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Gelisim University · Turkey

Tusi

Gelisim University Tusi

多旋翼 · 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
未公开/未录入
乘客
未公开/未录入
驾驶方式
1 person
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
80 kilos (176 lb)
空重
100 kg (220 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
Batteries
电机
6 electric motors
旋翼/螺旋桨
6 propellers
续航时间
9 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.

全部原始参数

Specifications:

Aircraft type
eVTOL passenger aircraft and is scalable
Piloting
1 person
Range for flying
40 km (24 m)
Range for the road
220 km (136 m)
Flight Time
9 minutes
Maximum payload
80 kilos (176 lb)
Empty weight
100 kg (220 lb)
Propellers
6 propellers
Electric Motors
6 electric motors
Power source
Batteries
Fuselage
Unknown
Windows
Canopy over cockpit
Landing gear
Fixed tricycle wheeled landing gear which double as wheels for ground travel
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.