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Nalwa Aero · India

Nalwa 5X

Nalwa Aero Nalwa 5X

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
4 passengers and luggage
乘客
未公开/未录入
驾驶方式
1 pilot, autonomous or remote piloting
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
未公开/未录入
载荷
未公开/未录入
空重
Unknown
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
12 electric motors
旋翼/螺旋桨
12 tilt-electric ducted fans (EDFs)
续航时间
1-1/2 hours plus 15 minutes of reserve time
飞行高度
2,000 m (6,562 ft)
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 including the engines, flight control and navigation systems. There is a whole aircraft emergency ballistic parachute.

全部原始参数

Specifications:

Aircraft type
eVTOL passenger and air cargo concept design aircraft
Piloting
1 pilot, autonomous or remote piloting
Capacity
4 passengers and luggage
Maximum cruise speed
400 km/h (249 mph)
Flight time
1-1/2 hours plus 15 minutes of reserve time
Maximum altitude
2,000 m (6,562 ft)
Empty weight
Unknown
Maximum payload weight
700 kg (1,543 lb)
Propellers
12 tilt-electric ducted fans (EDFs)
Electric motors
12 electric motors
Power source
Batteries
Fuselage
Carbon fiber composite
Windows
Panoramic wrap around tinted windows allowing forward, left and right visibility for spectacular views with a solid roof above the passenger compartment
Wings
1 forward canard wing and 1 rear box wing
Landing gear
Fixed tricycle landing legs
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 including the engines, flight control and navigation systems. There is a whole aircraft emergency ballistic parachute.