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Moller International / Freedom Motors · USA

Autovolantor

Moller International Autovolantor

升力+巡航 · 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
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
150 mph (241 km/h)
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
~2,400 lb (1,088 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
Rotapower engines and battery packs
电机
8 Rotapower engines create electricity for the batteries
旋翼/螺旋桨
8 ducted fans
续航时间
30 minutes
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. If there is a power failure, the aircraft can glide and land on a runway or road.

全部原始参数

Specifications:

Aircraft type
Hybrid-electric VTOL passenger and roadable concept design vehicle
Piloting
1 pilot
Capacity
1 passenger
Cruise speed
150 mph (241 km/h)
Flight time
30 minutes
Range (air)
75 miles (120 km)
Range (ground with Rotapower engines)
150 miles (241 km/h)
Ground range (batteries alone)
40 miles (64 km/h)
Maximum cruise altitude
2,500 feet (762 meters)
Empty weight
~2,400 lb (1,088 kg)
Propellers
8 ducted fans
Electric motors
8 Rotapower engines create electricity for the batteries
Power source
Rotapower engines and battery packs
Fuselage
Carbon fiber composite (the body style is based on the Ferrari 599 GTB)
Windows
Automobile type windows
Wings
4 wings (2 wings extend from the front bottom of the car, 2 wings fold open in the rear of the car)
Landing gear
4 automobile tires
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. If there is a power failure, the aircraft can glide and land on a runway or road.