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Trek Aerospace, Inc. · USA
TERN
Trek Aerospace Tern
矢量推力 · 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
- 600 pounds (272 kg). Cargo would include intelligence, surveillance, reconnaissance equipment and carry missiles (or bombs) for strike capability.
- 乘客
- 未公开／未录入
- 驾驶方式
- Autonomous
- 航程（按来源口径）
- 1,035 m (1,665 km)
- 巡航速度
- 253 mph (407 km/h)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 3,462 lb (1,570 kg)
- 载荷
- 1,608 lb (729 kg)
- 空重
- 1,854 lb (841 kg)
- 长度
- 19.04 ft (5.803 m)
- 翼展
- 未公开／未录入
- 高度
- 5.74 ft (1.749 m)
- 动力来源
- Hybrid-electric power source with 200 hp engine and battery packs
- 电机
- 4 electric motors (95 kW each motor)
- 旋翼／螺旋桨
- 4 ducted propellers
- 续航时间
- 9-1/2 hours
- 飞行高度
- 32,500 ft (9,906 m)
- 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.
全部原始参数
Specifications:
- Aircraft type
- Heavy-lift hybrid-electric VTOL concept design military drone
- Piloting
- Autonomous
- Capacity
- 600 pounds (272 kg). Cargo would include intelligence, surveillance, reconnaissance equipment and carry missiles (or bombs) for strike capability.
- Cruise speed
- 253 mph (407 km/h)
- Maximum sustained speed
- 276 mph (444 km/h)
- Maximum burst speed
- 432 mph (695 km/h)
- Range
- 1,035 m (1,665 km)
- Flight time
- 9-1/2 hours
- Maximum altitude
- 32,500 ft (9,906 m)
- Empty weight
- 1,854 lb (841 kg)
- Maximum payload
- 1,608 lb (729 kg)
- Maximum takeoff weight
- 3,462 lb (1,570 kg)
- Propellers
- 4 ducted propellers
- Electric Motors
- 4 electric motors (95 kW each motor)
- Power source
- Hybrid-electric power source with 200 hp engine and battery packs
- Fuselage
- Carbon fiber composite
- Wing span maximum width
- 22.00 ft (3.797 m)
- Wing span stowed
- 12.46 ft (6.70 m)
- Length
- 19.04 ft (5.803 m)
- Height
- 5.74 ft (1.749 m)
- Wings
- 1 X-wing, pivoting wings (wings fold for compact stowage)
- Tail
- 1 rear mounted horizontal stabilizer with two inverted vertical stabilizers
- Landing gear
- Fixed skid 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.