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ARC Aerosystems · United Kingdom
Starling Jet
ARC Aerosystems Starling Jet
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
- 10 passengers
- 乘客
- 未公开／未录入
- 驾驶方式
- Piloted at first and in the future the aircraft have autonomous piloting
- 航程（按来源口径）
- 1,450-2,414 km (900-1,500 miles)
- 巡航速度
- 740 km/h (460 mph)
- 最大速度
- 未公开／未录入
- 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
- 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 and battery packs. The batteries will be charged by the jet engines during forward flight.
- 电机
- 2 electric motors (maybe more)
- 旋翼／螺旋桨
- 未公开／未录入
- 续航时间
- 未公开／未录入
- 飞行高度
- 9,100 m (29,855 ft)
- 安全设计
- 未公开／未录入
全部原始参数
Specifications:
- Aircraft type
- Hybrid-electric VTOL passenger concept design aircraft
- Piloting
- Piloted at first and in the future the aircraft have autonomous piloting
- Capacity
- 10 passengers
- Cruise speed
- 740 km/h (460 mph)
- Range
- 1,450-2,414 km (900-1,500 miles)
- Maximum altitude
- 9,100 m (29,855 ft)
- VTOL propellers
- 2 propellers (hidden in the fuselage until needed)
- Jet engines
- 3 jet engines
- Electric Motors
- 2 electric motors (maybe more)
- Power source
- Hybrid-electric and battery packs. The batteries will be charged by the jet engines during forward flight.
- Fuselage
- Carbon fiber composite
- Windows
- Round windows
- Wings
- 1 main high wing with winglets
- Tail
- V-tail
- Landing gear
- Retractable wheeled landing gear