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Kitty Hawk Corporation · USA
Flyer (Defunct Prototype)
Kitty Hawk Flyer
个人飞行器 · 停研／历史型号 · 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
- 未公开／未录入
- 航程（按来源口径）
- 未公开／未录入
- 巡航速度
- 20–30 mph (32–48 km/h)
- 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
- Under 250 lb (113 kg) - (Not including the pontoons: 230 lb [104 kg]
- 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
- 旋翼／螺旋桨
- 8
- 续航时间
- 未公开／未录入
- 飞行高度
- 10–20 feet [3-6 m]
- 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. With its two pontoons, the aircraft can safely on the land or on water. The propellers were under the webbing on the airframe which also provided safety to the pilot, in case the pilot fell off the seat, he/she would fall onto the frame and not into the propellers. The aircraft also has an auto-land capability for safety.
全部原始参数
Specifications:
- Aircraft type
- eVTOL aircraft capable of water landings
- Piloting/Capacity
- 1 pilot
- Pilot controls
- 2 handle bars
- Cruise speed
- 20–30 mph (32–48 km/h)
- Cruise altitude
- 10–20 feet [3-6 m]
- Empty weight
- Under 250 lb (113 kg) - (Not including the pontoons: 230 lb [104 kg]
- Propellers
- 8
- Electric Motors
- 8
- Power source
- Batteries
- Cockpit
- Open cockpit
- Fuselage
- A airframe with webbing on the frame.
- Landing gear
- Two large pontoons
- 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. With its two pontoons, the aircraft can safely on the land or on water. The propellers were under the webbing on the airframe which also provided safety to the pilot, in case the pilot fell off the seat, he/she would fall onto the frame and not into the propellers. The aircraft also has an auto-land capability for safety.