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NASA · USA

Tiltduct

NASA Tiltduct

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
6 passengers
乘客
未公开/未录入
驾驶方式
Unknown, possibly piloted or autonomous
航程(按来源口径)
未公开/未录入
巡航速度
174 mph (280 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
All batteries or a hybrid-electric power source
电机
6 electric motors (or double the amount depending upon the manufacturer)
旋翼/螺旋桨
6 tilt ducts (8 VTOL-only propellers, 1 pusher propeller for forward 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) 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 aircraft
Piloting
Unknown, possibly piloted or autonomous
Capacity
6 passengers
Cruise speed
174 mph (280 km/h)
Reserve cruise power
20 minutes
Empty weight, estimated
5,889 lb (2,672 kg)
Maximum payload weight, estimated
1,200 lb (544 kg)
Maximum takeoff weight, estimated
7,089 lb (3,216 kg)
Propellers
6 tilt ducts (8 VTOL-only propellers, 1 pusher propeller for forward flight)
Electric motors
6 electric motors (or double the amount depending upon the manufacturer)
Power source
All batteries or a hybrid-electric power source
Fuselage
Carbon fiber composite
Windows
Panoramic wrap around windows allowing forward, left and right visibility for spectacular views with a solid roof above
Wings
1 canard and 1 main high wing
Tail
1 tail fin (or vertical stabilizer) and 1 horizontal stabilizer
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.