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VTOL Aviation India PVT. LTD. · India

Abhiyaan ENM800

VTOL Aviation India Abhiyaan ENM800

升力+巡航 · 阶段未核实 · 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
Autonomous
航程(按来源口径)
600 km (373 miles)
巡航速度
180 km/h (112 mph)
最大速度
234 km/h (145 mph)
最大起飞重量
800 kg (1,764 lb)
载荷
200 kg (441 lb)
空重
600 kg (1,323 lb)
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
Hybrid-electric and batteries
电机
9 electric motors
旋翼/螺旋桨
9 propellers
续航时间
未公开/未录入
飞行高度
2,000 meters (6,652 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 in the sub-systems of the aircraft. The aircraft can also land conventionally if needed. The aircraft has a whole aircraft ballistic parachute.

全部原始参数

Specifications Hybrid-Electric VTOL Model:

Aircraft type
Hybrid-electric VTOL air taxi aircraft
Piloting
Autonomous
Capacity
2 passengers
Cruise speed
180 km/h (112 mph)
Maximum speed
234 km/h (145 mph)
Range
600 km (373 miles)
Maximum flight time
3 hours, 20 minutes
Maximum speed
234 km/h (145 mph)
Cruise altitude
2,000 meters (6,652 ft)
Maximum altitude
5,700 meters (18,701 ft)
Empty weight
600 kg (1,323 lb)
Maximum payload
200 kg (441 lb)
Maximum takeoff weight
800 kg (1,764 lb)
Propellers
9 propellers
Electric Motors
9 electric motors
Power source
Hybrid-electric and batteries
Fuselage
Carbon fiber composite
Windows
Small canopy over cockpit
Wings
1 high wing
Tail
1 t-tail
Landing gear
Tricycle fixed 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 in the sub-systems of the aircraft. The aircraft can also land conventionally if needed. The aircraft has a whole aircraft ballistic parachute.

Specifications eVTOL Model:

Aircraft type
eVTOL air taxi aircraft
Piloting
Autonomous
Capacity
2 passengers
Cruise speed
180 km/h (112 mph)
Maximum Range
250 km (155 miles)
Maximum flight time
Over 1 hour
Cruise altitude
2,000 meters (6,652 ft)
Maximum altitude
5,700 meters (18,701 ft)
Empty weight
600 kg (1,323 lb)
Maximum payload
200 kg (441 lb)
Maximum takeoff weight
800 kg (1,764 lb)
Propellers
9 propellers
Electric Motors
9 electric motors
Power source
Batteries
Fuselage
Carbon fiber composite
Windows
Small canopy over cockpit
Wings
1 high wing
Tail
1 t-tail
Landing gear
Tricycle fixed 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 in the sub-systems of the aircraft. The aircraft can also land conventionally if needed. The aircraft has a whole aircraft ballistic parachute.