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NAATS Aviation Pvt Ltd · India

ProMobility

NAATS Aviation ProMobility

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
2 passengers
乘客
未公开/未录入
驾驶方式
Unknown
航程(按来源口径)
1,500 km (932 m)
巡航速度
400 km/h (249 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
5 electric motors
旋翼/螺旋桨
5 propellers (4 VTOL-only propellers, 1 pusher propeller)
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.

全部原始参数

Specifications:

Aircraft type
Passenger eVTOL long-range aircraft
Piloting
Unknown
Capacity
2 passengers
Cruise speed
400 km/h (249 mph)
Range
1,500 km (932 m)
Propellers
5 propellers (4 VTOL-only propellers, 1 pusher propeller)
Electric motors
5 electric motors
Power source
Batteries
Fuselage
Carbon fiber composite
Windows
Panoramic wrap around windows allowing forward, left and right visibility for spectacular views with a solid roof above the passenger compartment
Wings
1 high main wing
Tail
1 boom mounted inverted V-tail
Landing gear
Fixed quadricycle strut 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.