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Aeroelektromash JSC · Russia
R-34
Aeroelektromash R-34
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
- 2 passengers
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- 350-600 km (217-373 m)
- 巡航速度
- 130 km/h (81 mph)
- 最大速度
- 170 km/h (105 mph)
- 最大起飞重量
- 590 kg (1,301 lb)
- 载荷
- 280 kg (618 lb)
- 空重
- 310 kg (6831 lb)
- 长度
- 4.95 m (16 feet, 2-7/8 inches)
- 翼展
- 未公开／未录入
- 高度
- 2.85 m (9 feet, 7-/32 inches)
- 动力来源
- Rotax 915 engine rated at 96 kW (130 h.p.)
- 电机
- 1 ВД-25000, its rated power is 25 kW (34 hp), with an approximate nominal rotation speed of 2,500 rpm
- 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 or can deploy its whole aircraft emergency parachute
全部原始参数
Specifications:
- Aircraft type
- Hybrid-electric ultralight passenger helicopter prototype
- Piloting
- 1 pilot
- Capacity
- 2 passengers
- Cruise speed
- 130 km/h (81 mph)
- Maximum speed
- 170 km/h (105 mph)
- Range
- 350-600 km (217-373 m)
- Maximum altitude
- 4,500 m (14,764 ft)
- Rate of climb
- 5.5 meters per second (18 ft per second)
- Empty weight
- 310 kg (6831 lb)
- Maximum payload
- 280 kg (618 lb)
- Maximum takeoff weight
- 590 kg (1,301 lb)
- Rotorblades
- Coaxial rotorblades, no tail rotor
- Electric motor
- 1 ВД-25000, its rated power is 25 kW (34 hp), with an approximate nominal rotation speed of 2,500 rpm
- Power source
- Rotax 915 engine rated at 96 kW (130 h.p.)
- Fuel capacity
- 50 l (13.21 gal)
- Fuselage
- Carbon fiber composite
- Length
- 4.95 m (16 feet, 2-7/8 inches)
- Height
- 2.85 m (9 feet, 7-/32 inches)
- Rotorblade diameter
- 6.30 m (20 feet, 8-1/32 inches)
- Windows
- Large helicopter windows
- Tail
- 2 rear inverted angled vertical stabilizers
- Landing gear
- Fixed skid landing gear
- Safety features
- In case of a power failure, the helicopter can autorotate to safety or can deploy its whole aircraft emergency parachute