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Aura Aerospace LLC · USA
Ranger
Aura Aerospace Ranger
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
- 5 passengers, a food galley, lavatory and room for luggage
- 乘客
- 未公开/未录入
- 驾驶方式
- Automatic pilot with manual override
- 航程(按来源口径)
- 11,185 miles (18,000 km)
- 巡航速度
- 510 mph (820 km/h)
- 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
- Battery packs
- 电机
- 8 electric motors
- 旋翼/螺旋桨
- 8 VTOL-only propellers. The propellers pop-out from the front and rear of the fuselage when in VTOL flight. During forward flight, all propellers retract inside the fuselage and are protected by caps.
- 续航时间
- 22 hours
- 飞行高度
- 10,000 ft (3,050 m)
- 安全设计
- Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. 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. The aircraft has full glide capability if it had to make an emergency landing.
全部原始参数
Specifications:
- Aircraft type
- Passenger ultra-long range hybrid-electric VTOL concept design aircraft
- Piloting
- Automatic pilot with manual override
- Capacity
- 5 passengers, a food galley, lavatory and room for luggage
- Cruise speed
- 510 mph (820 km/h)
- Range
- 11,185 miles (18,000 km)
- Flight time
- 22 hours
- Cruise altitude
- 10,000 ft (3,050 m)
- Maximum altitude
- 15,000 ft (4,572 m)
- Propellers
- 8 VTOL-only propellers. The propellers pop-out from the front and rear of the fuselage when in VTOL flight. During forward flight, all propellers retract inside the fuselage and are protected by caps.
- Electric motors
- 8 electric motors
- Power source
- Battery packs
- Forward flight propulsion
- 2 turbofan jet engines that use sustainable aviation fuel (SAF). The jet engines charge the batteries during flight
- Fuselage
- Carbon fiber composite
- Window
- Canopy over cockpit
- Wing
- 1 main wing (foldable wing). When wing is extended, 75 ft (23 m)
- Vertical stabilizers
- 2 under fuselage vertical stabilizers
- Landing gear
- Retractable quadricycle wheeled landing gear
- Safety features
- Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. 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. The aircraft has full glide capability if it had to make an emergency landing.