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Trek Aerospace, Inc. · USA
Mule
Trek Aerospace Mule
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
- Cargo only, with bottom loading cargo container
- 乘客
- 未公开／未录入
- 驾驶方式
- Autonomous (designed for autonomous piloting)
- 航程（按来源口径）
- 150 m (241 km)
- 巡航速度
- 132 mph (212 km/h)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 700 lb (318 kg)
- 载荷
- 未公开／未录入
- 空重
- 400 lb (181 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
- Hybrid-electric power source. Originally designed for a 120 hp engine. All power output information, including cruise speed, range, maximum payload weight and etc., would be dependent on the technology used as the power source.
- 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
- 未公开／未录入
全部原始参数
Specifications:
- Aircraft type
- Hybrid-electric air cargo VTOL concept design aircraft
- Piloting
- Autonomous (designed for autonomous piloting)
- Capacity
- Cargo only, with bottom loading cargo container
- Cruise speed
- 132 mph (212 km/h)
- Range
- 150 m (241 km)
- Empty weight
- 400 lb (181 kg)
- Maximum payload weight
- 200 lb (91 kg)
- Maximum fuel weight
- 100 lb (45 kg)
- Maximum takeoff weight
- 700 lb (318 kg)
- Propellers
- 2 ducted propellers
- Electric Motors
- 2 electric motors
- Power source
- Hybrid-electric power source. Originally designed for a 120 hp engine. All power output information, including cruise speed, range, maximum payload weight and etc., would be dependent on the technology used as the power source.
- Fuselage
- Carbon fiber composite
- Wings
- Two front stub wings
- Tail
- T-tail
- Landing gear
- Fixed skid landing gear