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Moller International / Freedom Motors · USA
Skycar® M200
Moller International Skycar® M200
矢量推力 · 原型机 · 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 the technology because available)
- 航程（按来源口径）
- 1,050 miles (1,689 km)
- 巡航速度
- 未公开／未录入
- 最大速度
- 403 mph (648 km/h)
- 最大起飞重量
- 载荷
- 空重
- 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 battery packs.
- 电机
- 未公开／未录入
- 旋翼／螺旋桨
- 6 ducted fans
- 续航时间
- 飞行高度
- 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. There is a whole aircraft emergency ballistic parachute in case of a power failure.
全部原始参数
Specifications:
- Aircraft type
- Hybrid-electric or all-electric VTOL prototype
- Piloting
- 1 pilot (autonomous piloting when the technology because available)
- Capacity
- 1 passenger
- Maximum speed
- 403 mph (648 km/h)
- Range
- 1,050 miles (1,689 km)
- Flight time
- Cruise altitude
- Empty weight
- Maximum payload
- Maximum takeoff weight
- Propellers
- 6 ducted fans
- Engines/Electric motors
- 6 engines or 6 electric motors depending upon the customer demands.
- Power source
- Hybrid-electric or battery packs.
- Fuselage
- Carbon fiber composite
- Window
- Canopy over cockpit
- 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. There is a whole aircraft emergency ballistic parachute in case of a power failure.