Eight tilt rotors on fixed wing structure
11.3 m (including rotors) |
|
Maximum Takeoff Weight (MTOW)
|
1,400 kg (3,100 lbs) |
|
Passenger Capacity
|
1 pilot + 4 passengers (5 total)
3 (1 pilot + 2 passengers) |
|
Cargo Capacity
|
Modular interior supports light cargo configuration
Small luggage only |
|
Landing Gear Type
|
Fixed tricycle wheeled gear
Fixed skids with stabilizing fins |
Power & Propulsion
|
Battery Type
|
High-voltage lithium-based electric pack
Electric (chemistry not disclosed) |
|
Solar / Hybrid Assist
|
fully electric
None (battery only) |
|
Motor
|
8 independent electric tilt rotors
12 electric motors / 12 propellers |
|
Propulsion System
|
Distributed Electric Propulsion
Distributed Electric Propulsion (DEP) |
|
transmission
|
Direct-drive electric
Direct drive |
Electric Flying Vehicle Performance
|
Cruising speed
|
120 mph (193 km/h)
~100 km/h |
|
Top Speed
|
160 mph
~100 km/h |
|
Maximum Range
|
60 miles
15 km (future goal: 30–40 km) |
|
Endurance (Flight Time)
|
5–10 minutes |
|
Service Ceiling (Max Altitude)
|
1,500 ft AGL
|
|
Takeoff / Landing Type
|
Vertical (VTOL)
VTOL |
|
Noise Level (dB)
|
65 dBA in hover / < 45 dBA in cruise
|
|
Flight Modes
|
Piloted initially; autonomous planned
Piloted with stability assist; remote piloting possible |
Safety & Systems
|
Avionics
|
IFR-capable flight suite
|
|
Flight Control
|
Redundant distributed electric system
Computer-controlled stability system |
|
Safety Features
|
Composite airframe, multi-rotor redundancy, energy-absorbing structure
Redundant motors (DEP), lightweight composite structure |
|
Emergency Landing System
|
Full-aircraft ballistic parachute planned
|
|
Certifications
|
FAA and EASA certification in progress
Under JCAB (Japan) & FAA (US) certification process |
Interior & Comfort
|
Seating Layout
|
pilot + 4 passengers (luxury cabin)
1 pilot front, 2 passengers rear |
|
Cabin Type
|
Automotive-inspired interior with large panoramic windows
Enclosed, panoramic windows |
|
Infotainment & Displays
|
Minimalist digital cockpit and passenger information panels
|
|
Storage Compartments
|
Luggage and carry-on spaces behind seats
Small luggage space |
|
Other Features
|
Energy-absorbing seats, ambient lighting, advanced noise insulation
Large windows, carbon fiber/aluminum build, rooftop/vertiport use |
Capacities
|
Passenger Capacity
|
4 (+ pilot)
3 (1 pilot + 2 passengers) |
|
Payload Capacity
|
400 kg
|
Disclaimer Note
We can not guarantee that the information on this page is 100% correct
