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Hari Krishnan G · India
Reconnaissance Copter
Krishnan Reconnaissance Copter
多旋翼 · 概念设计 · 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
- Autonomous piloting by Artificial Intelligence (AI) when it becomes available
- 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
- 2 electric motors
- 旋翼／螺旋桨
- 2 ducted propellers
- 续航时间
- 未公开／未录入
- 飞行高度
- 未公开／未录入
- 安全设计
- There are redundancies in the sub-systems of the aircraft for added safety. There is a whole aircraft emergency ballistic parachute.
全部原始参数
Specifications:
- Aircraft type
- Passenger eVTOL helicopter and roadable vehicle concept design
- Piloting
- Autonomous piloting by Artificial Intelligence (AI) when it becomes available
- Capacity
- 1 passenger
- Cruise speed (air)
- Unknown
- Cruise speed (ground)
- Unknown
- Propellers
- 2 ducted propellers
- Electric Motors
- 2 electric motors
- Power source
- Battery packs
- Fuselage
- Carbon fiber composite
- Windows
- Large panoramic wrap around window allowing forward, left and right views with a solid roof above the passenger compartment
- Wings
- 1 main high dihedral wing
- Landing gear
- Fixed wheeled landing gear that double as road wheels
- Safety features
- There are redundancies in the sub-systems of the aircraft for added safety. There is a whole aircraft emergency ballistic parachute.