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ALEF Aeronautics · USA
Model A
ALEF Aeronautics Model A
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
- 1 passenger
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot (autonomous piloting when it becomes available)
- 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
- 200 lb (91 kg)
- 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
- Batteries
- 电机
- 8 electric motors
- 旋翼／螺旋桨
- 8 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), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. There are also redundancies of critical components in the sub-systems of the aircraft. The aircraft has detect and avoid technology. The aircraft has redundancy in all of key the components of the aircraft. The aircraft has a whole aircraft emergency ballistic parachute.
全部原始参数
Specifications:
- Aircraft type
- Road driveable eVTOL passenger concept design vehicle
- Piloting
- 1 pilot (autonomous piloting when it becomes available)
- Capacity
- 1 passenger
- Cruise speed (air)
- Unknown
- Cruise speed (road)
- 25 mph (40 km/h)
- Range (air)
- 110 m (117 km)
- Range (road)
- 200 m (322 km)
- Maximum payload
- 200 lb (91 kg)
- Propellers
- 8 propellers
- Electric motors
- 8 electric motors
- Power source
- Batteries
- Fuselage
- Carbon fiber composite
- Windows
- Gimballed rotating cockpit with windows allowing forward, left, right, rear and top visibility
- Landing gear
- 4 automotive wheels
- Safety features
- Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. There are also redundancies of critical components in the sub-systems of the aircraft. The aircraft has detect and avoid technology. The aircraft has redundancy in all of key the components of the aircraft. The aircraft has a whole aircraft emergency ballistic parachute.