← eVTOL产品
Bartini Aero, Inc. · USA
Bartini
Bartini
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 (when autonomous, 4 passengers)
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot (in the future will be autonomous)
- 航程（按来源口径）
- 未公开／未录入
- 巡航速度
- 186 mph (300 km/h)
- 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
- Lithium batteries or hydrogen fuel cells
- 电机
- 8 electric motors
- 旋翼／螺旋桨
- 8 ducted propellers
- 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 in the sub-systems of the aircraft.
全部原始参数
Specifications:
- Aircraft type
- Hybrid-electric or all-electric VTOL passenger aircraft
- Piloting
- 1 pilot (in the future will be autonomous)
- Capacity
- 3 passengers (when autonomous, 4 passengers)
- Cruise speed
- 186 mph (300 km/h)
- Range with batteries
- 93 m (150 km)
- Range hydrogen fuel cells
- 342 m (550 km)
- Flight time with battery packs
- 30 minutes
- Flight time with hydrogen fuel cells
- 2 hours
- Ducts
- 4 tilting-ducts
- Propellers
- 8 ducted propellers
- Electric Motors
- 8 electric motors
- Power source
- Lithium batteries or hydrogen fuel cells
- Fuselage
- Carbon fiber composite
- Windows
- Panoramic wrap around windows allowing forward, left, right visibility for spectacular views with a solid roof above the passenger compartment
- Landing gear
- 4 fixed landing legs
- 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 in the sub-systems of the aircraft.