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Moller International / Freedom Motors · USA
Skycar
Moller International Skycar® 400
其他推力转向(待细分) · 原型机 · 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 · 原型机 · 目录依据 · 目录阶段,尚未核实批准状态
查看状态依据 ↗订阅本机型报道 RSS →主要参数
- 座位/载员
- 3 passengers
- 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
- 2,400 lb (1,088 kg)
- 载荷
- 720 lb (326 kg)
- 空重
- 1,680 lb (762 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
- Petroleum fueled engines (ethanol) or a hybrid-electric power source
- 电机
- 8 engines or 8 electric motors
- 旋翼/螺旋桨
- Ducted fans or electric ducted fans (EDFs)
- 续航时间
- 未公开/未录入
- 飞行高度
- 36,000 ft (10,972 m)
- 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 a whole aircraft emergency ballistic parachute.
全部原始参数
Specifications:
- Aircraft type
- Conventional, hybrid-electric or all-electric VTOL passenger prototype aircraft
- Piloting
- 1 pilot
- Capacity
- 3 passengers
- Cruise speed at sea level (at 65% power)
- 284 mph (457 km/h)
- Maximum speed at sea level
- 331 mph (532 km/h)
- Maximum speed (20,000 ft/6,096 m)
- 308 mph (495 km/h)
- Range in the air (economic cruise)
- 750 miles (1,206 km)
- Maximum speed on paved roads
- 30 mph (50 km/h)
- Flight time (at sea level at 131 mph/210 km/h)
- 5.9 hours (engine)
- Maximum altitude
- 36,000 ft (10,972 m)
- Area needed for takeoff and landing
- 35 feet in diameter (11 meters in diameter)
- Empty weight
- 1,680 lb (762 kg)
- Maximum payload
- 720 lb (326 kg)
- Maximum takeoff weight
- 2,400 lb (1,088 kg)
- Noise level goal (at 500 ft/152 m)
- 65 dBA
- Propellers
- Ducted fans or electric ducted fans (EDFs)
- Electric motors
- 8 engines or 8 electric motors
- Power source
- Petroleum fueled engines (ethanol) or a hybrid-electric power source
- Fuselage
- Carbon fiber composite
- Dimensions (Length X Width X Height)
- 21.5' X 8.5' X 7.5' (6.5m X 2.5m X 2.25m)
- Window
- Canopy over cockpit
- Wings
- 1 main low wing (depending upon the model variation)
- Tail
- 1 vertical stabilizer or 1 T-tail (depending upon the model variation)
- Landing gear
- Retractable tricycle wheeled landing gear (or fixed 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. 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。