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Supernal (Hyundai Motor Group) · USA
S-A2
Supernal (Hyundai Motor Group) S-A2
矢量推力 · 概念设计 · 核查 2026-10-01
下列为 VFS 目录披露的参数，包含设计目标及历史版本信息。目录阶段不等于适航或量产状态；不同任务条件的航程与载荷不能直接当作同一条件下的性能。
主要参数
- 座位／载员
- 未公开／未录入
- 乘客
- 4 seats for a luxury ride (no middle seat) with enough space for baggage. The interior can be easily switched from 4 passengers, to 2 passengers and to cargo-only flights.
- 驾驶方式
- 1 pilot, will be initially piloted and will transition into an autonomous aircraft
- 航程（按来源口径）
- 未公开／未录入
- 巡航速度
- 未公开／未录入
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 未公开／未录入
- 载荷
- 未公开／未录入
- 空重
- 未公开／未录入
- 长度
- 未公开／未录入
- 翼展
- 未公开／未录入
- 高度
- 未公开／未录入
- 动力来源
- 未公开／未录入
- 电机
- 8 electric motors
- 旋翼／螺旋桨
- 8 tilt-propellers
- 续航时间
- 未公开／未录入
- 飞行高度
- 未公开／未录入
- 安全设计
- Distributed Electric Propulsion (DEP) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for its passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy for its passengers or cargo. Having multiple redundant systems on any aircraft decreases having any single point of failure. The aircraft is certified for Instrument Flight Rules (IFR). There is a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency.
全部原始参数
Specifications:
- Aircraft type
- Passenger eVTOL concept design aircraft
- Piloting
- 1 pilot, will be initially piloted and will transition into an autonomous aircraft
- Passengers
- 4 seats for a luxury ride (no middle seat) with enough space for baggage. The interior can be easily switched from 4 passengers, to 2 passengers and to cargo-only flights.
- Average cruising speed
- 193 km/h (120 mph)
- Average trip distance
- 39-64 km (25-40 miles)
- Cruising altitude
- 457 m (1,500 ft)
- Propellers
- 8 tilt-propellers
- Electric motors
- 8 electric motors
- Batteries
- Battery packs (high-voltage, fast-charging)
- Noise at hover
- <65 dBA
- Noise at cruise
- <45 dBA
- Emissions
- 0 emissions
- Windows
- Tall windows
- Fuselage
- Carbon fiber composite
- Wings
- 1 high main wing
- Tail assembly
- 1 V tail
- Landing gear
- Fixed tricycle wheeled landing gear
- Safety features
- Distributed Electric Propulsion (DEP) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for its passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy for its passengers or cargo. Having multiple redundant systems on any aircraft decreases having any single point of failure. The aircraft is certified for Instrument Flight Rules (IFR). There is a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency.