产品描述
This is a micro turbojet engine specially developed for target drones and small tactical missiles.
Design Features
Compressor: 1-stage centrifugal type with a boost ratio of 3.9.
Combustion chamber: annular baffle combustion chamber.
Turbine: 1-stage centripetal.
Nozzle: Simple Converging Nozzle.
Control system: digital electronic control system.
Fuel system: Use RP-3 fuel.
Lubricating oil system: 4010 lubricating oil is used.
Ignition system: motor start or compressed air start, spark plug or electric igniter ignition.
Accessories: starter motor, brushless electric fuel pump.
Technical data
Dimensions
Length: 345mm
Diameter: 158mm
weight
Dry mass: 23kg
Performance
Takeoff thrust: ≥0.42kN
Cruising thrust (H=0, Ma0.3): ≥0.28kN
fuel consumption
Take-off state: 156kg/(kN h)
Life: 20h
- 无人机
- 无人及配件
- 雷达
- 硬件
- 导航
- 监测
- 发动机
产能:
未通知
运输时间表:
根据订单的规模
Incoterms:
未通知包装明细:
未通知
更多关于
Shenzhen Nuobashi Trading Co.,Ltd
10-50
员工
未通知
100%
% 出口销售额
Year
成立年份
业务类型
- Industry / Manufacturer
- Distributor / Wholesaler
关键词
- 半导体
- 汽车诊断仪
- 无人机
- 示波器
- 电子元器件
联系方式和位置
- Weili Liang
- +86 xxxxxxxx
- 深圳 / | 中国