← eVTOL产品
Moller International / Freedom Motors · USA
Skycar® 600 LAMV
Moller International Skycar® 600 LAMV
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
- 5 people and/or cargo or a combination of both
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- 750 miles (1,207 km)
- 巡航速度
- 305 mph (491 km/h)
- 最大速度
- 395 mph (645 km/h)
- 最大起飞重量
- 未公开／未录入
- 载荷
- 1,250 lb (567 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
- Hybrid-electric or all electric power source depending upon the customer and current technology
- 电机
- 未公开／未录入
- 旋翼／螺旋桨
- 4 propeller nacelles
- 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.
全部原始参数
Specifications:
- Aircraft type
- Hybrid-electric or all electric VTOL passenger military concept design aircraft
- Piloting
- 1 pilot
- Capacity
- 5 people and/or cargo or a combination of both
- Cruise speed
- 305 mph (491 km/h)
- Maximum speed
- 395 mph (645 km/h)
- Range
- 750 miles (1,207 km)
- Operational altitude
- 25,000 feet (7,620 km)
- Maximum payload
- 1,250 lb (567 kg)
- Propellers
- 4 propeller nacelles
- Power source
- Hybrid-electric or all electric power source depending upon the customer and current technology
- Fuselage
- Carbon fiber composite
- Window
- Large windows for the pilots and larger than conventional side windows for passengers
- Wings
- Tandem wings
- Tail
- T-tail
- Landing gear
- Retractable tricycle wheeled landing gear
- 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.