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Sierra Technical Services, Inc. · USA
Fledermauser FM1
Sierra Technical Services Fledermauser FM1
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）
- 523 miles (841 km)
- 巡航速度
- 178 mph (286 km/h)
- 最大速度
- 215 mph (346 km/h)
- 最大起飞重量
- 1,190 lb (538 kg)
- 载荷
- 260 lb (117 kg)
- 空重
- 930 lb (421 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 cargo concept design aircraft
- Piloting
- Remote or autonomous
- Capacity
- Cargo
- Cruise speed
- 178 mph (286 km/h)
- Maximum speed
- 215 mph (346 km/h)
- Range
- 523 miles (841 km)
- Flight time
- 2-1/2 hours
- Empty weight
- 930 lb (421 kg)
- Maximum payload
- 260 lb (117 kg)
- Maximum takeoff weight
- 1,190 lb (538 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
- 13', 11''
- Fuselage width
- 12', 2''
- Fuselage height
- 4', 6''
- 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.