Rotor X Aircraft Manufacturing Company · USA

eJavelin

Rotor X eJavelin

旋翼机（待细分） · 阶段未核实 · 核查 2026-10-01

飞行构型与公司名称

旋翼机（待细分）

VFS 原始目录分组：电动旋翼机。尚无足够资料确定具体布局。

原始目录分组：电动旋翼机

中文名称：待核实 · 原名：Rotor X Aircraft Manufacturing Company

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。

可用性能指标 0/3 · 阶段未核实 · 目录依据 · 目录阶段，尚未核实批准状态

Capacity: 1 pilot
Maximum speed: 85 mph (164 km/h)
Flight time: 2 hours, 15 minutes
Service ceiling: 11,500 ft (3,505 m)
Engine: Continental O-200, 100 hp petroleum powered engine
Empty weight: 500 lb (227 kg)
Gross weight: 880 lb (399 kg)
Fuel capacity: 12 gal (45.4 l)
Rotorblade: 1 main rotorblade
Main rotor diameter: 21.4 ft (6.52 m)
Tail rotor: 1 tail rotor
Windows: Full front window with plexiglass framed doors (the production model which was never built, was to have plexiglass doors)
Landing gear: Fixed skid helicopter landing gear
Safety feature: Can use autorotation to land, in case of an engine failure

Aircraft type: Electric helicopter
Capacity: 2 people (1 pilot and 1 passenger)
Cruise speed: Unknown
Range: Unknown
Flight Time: Unknown
Rotorblade: 1 main rotorblade
Tail rotor: 1 tail rotor
Electric Motors: Possibly 1 electric motor, unknown at this time
Power source: Batteries
Fuselage: Carbon fiber composite
Windows: Unknown
Tail: Unknown if tail will have a standard helicopter vertical stabilizer, ventral fin and tail boom elevators
Landing gear: Fixed skid landing gear
Safety feature: Ability to autorotate and land, in case of emergency

暂无明确匹配的公开报道；通用或重名型号不会自动关联。

从保存的目录刷新快照比较，资料修改不等于实机性能发生变化。

暂无已保存的版本变化，后续目录刷新将保留快照。