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Aeroelektromash JSC · Russia
VA-115
Aeroelektromash VA-115
电动旋翼机 · 原型机 · 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
- 未公开／未录入
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- 未公开／未录入
- 巡航速度
- 80 km/h (50 mph)
- 最大速度
- 110 km/h (68 mph)
- 最大起飞重量
- 260 kg (573 lbs)
- 载荷
- 121 kg (267 lbs)
- 空重
- 139 kg (306 lb)
- 长度
- 3.7 m (12 ft, 2-2/3 inches)
- 翼展
- 未公开／未录入
- 高度
- 2.6 m (8 ft, 6.7/16 inches)
- 动力来源
- 2 Hirth Engines GmbH F23 RS-01 2 cylinder boxer two stroke
- 电机
- 2 electric motors 24 kW (34 h.p.)
- 旋翼／螺旋桨
- 未公开／未录入
- 续航时间
- 未公开／未录入
- 飞行高度
- 4,500 m (14,764 ft)
- 安全设计
- In case of a power failure, the helicopter can autorotate to safety.
全部原始参数
Specifications:
- Aircraft type
- Hybrid-electric ultralight passenger training helicopter prototype
- Piloting
- 1 pilot
- Cruise speed
- 80 km/h (50 mph)
- Maximum speed
- 110 km/h (68 mph)
- Maximum altitude
- 4,500 m (14,764 ft)
- Rate of climb
- 4.0 m/s (13.1 ft per second)
- Empty weight
- 139 kg (306 lb)
- Maximum payload
- 121 kg (267 lbs)
- Maximum takeoff weight
- 260 kg (573 lbs)
- Rotorblades
- Coaxial rotorblades
- Electric motor
- 2 electric motors 24 kW (34 h.p.)
- Power source
- 2 Hirth Engines GmbH F23 RS-01 2 cylinder boxer two stroke
- Fuel capacity
- 30 l (8 gal.)
- Fuselage
- Aircraft aluminum and carbon fiber composite
- Length
- 3.7 m (12 ft, 2-2/3 inches)
- Width
- 1.6 m (5 ft, 2-31/32 inches)
- Height
- 2.6 m (8 ft, 6.7/16 inches)
- Rotorblade diameter
- 4.5 m (14 ft, 9-1/6 inches)
- Cockpit
- Open cockpit
- Tail
- H-tail
- Landing gear
- Fixed tricycle wheeled landing gear
- Safety features
- In case of a power failure, the helicopter can autorotate to safety.