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Sirius Aviation AG · Switzerland
Sirius Business Jet
Sirius Aviation Sirius Business 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
- 3 passengers
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- 1,850 km (1,150 m)
- 巡航速度
- 600 km/h (323 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 (using liquid-hydrogen fuel, high temperature fuel cells and batteries)
- 电机
- 28 electric motors
- 旋翼／螺旋桨
- 28 electric ducted fans (EDFs)
- 续航时间
- 未公开／未录入
- 飞行高度
- 9,144 m (30,000 ft)
- 安全设计
- Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. There are also redundancies of critical components in the sub-systems of the aircraft. There is a whole aircraft emergency ballistic parachute.
全部原始参数
Specifications:
- Aircraft type
- Hybrid-electric VTOL regional concept design aircraft
- Piloting
- 1 pilot
- Capacity
- 3 passengers
- Cargo only
- 1,100 liters (5.1 M3 or CA.39FT3)
- Cruise speed
- 600 km/h (323 mph)
- Range
- 1,850 km (1,150 m)
- Cruise altitude
- 9,144 m (30,000 ft)
- Propellers
- 28 electric ducted fans (EDFs)
- Electric motors
- 28 electric motors
- Power source
- Hybrid-electric (using liquid-hydrogen fuel, high temperature fuel cells and batteries)
- Noise
- <60 dB at a 100 meters distance
- Fuselage
- Carbon fiber composite
- Windows
- Larger than standard small jet windows
- Wings
- 1 canard with winglets and 1 main high wing with winglets
- Tail
- 1 V tail
- Landing gear
- Retractable tricycle wheeled landing gear
- Safety features
- Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. There are also redundancies of critical components in the sub-systems of the aircraft. There is a whole aircraft emergency ballistic parachute.