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Elytron Aircraft LLC (out of business) · USA
Elytron 4S
Elytron Aircraft Elytron 4S
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
- 3 passengers
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- 1,022 m (1,646 km)
- 巡航速度
- 未公开／未录入
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 未公开／未录入
- 载荷
- 1,100 lb (500 kg)
- 空重
- 2,420 lb (1,100 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 using 2 turbine engines for the power source
- 电机
- 2 electric motors
- 旋翼／螺旋桨
- 2 prop-propellers
- 续航时间
- 未公开／未录入
- 飞行高度
- 30,000 ft (9,144 m)
- 安全设计
- The aircraft can land conventionally as an airplane if the propellers stop working. In case of an emergency water landing, the front wing acts as a hydrofoil.
全部原始参数
Specifications:
- Aircraft type
- Hybrid-electric VTOL passenger concept design aircraft
- Piloting
- 1 pilot
- Capacity
- 3 passengers
- Maximum cruise speed
- 316 mph (196 km/h)
- Range
- 1,022 m (1,646 km)
- Maximum altitude
- 30,000 ft (9,144 m)
- Empty weight
- 2,420 lb (1,100 kg)
- Maximum payload
- 1,100 lb (500 kg)
- Maximum takeoff weight at sea level
- 4,422 lb (2,006 kg)
- Propellers
- 2 prop-propellers
- Electric motors
- 2 electric motors
- Power source
- Hybrid-electric using 2 turbine engines for the power source
- Fuselage
- Carbon fiber composite
- Window
- Canopy over cockpit
- Wings
- 1 high main tilt-wing and 1 box wing
- Tail
- 1 vertical stabilizer
- Landing gear
- Retractable tricycle wheeled landing gear
- Safety features
- The aircraft can land conventionally as an airplane if the propellers stop working. In case of an emergency water landing, the front wing acts as a hydrofoil.