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Sierra Technical Services, Inc. · USA

Fledermauser FM3

Sierra Technical Services Fledermauser FM3

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
Cargo
乘客
未公开/未录入
驾驶方式
Remote or autonomous
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
253 mph (157 km/h)
最大起飞重量
5,366 lb (2,434 kg)
载荷
1,175 lb (533 kg)
空重
4,191 lb (1,901 kg)
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
Turbine hybrid-electric and batteries
电机
32 electric motors
旋翼/螺旋桨
32 electric ducted fans with trailing edge flaperons
续航时间
2-1/2 hours
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. There are also redundancies of critical components in the sub-systems of the aircraft.

全部原始参数

Specifications:

Aircraft type
Hybrid-electric CTOL/STOL/VTOL passenger aircraft
Piloting
Remote or autonomous
Capacity
Cargo
Maximum speed
253 mph (157 km/h)
Flight time
2-1/2 hours
Empty weight
4,191 lb (1,901 kg)
Maximum payload
1,175 lb (533 kg)
Maximum takeoff weight
5,366 lb (2,434 kg)
Propellers
32 electric ducted fans with trailing edge flaperons
Electric motors
32 electric motors
Power source
Turbine hybrid-electric and batteries
Fuselage
Carbon fiber composite
Fuselage length
28.75 ft
Fuselage width
18.75 ft
Windows
Panoramic wrap around windows allowing forward, left, right and top visibility, for spectacular views - with a solid roof above the passenger compartment
Window
Canopy over cockpit
Wings
Box wing
Landing gear
Retractable quadricycle 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 of critical components in the sub-systems of the aircraft.