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Trek Aerospace · USA
FlyKart 2
Trek Aerospace FlyKart 2
个人飞行器 · 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
- 未公开／未录入
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot with autopilot technology
- 航程（按来源口径）
- 未公开／未录入
- 巡航速度
- 52 mph (83 km/h)
- 最大速度
- 63 mph (102 km/h)
- 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
- 6.2 ft (1.95 m)
- 翼展
- 未公开／未录入
- 高度
- 3.9 ft (1.2 m)
- 动力来源
- 9.6 kWh battery packs
- 电机
- 10 electric motors (5.6- kW)
- 旋翼／螺旋桨
- 10 ducted propellers
- 续航时间
- 30+ minutes
- 飞行高度
- 未公开／未录入
- 安全设计
- Distributed Electric Propulsion (DEP) uses multiple propellers or electric ducted fans, each powered by electric motors, to increase safety through redundancy. If one or more components fail, the remaining ones can still ensure a safe landing. 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. The aircraft has auto-pilot system, 4-point safety harness and screened propellers.
全部原始参数
Specifications:
- Aircraft type
- Passenger eVTOL prototype personal flying device
- Pilot
- 1 pilot with autopilot technology
- Cruise speed
- 52 mph (83 km/h)
- Maximum speed
- 63 mph (102 km/h)
- Flight time
- 30+ minutes
- Propellers
- 10 ducted propellers
- Electric motors
- 10 electric motors (5.6- kW)
- Power source
- 9.6 kWh battery packs
- Fuselage
- Carbon fiber composite
- Width
- 6-1/2 ft (2 m)
- Length
- 6.2 ft (1.95 m)
- Height
- 3.9 ft (1.2 m)
- Cockpit
- Open cockpit
- Landing gear
- Fixed quadricycle wheeled landing gear
- Safety Features
- Distributed Electric Propulsion (DEP) uses multiple propellers or electric ducted fans, each powered by electric motors, to increase safety through redundancy. If one or more components fail, the remaining ones can still ensure a safe landing. 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. The aircraft has auto-pilot system, 4-point safety harness and screened propellers.