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Hari Prasad · Italy

Mobula

Prasad Mobula

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
5-7 passengers
乘客
未公开/未录入
驾驶方式
1 pilot (or AI piloting)
航程(按来源口径)
280 km (174 m)
巡航速度
222-259 km/h (138-161 mph)
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
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
Batteries
电机
18 electric motors
旋翼/螺旋桨
18 electric ducted fans (EDFs), 6 EDFs located in the wings tilt for VTOL, forward flight and any other type of maneuvering. 10 EDFs are inside the wing for forward flight and are also used for maneuvering. 2 EDFs are in the front of the aircraft used for VTOL flight, forward flight and for maneuvering.
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) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. Having multiple redundant systems on any aircraft decreases having any single point of failure. The aircraft has no moving wing surfaces when transitioning from vertical to forward flight and the reverse which increases safety by reducing complexity.

全部原始参数

Specifications:

Aircraft type
Passenger eVTOL concept design aircraft
Piloting
1 pilot (or AI piloting)
Capacity
5-7 passengers
Cruise speed
222-259 km/h (138-161 mph)
Range
280 km (174 m)
Maximum payload weight
Unknown
Propellers
18 electric ducted fans (EDFs), 6 EDFs located in the wings tilt for VTOL, forward flight and any other type of maneuvering. 10 EDFs are inside the wing for forward flight and are also used for maneuvering. 2 EDFs are in the front of the aircraft used for VTOL flight, forward flight and for maneuvering.
Electric motors
18 electric motors
Power source
Batteries
Fuselage
Carbon fiber composite
Windows
Larger than conventional windows and a sunroof over the passenger cabin
Wings
1 rear high main delta wing with winglets. The designer calls the rear main wing a manta ray wing.
Ventral fins/strakes
1 forward ventral fin (that doubles as the front landing gear strut) and 2 rear ventral strakes (that double as the rear landing gear struts)
Landing gear
Fixed tricycle wheeled landing gear
Safety features
Distributed electric propulsion (DEP) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. Having multiple redundant systems on any aircraft decreases having any single point of failure. The aircraft has no moving wing surfaces when transitioning from vertical to forward flight and the reverse which increases safety by reducing complexity.