← eVTOL产品
Terrafugia · USA
TF-2.0 Lift + Push
Terrafugia TF-2.0 Lift + Push
升力＋巡航 · 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
- 4 passengers
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot, in the future it will be autonomous
- 航程（按来源口径）
- 196-249 miles (315-400 km)
- 巡航速度
- 138 mph (222 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
- 1,102 lb (500 kg)
- 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 or 100% batteries
- 电机
- 5 electric motors
- 旋翼／螺旋桨
- 5 propellers (4 dedicated VTOL propellers, 1 pusher propeller)
- 续航时间
- Unknown
- 飞行高度
- Unknown
- 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 in the sub-systems of the aircraft.
全部原始参数
Specifications:
- Aircraft type
- Hybrid-electric and eVTOL roadable passenger aircraft
- Piloting
- 1 pilot, in the future it will be autonomous
- Capacity
- 4 passengers
- Cruise speed
- 138 mph (222 km/h)
- Range
- 196-249 miles (315-400 km)
- Flight time
- Unknown
- Cruise altitude
- Unknown
- Maximum payload
- 1,102 lb (500 kg)
- Propellers
- 5 propellers (4 dedicated VTOL propellers, 1 pusher propeller)
- Electric motors
- 5 electric motors
- Power source
- Hybrid-electric or 100% batteries
- Fuselage
- Carbon fiber composite
- Windows
- Panoramic wrap around windows allowing forward, left, right for spectacular views with a solid roof above the passenger compartment
- Wing
- 1 high-wing
- Tail
- 1 duel rudder and high stabilizer configuration
- Landing gear
- Fixed skid-type 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 in the sub-systems of the aircraft.