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LuftCar · USA
LuftCar
LuftCar
矢量推力 · 生产型设计 · 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
- 4 passengers
- 乘客
- 未公开／未录入
- 驾驶方式
- Autonomous
- 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
- Hybrid-electric
- 电机
- 6 electric motors
- 旋翼／螺旋桨
- 6 propellers
- 续航时间
- 未公开／未录入
- 飞行高度
- 4,000 feet (1.22 km)
- 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 in the sub-systems of the aircraft.
全部原始参数
Specifications:
- Aircraft type
- Hybrid-electric VTOL air and ground vehicle
- Piloting
- Autonomous
- Capacity
- 4 passengers
- Maximum cruise speed (air)
- 217 mph (350 km/h)
- Maximum range (air)
- 273 m (450 Km)
- Cruise altitude
- 4,000 feet (1.22 km)
- Maximum range (ground)
- 150 m (241 km)
- Propellers
- 6 propellers
- Electric Motors
- 6 electric motors
- Power source
- Hybrid-electric
- Fuselage
- Carbon fiber composite
- Windows
- Panoramic wrap around windows allowing forward, left, right visibility, for spectacular views with a solid roof above the passenger compartment
- Window
- Canopy over cockpit
- Wing assembly
- 1 high wing with tricycle wheeled land gear allowing the wing assembly to stand alone when needed
- Tail
- 1 rear t-tail
- Road vehicle
- 4 road 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 in the sub-systems of the aircraft.