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Pegasus International Group · Australia
Pegasus E Class
Pegasus International Group Pegasus E Class
电动旋翼机 · 生产型设计 · 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
- 1 person, 2 person and 4 person models
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- 未公开／未录入
- 巡航速度
- 未公开／未录入
- 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
- Hybrid-electric power source (uses batteries for ground travel and a piston engine and batteries for flight)
- 电机
- Unknown
- 旋翼／螺旋桨
- 未公开／未录入
- 续航时间
- 3 hours
- 飞行高度
- 1,800 m (5,906 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. If there is a power loss during flight, the aircraft can autorotate and land safely.
全部原始参数
Specifications:
- Aircraft type
- Passenger hybrid-electric helicopter and road vehicle
- Piloting
- 1 pilot
- Capacity
- 1 person, 2 person and 4 person models
- Time to change from VTOL to road vehicle
- 3 seconds
- Top speed (ground)
- 120 km/h (75 mph)
- Cruise speed (air)
- 132 km/h (82 mph)
- Maximum speed (air)
- 160 km/h (99 mph)
- Range (ground)
- 75 km (47 m)
- Range (air)
- 482 km (300 miles)
- Flight time
- 3 hours
- Maximum altitude
- 1,800 m (5,906 ft)
- Maximum payload weight
- 195 kg (423 lb)
- Rotorblade
- 1 main rotorblade
- Tail rotor
- 1 tail rotor
- Electric motors
- Unknown
- Power source
- Hybrid-electric power source (uses batteries for ground travel and a piston engine and batteries for flight)
- Fuselage
- Carbon fiber composite
- Window
- Canopy over cockpit
- Landing gear
- Fixed quadricycle road wheels
- 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. If there is a power loss during flight, the aircraft can autorotate and land safely.