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DTA Aircraft Manufacturer · France

eVTOL-2 DTA

DTA Aircraft Manufacturer eVTOL-2 DTA

多旋翼 · 生产型设计 · 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)
未公开/未录入
巡航速度
未公开/未录入
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
Battery packs
电机
8 brushless electric motors
旋翼/螺旋桨
8 carbon fiber propellers
续航时间
2 hours
飞行高度
未公开/未录入
安全设计
Distributed Electric Propulsion (DEP) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for its passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy for its passengers or cargo. 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 multicopter aircraft
Piloting
1 pilot
Capacity
1 passenger
Flight time
2 hours
Maximum cruise altitude
4,000 m (13,123 ft)
Propellers
8 carbon fiber propellers
Electric motors
8 brushless electric motors
Power source
Battery packs
Fuselage
Carbon fiber composite
Window
Canopy over cockpit
Tail
1 V-tail
Landing gear
Fixed tricycle wheeled landing gear
Safety features
Distributed Electric Propulsion (DEP) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for its passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy for its passengers or cargo. 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.