引信试验用模拟火箭弹

Simulated Test Rocket for Fuze

为了解决火箭弹试验成本高的问题,并加快研制进度和改善试验观测条件,研制了模拟试验火箭弹。以小型专用火箭弹模拟火箭弹的弹道参数,用来考核引信。该弹可以相当满意地模拟火箭弹的加速度、推进时间、主动段末速、转速等主要参数,非常适合火箭弹触发引信研制中的靶场射击试验和生产交验,具有对试验场地要求低、试验简便、安全性高、成本低、有利于缩短引信研制周期等优点。

In order to reduce expense of roket experiment, speed up the research progress and improve the observing condition during experiment, the simulated rocket was developed. P, alistic parameters of rocket are simulated for examining the fuze. This simulated rocket can simulate the acceleration, thrust time, speed at burning end, rotation speed and so on satisfily. It is not only suitable for firing test during development, but also delivery test. This simmulated rocket does not require ideal experiment environment, is easy to be implemented. It is characterized by high security, low cost, shortening the fuze researching period and other benifits.