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Rotor X Aircraft Manufacturing Company · USA
eJavelin
Rotor X eJavelin
电动旋翼机 · 阶段未核实 · 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 pilot
- 乘客
- 未公开／未录入
- 驾驶方式
- 未公开／未录入
- 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
- 85 mph (164 km/h)
- 最大起飞重量
- 未公开／未录入
- 载荷
- 未公开／未录入
- 空重
- 500 lb (227 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
- 未公开／未录入
- 电机
- 未公开／未录入
- 旋翼／螺旋桨
- 未公开／未录入
- 续航时间
- 2 hours, 15 minutes
- 飞行高度
- 未公开／未录入
- 安全设计
- 未公开／未录入
全部原始参数
Javelin Helicopter Specifications 1960s (For The Planned Production Model):
- 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
Specifications:
- 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