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Manta Aircraft SA · Italy
ANN Drone
Manta Aircraft ANN Drone
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
- 未公开/未录入
- 乘客
- 未公开/未录入
- 驾驶方式
- Remote, autopilot and autonomous (no crew)
- 航程(按来源口径)
- Unknown
- 巡航速度
- Unknown
- 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
- 8 electric motors
- 旋翼/螺旋桨
- 8 ducted fans. (4 ducted fans for VTOL are stationary. 4 tilting ducted fans for VTOL flight.)
- 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), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers and motors on the aircraft so if one or more motors or propellers fail, the other working motors and propellers can safely land the aircraft. The aircraft can also land like a conventional airplane its VTOL capability becomes disabled.
全部原始参数
Specifications:
- Aircraft type
- Hybrid-electric vertical short takeoff and landing (HeV/STOL) drone
- Piloting
- Remote, autopilot and autonomous (no crew)
- Surveillance instrument maximum payload
- Unknown
- Cruise speed
- Unknown
- Range
- Unknown
- Propellers
- 8 ducted fans. (4 ducted fans for VTOL are stationary. 4 tilting ducted fans for VTOL flight.)
- Electric Motors
- 8 electric motors
- Power source
- Hybrid-electric
- Wings
- Canard wings
- Landing gear
- Tricycle-wheeled retractable landing gear
- Safety Features
- Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers and motors on the aircraft so if one or more motors or propellers fail, the other working motors and propellers can safely land the aircraft. The aircraft can also land like a conventional airplane its VTOL capability becomes disabled.