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Pegasus Universal Aerospace · South Africa
Vertical Business Jet VBJ
Pegasus Universal Aerospace Vertical Business Jet
升力＋巡航 · 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
- 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.