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NAATS Aviation Pvt Ltd · India
NAV Copter 254
NAATS Aviation NAV Copter 254
多旋翼 · 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
- 2 passengers
- 乘客
- 未公开／未录入
- 驾驶方式
- Unknown
- 航程（按来源口径）
- 40 km (25 m)
- 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
- 8 electric motors
- 旋翼／螺旋桨
- 8 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
- 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 passengers or cargo. 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.
全部原始参数
Specifications:
- Aircraft type
- Passenger eVTOL multicopter prototype aircraft
- Piloting
- Unknown
- Capacity
- 2 passengers
- Cruise speed
- 100 km/h (62 mph)
- Range
- 40 km (25 m)
- Propellers
- 8 propellers
- Electric motors
- 8 electric motors
- Power source
- Batteries
- Fuselage
- Carbon fiber composite with one door and bench seating for the passengers
- Windows
- Front and two side windows
- Landing gear
- Fixed skid 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 passengers or cargo. 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.