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teTra Aviation Corporation · Japan

teTra Mk-3

teTra Aviation Mk-3

个人飞行器 · 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
未公开/未录入
乘客
未公开/未录入
驾驶方式
1 pilot
航程(按来源口径)
未公开/未录入
巡航速度
100 km/h (62 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
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
Batteries
电机
4 electric motors
旋翼/螺旋桨
4 propellers
续航时间
未公开/未录入
飞行高度
30 m (98 ft)
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. There is also a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency.

全部原始参数

Specifications:

Aircraft type
Passenger eVTOL prototype aircraft
Piloting
1 pilot
Cruise speed
100 km/h (62 mph)
Cruise altitude
30 m (98 ft)
Propellers
4 propellers
Electric Motors
4 electric motors
Power source
Batteries
Fuselage
Carbon fiber composite and aluminum
Dimensions
1.65 m high (5.4 feet) X 2.2 meters wide (7.2 feet) X 2 meters long (6.6 feet)
Wing
1 main high stub wing with winglets
Landing gear
Fixed skids and 1 center wheel
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. There is also a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency.