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Moller International / Freedom Motors · USA
Firefly
Moller International Firefly
多旋翼 · 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
- 3 passengers
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- 100 miles (161 km)
- 巡航速度
- 80 mph (128 km/h)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 未公开／未录入
- 载荷
- 675 lb (306 kg)
- 空重
- 未公开／未录入
- 长度
- 10 feet (3.04 meters)
- 翼展
- 未公开／未录入
- 高度
- 2.5 feet (.762 meters)
- 动力来源
- Conventional and hybrid-electric (ethanol) or battery packs (the power source is chosen by the customer)
- 电机
- 未公开／未录入
- 旋翼／螺旋桨
- 8 ducted fans
- 续航时间
- 未公开／未录入
- 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. The aircraft also has emergency airbags.
全部原始参数
Specifications:
- Aircraft type
- Conventional, hybrid-electric or all-electric VTOL rescue concept design aircraft
- Piloting
- 1 pilot
- Capacity
- 3 passengers
- Cruise speed
- 80 mph (128 km/h)
- Maximum speed (sea level)
- 100 mph (161 km/h)
- Range
- 100 miles (161 km)
- Maximum payload
- 675 lb (306 kg)
- Propellers
- 8 ducted fans
- Electric motors/engines
- 8 electric motors or 8 electric engines (depending upon the customer)
- Power source
- Conventional and hybrid-electric (ethanol) or battery packs (the power source is chosen by the customer)
- Fuselage
- Carbon fiber composite
- Length
- 10 feet (3.04 meters)
- Width
- 9 feet (2.74 meters)
- Height
- 2.5 feet (.762 meters)
- Window
- Open cockpit
- Landing gear
- Fixed strut 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. The aircraft also has emergency airbags.