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Scienex · Russia

Flyter

Scienex Flyter

矢量推力 · 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 plus luggage
乘客
未公开/未录入
驾驶方式
Autonomous via artificial intelligence
航程(按来源口径)
150 km (93 m)
巡航速度
100 km/h (62 mph)
最大速度
120 km/h (75 mph)
最大起飞重量
未公开/未录入
载荷
250 kg (551 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
Hydrogen fuel cells
电机
Unknown
旋翼/螺旋桨
Unknown
续航时间
未公开/未录入
飞行高度
1,500 m (4,921 ft)
安全设计
Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers and motors on the aircraft so if one or more motors or propellers fail, the other working motors and propellers can safely land the aircraft.

全部原始参数

Specifications:

Aircraft type
Hybrid-electric VTOL
Piloting
Autonomous via artificial intelligence
Capacity
2 passengers plus luggage
Cruise speed
100 km/h (62 mph)
Maximum speed
120 km/h (75 mph)
Normal range
100 km (62 m)
Maximum range
150 km (93 m)
Maximum altitude
1,500 m (4,921 ft)
Maximum payload
250 kg (551 lb)
Empty weight
600 kg (1,323 lb)
Operating temperature
-20/+40°C (-4/+104°F)
Propellers
Unknown
Electric Motors
Unknown
Power source
Hydrogen fuel cells
Fuselage
Carbon fiber composite
Windows
Panoramic windows forward, left, right and top visibility, for spectacular views
Landing gear
Retractable quad-legged landing gear
Safety Features
Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers and motors on the aircraft so if one or more motors or propellers fail, the other working motors and propellers can safely land the aircraft.