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NASA Langley · USA

Greased Lightning (GL-10)

NASA Greased Lightning

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
No passengers but there was a small payload area where the cockpit of the aircraft would have been located
乘客
未公开/未录入
驾驶方式
Remote piloting
航程(按来源口径)
Unknown
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
62 lb (28 kg)
载荷
未公开/未录入
空重
46 lb (21 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
Batteries and two diesel engines (Launchpoint Technologies Genset)
电机
10 electric motors (Scorpion SII-4020-360KV)
旋翼/螺旋桨
10 propellers (Aeronaut CAM Carbon 16x8”)
续航时间
未公开/未录入
飞行高度
Unknown
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
Uncrewed subscale hybrid-electric VTOL technology demonstrator
Piloting
Remote piloting
Capacity
No passengers but there was a small payload area where the cockpit of the aircraft would have been located
Cruise speed, estimated
70 mph (113 km/h)
Range
Unknown
Cruise altitude
Unknown
Empty weight
46 lb (21 kg)
Maximum payload weight
16 lb (7 kg)
Maximum takeoff weight
62 lb (28 kg)
Propellers
10 propellers (Aeronaut CAM Carbon 16x8”)
Electric motors
10 electric motors (Scorpion SII-4020-360KV)
Power source
Batteries and two diesel engines (Launchpoint Technologies Genset)
Fuselage
Carbon fiber composite with a front SpaceAge Controls Alpha/Beta Pitot Tube
Windows
No windows
Wings
1 main high swept back tilt-wing (10-foot wingspan or 3.05 meters)
Tail
1 rear tilt-horizontal stabilizer with dihedral angle with 3 vertical stabilizers
Landing gear
Retractable landing skids
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.