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Side-by-Side
NASA Side-by-Side
电动旋翼机 · 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
- 6 total people
- 乘客
- 未公开／未录入
- 驾驶方式
- Piloted or autonomous
- 航程（按来源口径）
- 86 m (138 km)
- 巡航速度
- Unknown
- 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
- All batteries or a hybrid-electric power source
- 电机
- 2 or more electric motors
- 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) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for passengers or cargo. There are also 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 eVTOL concept design helicopter
- Piloting
- Piloted or autonomous
- Capacity
- 6 total people
- Cruise speed
- Unknown
- Range
- 86 m (138 km)
- Reserve cruise power
- 20 minutes
- Maximum payload weight, estimated
- 1,200 lb (544 kg)
- Rotorblades
- 2 rotorblades that are side-by-side
- Electric motors
- 2 or more electric motors
- Power source
- All batteries or a hybrid-electric power source
- Fuselage
- Carbon fiber composite
- Windows
- Conventional helicopter windows
- Tail
- 1 inverted V tail
- Landing gear
- Fixed tricycle wheeled landing gear
- Safety features
- Distributed Electric Propulsion (DEP) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for passengers or cargo. There are also 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.