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Freedom Transports, Inc. · USA
Zero G eCruzer
Freedom Transports Zero G eCruzer
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
- 6-8 passengers
- 乘客
- 未公开/未录入
- 驾驶方式
- Unknown
- 航程(按来源口径)
- 1,726 m (2,778 km)
- 巡航速度
- 420 mph (676 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
- 未公开/未录入
- 空重
- 未公开/未录入
- 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
- Hybrid-electric
- 电机
- 11 or more (including motors for the retractable landing gear)
- 旋翼/螺旋桨
- 未公开/未录入
- 续航时间
- 未公开/未录入
- 飞行高度
- 未公开/未录入
- 安全设计
- Has electric motors which are more reliable than gas-powered engines, has particle separators for each ducted fan, can land like a conventional airplane in the unlikely event of a motor failure, has fly-by-wire control technology, with conventional flight controls for added redundancy, there will be two electric motors in each motor nacelle in tandem, for redundancy, has weather protection system beyond FAA requirements and more.
全部原始参数
Specifications:
- Aircraft type
- Hybrid-electric VTOL corporate jet aircraft
- Piloting
- Unknown
- Capacity
- 6-8 passengers
- Cruise speed
- 420 mph (676 km/h)
- Range
- 1,726 m (2,778 km)
- Ducted fans
- 4 ducted fans with tilting exhaust used for both VTOL and forward flight.
- Electric Motors
- 11 or more (including motors for the retractable landing gear)
- Power source
- Hybrid-electric
- Fuselage
- CNC machined metal airframe except fuselage top section, the floor is one piece machined section with a composite top
- Windows
- Typical corporate jet vertically oval windows
- Wings
- Canard wings with a swept back rear wing with winglets
- Landing gear
- Retractable wheeled landing gear
- Safety Features
- Has electric motors which are more reliable than gas-powered engines, has particle separators for each ducted fan, can land like a conventional airplane in the unlikely event of a motor failure, has fly-by-wire control technology, with conventional flight controls for added redundancy, there will be two electric motors in each motor nacelle in tandem, for redundancy, has weather protection system beyond FAA requirements and more.