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Baaz · Germany

Baaz B5

Baaz Production Model

其他推力转向(待细分) · 生产型设计 · 核查 2026-10-01

飞行构型与公司名称

其他推力转向(待细分)

VFS 原始目录分组:矢量推力。尚无足够资料确定具体布局。

核对构型依据 ↗

原始目录分组:矢量推力

中文名称:待核实 · 原名:Baaz

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 1/3 · 生产型设计 · 目录依据 · 目录阶段,尚未核实批准状态

查看状态依据 ↗

航程未纳入:单位或条件未能一致解析

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主要参数

座位/载员
At the start, 1 pilot, 4 passengers, later piloted by AI
乘客
未公开/未录入
驾驶方式
Piloting at first, then autonomous piloting using predictive analytics, artificial intelligence (AI) and machine learning (ML)
航程(按来源口径)
200 km (124 m) with Lithium-ion batteries, 300 km (186 m) with hydrogen fuel cells
巡航速度
未公开/未录入
最大速度
300 km/h (186 mph)
最大起飞重量
未公开/未录入
载荷
600 kg (1,323 lb)
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
Powered by swappable lithium-ion batteries for travel within a city or can be powered by hydrogen fuel cells for travel between two cities.
电机
9 electric motors for propellers (there more electric motors for landing gear, folding wings and for openings for middle VTOL propeller)
旋翼/螺旋桨
9 propellers (4 rotating ducted propellers nacelles, each nacelle has 2 sets of propellers, 1 propellers is in the rear of the fuselage for vertical flight)
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 motor or propeller fails, the other working motors and propellers can safely land the aircraft.

全部原始参数

Specifications:

Aircraft type
eVTOL and hybrid-electric VTOL aircraft
Piloting
Piloting at first, then autonomous piloting using predictive analytics, artificial intelligence (AI) and machine learning (ML)
Capacity
At the start, 1 pilot, 4 passengers, later piloted by AI
Maximum speed
300 km/h (186 mph)
Range
200 km (124 m) with Lithium-ion batteries, 300 km (186 m) with hydrogen fuel cells
Maximum payload
600 kg (1,323 lb)
Propellers
9 propellers (4 rotating ducted propellers nacelles, each nacelle has 2 sets of propellers, 1 propellers is in the rear of the fuselage for vertical flight)
Electric Motors
9 electric motors for propellers (there more electric motors for landing gear, folding wings and for openings for middle VTOL propeller)
Power source
Powered by swappable lithium-ion batteries for travel within a city or can be powered by hydrogen fuel cells for travel between two cities.
Fuselage height
1.5 m (4 ft, 11.1 in)
Fuselage width
1.8 m (5 ft, 11 in)
Fuselage length
2.0 m (6 ft, 6.7 in)
Total width wings open
13.5 m (44 ft, 3.5 in)
Total width wings closed
7.8 m (25 ft, 7.1 in)
Total length
7.8 m (25 ft, 7.1 in)
Windows
Large windows for spectacular views
Wing
One low main wing with winglets and the wing is foldable allowing the aircraft to park in tight spaces. The wing can unfold and fold while hovering so that it can take off or land in a very small space.
Tail
One vertical stabilizer
Landing gear
Retractable tricycle 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 motor or propeller fails, the other working motors and propellers can safely land the aircraft.

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。