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Pegasus Universal Aerospace · South Africa

Vertical Business Jet VBJ

Pegasus Universal Aerospace Vertical Business Jet

复合翼(升力+巡航) · 概念设计 · 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:Pegasus Universal Aerospace

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 ↗

概念参数,尚不代表已实现性能

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主要参数

座位/载员
未公开/未录入
乘客
1 pilot, 6 passengers
驾驶方式
未公开/未录入
航程(按来源口径)
未公开/未录入
巡航速度
759 km/h (472 mph)
最大速度
796 km/h (495 mph)
最大起飞重量
5,700 kg (12,566 lb)
载荷
未公开/未录入
空重
3,040 kg (6,702 lb)
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
未公开/未录入
电机
未公开/未录入
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
10,668 m (35,000 ft)
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 its passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy for its passengers or cargo. Having multiple redundant systems on any aircraft decreases having any single point of failure.

全部原始参数

Specifications:

Aircraft type
Passenger hybrid-electric VTOL jet aircraft
Passengers
1 pilot, 6 passengers
Cruise speed
759 km/h (472 mph)
Maximum speed
796 km/h (495 mph)
Range using VTOL capability
2,124 km (1,320 m)
Range using conventional runways
4,400 km (2,743 m)
Maximum flight time VTOL mode
Approximately 3 hours
Maximum flight time conventional takeoff
Approximately 6-1/2 hours
Maximum altitude
10,668 m (35,000 ft)
Empty weight
3,040 kg (6,702 lb)
Maximum payload weight
2,660 kg (5,864 lb)
Maximum takeoff weight
5,700 kg (12,566 lb)
Propellers for VTOL flight
8 electric propellers-in-wing with , two propellers are pair of fans are counter rotating, with bottom and top louvers that close during forward flight
Engines for forward flight
2 GE Aviation CT7-8 turboshaft engines, 2,300 shp
Main Wings
Cranked dihedral wings with winglets
Tail
V-tail and two horizontal stabilizers
Landing Gear
Retractable 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 its passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy for its passengers or cargo. 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。