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Sirius Aviation AG · Switzerland
Sirius Hybrid-Electric VTOL Jet
Sirius Aviation Sirius Hybrid-Electric VTOL Jet
矢量推力 · 停研/历史型号 · 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。
资料覆盖与状态依据
可用性能指标 2/3 · 停研/历史型号 · 目录阶段,尚未核实批准状态
查看状态依据 ↗订阅本机型报道 RSS →主要参数
- 座位/载员
- Unknown
- 乘客
- 未公开/未录入
- 驾驶方式
- 1 pilot
- 航程(按来源口径)
- 800 km (497 miles)
- 巡航速度
- 299 km/h (186 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
- Battery packs
- 电机
- 24 electric motors
- 旋翼/螺旋桨
- 24 electric ducted fans (EDFs)
- 续航时间
- 未公开/未录入
- 飞行高度
- 未公开/未录入
- 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
- Long-range hydrogen-electric VTOL concept design jet aircraft
- Piloting
- 1 pilot
- Capacity
- Unknown
- Cruise speed
- 299 km/h (186 mph)
- Range
- 800 km (497 miles)
- Propellers
- 24 electric ducted fans (EDFs)
- Electric motors
- 24 electric motors
- Power source
- Battery packs
- Noise
- <60 dB at a 100 meters (328 ft) distance
- Fuselage
- Carbon fiber composite
- Windows
- Larger than conventional business jet windows
- Wings
- 1 canard wing with winglets and 1 main high wing with winglets
- 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.
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。