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Baaz · Germany
Baaz B5
Baaz Production Model
矢量推力 · 生产型设计 · 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
- 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.