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Transcend Air Corporation · USA
V-621
Transcend Air V-621
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
- 11 people, maximum 365 lb (166 kg) each person
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot and autonomous capable
- 航程（按来源口径）
- 3,127 m (5,032 km)
- 巡航速度
- 541 mph (871 km/h)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 15,300 lb (6,940 kg)
- 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
- 2 GE turboshaft engines
- 电机
- 4 electric motors
- 旋翼／螺旋桨
- 2 turbine powered propellers, 4 electric tailfan propeller
- 续航时间
- 未公开／未录入
- 飞行高度
- 未公开／未录入
- 安全设计
- The aircraft can land conventionally if there is a power loss in the tractor propellers. There are also redundancies of critical components in the sub-systems of the aircraft.
全部原始参数
Specifications:
- Aircraft type
- Military hybrid-electric passenger and cargo VTOL concept design aircraft
- Piloting
- 1 pilot and autonomous capable
- Capacity
- 11 people, maximum 365 lb (166 kg) each person
- Cruise speed
- 541 mph (871 km/h)
- Range
- 3,127 m (5,032 km)
- Maximum operating altitude
- 30,000 ft (9,144 m)
- Maximum takeoff weight
- 15,300 lb (6,940 kg)
- Propellers
- 2 turbine powered propellers, 4 electric tailfan propeller
- Electric motors
- 4 electric motors
- Power source
- 2 GE turboshaft engines
- Fuselage
- Carbon fiber composite
- Windows
- Typical military windows
- Wings
- 1 high main tilt-wing
- Tail
- 1 H-tail
- Landing gear
- Retractable wheeled landing gear
- Safety features
- The aircraft can land conventionally if there is a power loss in the tractor propellers. There are also redundancies of critical components in the sub-systems of the aircraft.