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Aurora Flight Sciences, a Boeing Company · USA

Pegasus Passenger Air Vehicle (PAV)

Aurora Flight Sciences (Boeing) Pegasus PAV

复合翼(升力+巡航) · 原型机 · 核查 2026-10-01

飞行构型与公司名称

复合翼(升力+巡航)

VFS 原始目录分组:升力+巡航。按目录所述推进方式归类。

核对构型依据 ↗

原始目录分组:升力+巡航

中文名称:待核实 · 原名:Aurora Flight Sciences, a Boeing Company

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 · 原型机 · 目录依据 · 目录阶段,尚未核实批准状态

查看状态依据 ↗订阅本机型报道 RSS →

主要参数

座位/载员
No passengers
乘客
未公开/未录入
驾驶方式
Autonomous
航程(按来源口径)
未公开/未录入
巡航速度
56 mph (90 km/h)
最大速度
未公开/未录入
最大起飞重量
27.6 lb (12.5 kg)
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
Battery packs
电机
9 electric motors, 8 X 100 hp (8 X 75 kW)
旋翼/螺旋桨
8 VTOL propellers, 1 pusher propeller
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

1/4 Subscale PAV Specifications:

Aircraft type
Subscale eVTOL prototype aircraft
First flight
April 2017
Piloting
Autonomous
Capacity
No passengers
Cruise speed
56 mph (90 km/h)
Maximum takeoff weight
27.6 lb (12.5 kg)
Propellers
8 VTOL propellers, 1 pusher propeller
Electric motors
9 electric motors, 8 X 100 hp (8 X 75 kW)
Power source
Battery packs
Fuselage
6.6 ft (2 m) length, 6.6 ft (2 m) width
Wings
1 main low main wing with winglets, 2 low booms parallel to the fuselage to hold the 8 VTOL propellers, 1 canard (or forewing)
Tail
1 U tail on the ends of the 2 booms, 2 downward angled vertical stabilizers under the rear of the fuselage
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.

Full-Scale PAV Specifications:

Aircraft type
Full-scale passenger eVTOL prototype aircraft
First flight
January 22, 2019
Piloting
Autonomous
Capacity
2 passengers
Cruise speed
112 mph (180 km/h)
Range
50 miles (80 km)
Flight time
Cruise altitude
Empty weight
1,265 lb (565 (kg)
Maximum payload weight
496 lb (225 kg)
Maximum takeoff weight
1,761 lb (790 kg)
Propellers
8 VTOL propellers, 1 pusher propeller
Electric motors
9 electric motors, 8 X 100 hp (8 X 75 kW)
Power source
Battery packs
Fuselage
Carbon fiber composite or aircraft aluminum or both, 30 ft (9.14 m) length, 28 ft (8.53 m) width (wingspan)
Wings
1 main low main wing with winglets, 2 low booms parallel to the fuselage to hold the 8 VTOL propellers, 1 forward swept canard (or small forewing)
Tail
1 U tail on the ends of the 2 booms, 2 downward angled vertical stabilizers under the rear of the fuselage that connect to the U tail
Landing gear
Fixed quadricycle landing struts
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。