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Embraer · Brazil
Pulse Concept
Embraer Pulse Concept
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
- Unknown (possibly 4 to 6 people)
- 乘客
- 未公开/未录入
- 驾驶方式
- 1 pilot or autonomous, air and ground
- 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
- 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
- Most likely, hybrid-electric power source including batteries
- 电机
- 4 electric motors
- 旋翼/螺旋桨
- 4 propellers (stacked 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
- Using electric motors instead of conventional piston or turbine engines to power the propellers increases the safety of the aircraft. There are redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. Having multiple redundant systems on any aircraft decreases having any single point of failure.
全部原始参数
Specifications:
- Aircraft type
- Passenger pod which fits inside eVTOL and electric car vehicles
- Piloting
- 1 pilot or autonomous, air and ground
- Capacity
- Unknown (possibly 4 to 6 people)
- Passenger pod
- All glass, with use of futuristic glass and transparent aluminum
- Propellers
- 4 propellers (stacked propellers)
- Electric motors
- 4 electric motors
- Power source
- Most likely, hybrid-electric power source including batteries
- Windows
- Canopy over the cockpit and entire passenger compartment for excellent views in all directions for the pilot and passengers
- Wing
- 1 joined wing
- Tail
- 1 sloping rearward vertical stabilizer
- Ground vehicle
- 6 wheels
- Landing gear (aircraft)
- Retractable tricycle tail wheeled landing gear
- Safety features
- Using electric motors instead of conventional piston or turbine engines to power the propellers increases the safety of the aircraft. There are redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. Having multiple redundant systems on any aircraft decreases having any single point of failure.