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Transcend Air Corporation · USA
V-653
Transcend Air V-653
倾转机翼 · 概念设计 · 核查 2026-10-01
飞行构型与公司名称
倾转机翼
The aircraft has one high main tilt-wing and one H-tail.
核对构型依据 ↗原始目录分组：矢量推力
中文名称：待核实 · 原名：Transcend Air Corporation
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。
资料覆盖与状态依据
可用性能指标 3/3 · 概念设计 · 目录依据 · 目录阶段，尚未核实批准状态
查看状态依据 ↗概念参数，尚不代表已实现性能
订阅本机型报道 RSS →主要参数
- 座位／载员
- 100 people, maximum 365 lb (166 kg) each person
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot, autonomous capable
- 航程（按来源口径）
- 5,824 miles (9,373 km)
- 巡航速度
- 529 mph (851 km/h)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 105,000 lb (47,627 kg)
- 载荷
- 42,000 lb (19,051 kg)
- 空重
- 63,000 lb (28,576 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
- 5 GE turboshaft engines T408, 7,500 shp
- 电机
- 1 electric motor
- 旋翼／螺旋桨
- 2 turbine powered propellers, 1 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
- Long-range heavy-lift hybrid-electric VTOL passenger and cargo concept design military aircraft
- Piloting
- 1 pilot, autonomous capable
- Capacity
- 100 people, maximum 365 lb (166 kg) each person
- Cruise speed
- 529 mph (851 km/h)
- Range
- 5,824 miles (9,373 km)
- Maximum operating altitude
- 30,000 ft (9,144 m)
- Empty weight
- 63,000 lb (28,576 kg)
- Maximum payload
- 42,000 lb (19,051 kg)
- Maximum takeoff weight
- 105,000 lb (47,627 kg)
- Cabin volume
- ~5,000 cubic feet
- Propellers
- 2 turbine powered propellers, 1 electric tailfan propeller
- Electric motors
- 1 electric motor
- Power source
- 5 GE turboshaft engines T408, 7,500 shp
- Fuselage
- Carbon fiber composite
- Windows
- The aircraft has typical military windows
- Wings
- 1 high wing
- Tail
- 1 H-tail
- Landing gear
- Retractable wheeled landing gear, dual nose wheels and a 4-wheel truck main on each side of the rear bogies
- 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.
明确提及本机型的报道
暂无明确匹配的公开报道；通用或重名型号不会自动关联。
目录参数变化记录
从保存的目录刷新快照比较，资料修改不等于实机性能发生变化。
暂无已保存的版本变化，后续目录刷新将保留快照。