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Moller International / Freedom Motors · USA
Skycar® 200
Moller International Skycar® 200
其他推力转向(待细分) · 概念设计 · 核查 2026-10-01
飞行构型与公司名称
其他推力转向(待细分)
VFS 原始目录分组:矢量推力。尚无足够资料确定具体布局。
核对构型依据 ↗原始目录分组:矢量推力
中文名称:待核实 · 原名:Moller International / Freedom Motors
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。
资料覆盖与状态依据
可用性能指标 1/3 · 概念设计 · 目录依据 · 目录阶段,尚未核实批准状态
查看状态依据 ↗概念参数,尚不代表已实现性能
订阅本机型报道 RSS →主要参数
- 座位/载员
- 1 passenger
- 乘客
- 未公开/未录入
- 驾驶方式
- 1 pilot
- 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
- 1,320 lb (599 kg)
- 载荷
- 400 lb (181 kg)
- 空重
- 920 lb (417 kg)
- 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 and ethanol fuel
- 电机
- 2 electric motors
- 旋翼/螺旋桨
- 4 ducted fans
- 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. There are also redundancies of critical components in the sub-systems of the aircraft. The aircraft has a whole aircraft emergency ballistic parachute.
全部原始参数
Specifications:
- Aircraft type
- Hybrid-electric VTOL two passenger concept design aircraft
- Piloting
- 1 pilot
- Capacity
- 1 passenger
- Cruise speed (sea level at 65% power)
- 205 mph (330 km/h)
- Maximum speed (sea level)
- 242 mph (389 km/h)
- Cruise speed (25,000 ft/7,620 m)
- 300 mph (482 km/h)
- Maximum speed (on the road)
- ~30 mph (~48 km/h)
- Range (with two passengers at 122 mph/196 km/h)
- 434 miles (698 km)
- Flight time (sea level)
- 3.7 hours
- Empty weight
- 920 lb (417 kg)
- Maximum payload
- 400 lb (181 kg)
- Maximum takeoff weight
- 1,320 lb (599 kg)
- Propellers
- 4 ducted fans
- Engines
- 2 Freedom Motor Rotapower® engines
- Electric motors
- 2 electric motors
- Electrical Motor Power (90 seconds)
- 85 hp (63.4 kW) per motor
- Continuous Engine Power (total)
- 170 hp (126.8 kW)
- Power source
- Batteries and ethanol fuel
- Fuselage
- Carbon fiber composite
- Window
- Canopy over cockpit
- Wings
- 1 main low folding wing
- Tail
- 1 vertical stabilizer
- 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 are also redundancies of critical components in the sub-systems of the aircraft. The aircraft has a whole aircraft emergency ballistic parachute.
明确提及本机型的报道
暂无明确匹配的公开报道;通用或重名型号不会自动关联。
目录参数变化记录
从保存的目录刷新快照比较,资料修改不等于实机性能发生变化。
暂无已保存的版本变化,后续目录刷新将保留快照。