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Aurora Flight Sciences, A Boeing Company · USA
XV-24 LightningStrike
Aurora Flight Sciences (Boeing) XV-24 LightningStrike
矢量推力 · 停研／历史型号 · 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
- Weapons
- 乘客
- 未公开／未录入
- 驾驶方式
- Autonomous or remote
- 航程（按来源口径）
- Unknown
- 巡航速度
- >345 mph (>555 km/h)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- ~13,000 lb (~5,897 kg)
- 载荷
- 未公开／未录入
- 空重
- ~11,375 lb (~5,160 kg)
- 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. 1 Rolls-Royce AE1107C turboshaft 4,023 hp engine (used on the V-22 Osprey) to generate electric power by three Honeywell generators for the 24 electric ducted fans.
- 电机
- 24 electric motors (motor output: 18x 168 hp + 6x 121 hp, 18x 125 kW + 6x 90 kW)
- 旋翼／螺旋桨
- 24 electric ducted fans (EDFs)
- 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
Specifications:
- Aircraft type
- Hybrid-electric VTOL weapons platform concept design aircraft
- Piloting
- Autonomous or remote
- Capacity
- Weapons
- Cruise speed
- >345 mph (>555 km/h)
- Range
- Unknown
- Empty weight
- ~11,375 lb (~5,160 kg)
- Maximum payload weight
- ~1,625 lb (~737 kg)
- Maximum takeoff weight
- ~13,000 lb (~5,897 kg)
- Propellers
- 24 electric ducted fans (EDFs)
- Electric motors
- 24 electric motors (motor output: 18x 168 hp + 6x 121 hp, 18x 125 kW + 6x 90 kW)
- Power source
- Hybrid-electric power source. 1 Rolls-Royce AE1107C turboshaft 4,023 hp engine (used on the V-22 Osprey) to generate electric power by three Honeywell generators for the 24 electric ducted fans.
- Fuselage
- Carbon fiber composite
- Dimensions
- >38 ft (11.8 m) length, ~14 ft (4.3 m) height, >60 ft (18.2 m) width (or wingspan)
- Wings
- 1 tilt canard wing with EDFs in the middle of the entire wing with winglets, 1 rear high-main wing with EDFs in the middle of the entire wing with winglets
- 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 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.