Aurora Flight Sciences, a Boeing Company · USA

Pegasus Passenger Air Vehicle (PAV)

Aurora Flight Sciences (Boeing) Pegasus PAV

升力＋巡航 · 原型机 · 核查 2026-10-01

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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: 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.