The Ba-2 is the low-altitude, low-speed radioplane target drone developed by Northwest Polytechnic University (NPU) in the 1960s for the antiaircraft gunnery and radar crews to conduct target practice. Development began in 1966 and the drone made its first flight in 1968. The batch production began in 1970, with over a thousand examples delivered to the PLA since then.
Ba-2型低空、低速无线电靶机，在1960年由西北理工大学（NPU）发展用于防空射击和雷达组员去实施打靶练习。发展从1966年开始，而且无人机在1968年作了它的首次飞行。批量制造从1970年开始，此后超过一千架被交付给PLA。
The Ba-2 is a lightweight, versatile, and easy-to-use target drone. The fuselage and wings are made of mainly fibreglass, with some wooden and steel parts. The drone is driven by an air-cooled 2-stroke 14hp piston engine fuelled by ordinary motor vehicle gasoline. The wings and tails of the drone can be easily dissembled for transportation. The drone carries two target sleeves inside its cabin and can be fitted with light tracers and strobe lights for night training. The drone could also simulate the manoeuvres of fighters and attackers to make the target practice more realistic.
Ba-2型是一种轻型、多用途和易用靶机。机身和机翼主要用玻璃纤维制作，还有一些木制和钢制部件。无人机由一台风冷、二冲程14马力普通摩托车汽油发动机驱动。无人机的机翼和尾部能容易地为运输被拆卸。无人机在它的内舱携带二条瞄准飘带并能配备曳光弹和闪光灯用于夜间训练。无人机也可以模拟战斗机和攻击机的动作使打靶变得更真实。
Specifications
Dimensions: Wingspan: 2.7m; Length: 2.55m; Height 0.76m
Weight: Max take-off 53kg; Max load 5kg; Fuel 6kg
Speed: Max 250km/h
Service ceiling: 2,000m
Flight endurance: 1 hour
Remote control range: 15km
Powerplant: One HS-280 air-cooled, 4-cylinder, 2-stroke piston engine rated at 10.3kW (14hp)
Launch: Fixed ground launcher with a rocket booster
Recovery: Parachute
规格
尺寸： 翼展：2.7 米；机长：2.55 米；机高：0.76 米
重量： 最大起飞 53 公斤；最大负荷 5 公斤；燃料 6 公斤
速度： 最高 250 公里/小时
升限： 2,000 米
续飞： 1 小时
遥控范围： 15 公里
动力装置： 一台 HS-280型风冷、4-缸、额定10.3 千瓦的2 冲程活塞发动机（14 马力）
起飞： 采用火箭助推固定地面发射架
回收： 降落伞
Last update: 7 July 2008
最后更新： 2008年7月7日
