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Side-by-Side

NASA Side-by-Side

直升机 · 概念设计 · 核查 2026-10-01

飞行构型与公司名称

直升机

Aircraft type: Passenger eVTOL concept design helicopter

核对构型依据 ↗

原始目录分组:电动旋翼机

中文名称:待核实 · 原名:NASA

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 · 概念设计 · 目录依据 · 目录阶段,尚未核实批准状态

查看状态依据 ↗

巡航速度未纳入:单位或条件未能一致解析

概念参数,尚不代表已实现性能

订阅本机型报道 RSS →

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.

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。