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Electrofluidsystems · Germany

H2PlasmaRay 6.66

Electrofluidsystems H2PlasmaRay 6.66

升力+巡航 · 阶段未核实 · 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 0/3 · 阶段未核实 · 目录依据 · 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
2 passengers
乘客
未公开/未录入
驾驶方式
Pilot optional or autonomous
航程(按来源口径)
未公开/未录入
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
900 kg (1,984 lbs)
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
Hydrogen fuel cells, liquid hydrogen fuel cells, solid state batteries (when they become available.)
电机
48 / 195 mm diameter (Over 7.5 inches in diameter)
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
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 and motors on the aircraft so if one or more motors or propellers fail, the other working motors and propellers can safely land the aircraft. In the event of a catastrophic failure, the aircraft will also have a ballistic parachute allowing the passengers to land safely.

全部原始参数

Specifications:

Aircraft type
Hybrid-electric VTOL (in the future eVTOL)
Piloting
Pilot optional or autonomous
Capacity
2 passengers
Maximum takeoff weight
900 kg (1,984 lbs)
Ducted electric fans
48 (38 VTOL ducted fans, 10 forward flight ducted fans)
Electric motors
48 / 195 mm diameter (Over 7.5 inches in diameter)
Continous thrust
950 kg (2,094 lbs) of static thrust in continuous mode
Top thrust
1050 kg (2,315 lbs) for a short period of time
Power source
Hydrogen fuel cells, liquid hydrogen fuel cells, solid state batteries (when they become available.)
Wing
Blended wing body, 6.66 meters wide (~22 feet wide)
Landing gear
Retractable wheeled landing gear
Safety features
Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers and motors on the aircraft so if one or more motors or propellers fail, the other working motors and propellers can safely land the aircraft. In the event of a catastrophic failure, the aircraft will also have a ballistic parachute allowing the passengers to land safely.

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。