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Moller International / Freedom Motors · USA
Neuera 200
Moller International Neuera 200
多旋翼 · 原型机 · 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
- 1 passenger
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- 140 m (225 km)
- 巡航速度
- 75 (120 km/h)
- 最大速度
- 140 (160 km/h)
- 最大起飞重量
- 未公开／未录入
- 载荷
- 450 (204 kg)
- 空重
- 未公开／未录入
- 长度
- 10 feet (3 meters)
- 翼展
- 未公开／未录入
- 高度
- 3 feet (.91 meter)
- 动力来源
- Ethanol, gasoline or battery packs (depending upon customer specifications)
- 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
- Hundreds of feet (Many meters)
- 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 or all electric VTOL passenger prototype aircraft
- Piloting
- 1 pilot
- Capacity
- 1 passenger
- Cruise speed
- 75 (120 km/h)
- Maximum speed
- 140 (160 km/h)
- Range
- 140 m (225 km)
- Maximum altitude
- Hundreds of feet (Many meters)
- Maximum payload
- 450 (204 kg)
- Propellers
- 8 ducted fans
- Electric engines/motors
- 8 Rotapower engines or 8 electric motors (depending upon customer specifications)
- Power source
- Ethanol, gasoline or battery packs (depending upon customer specifications)
- Fuselage
- Carbon fiber composite
- Length
- 10 feet (3 meters)
- Width
- 10 feet (3 meters)
- Height
- 3 feet (.91 meter)
- Window
- Bubble canopy over cockpit
- Landing gear
- Quadricycle fixed wheeled landing gear (or fixed strut landing gear, possibly)
- 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.