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teTra Aviation Corporation · Japan
teTra Mk-3
teTra Aviation Mk-7
升力＋巡航 · 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）
- 110 m (177 km)
- 巡航速度
- 250 km/h (155 mph)
- 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
- 10 m (32.8 ft)
- 翼展
- 8 m (26.3 ft)
- 高度
- 未公开／未录入
- 动力来源
- Batteries
- 电机
- 11 electric motors
- 旋翼／螺旋桨
- 11 propellers (10 VTOL-only propellers, 1 rear pusher propeller)
- 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) uses multiple propellers or electric ducted fans, each powered by electric motors, to increase safety through redundancy. If one or more components fail, the remaining ones can still ensure a safe landing. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. Having multiple redundant systems on any aircraft decreases having any single point of failure. The aircraft has few moving surfaces and no tilting wings when transitioning from vertical to forward flight and the reverse which increases safety by reducing complexity. If the VTOL propellers fail, the aircraft can land conventionally at an airport runway or on a roadway.
全部原始参数
Specifications:
- Aircraft type
- Passenger eVTOL prototype aircraft
- Piloting
- 1 pilot
- Capacity
- 1 passenger
- Cruise speed
- 250 km/h (155 mph)
- Range
- 110 m (177 km)
- Propellers
- 11 propellers (10 VTOL-only propellers, 1 rear pusher propeller)
- Electric motors
- 11 electric motors
- Power source
- Batteries
- Fuselage material
- Carbon fiber composite and aircraft aluminum
- Wingspan
- 8 m (26.3 ft)
- Length
- 10 m (32.8 ft)
- Windows
- Panoramic wrap around windows allowing forward, left and right visibility for spectacular views with a solid roof above the passenger compartment
- Wings
- 1 main high wing with 4 booms for the VTOL propellers.
- Tail
- 1 boom tail with 2 downward vertical stabilizers
- Landing gear
- Fixed tricycle wheeled landing gear
- Safety features
- Distributed Electric Propulsion (DEP) uses multiple propellers or electric ducted fans, each powered by electric motors, to increase safety through redundancy. If one or more components fail, the remaining ones can still ensure a safe landing. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. Having multiple redundant systems on any aircraft decreases having any single point of failure. The aircraft has few moving surfaces and no tilting wings when transitioning from vertical to forward flight and the reverse which increases safety by reducing complexity. If the VTOL propellers fail, the aircraft can land conventionally at an airport runway or on a roadway.