함대공 유도탄 방어 유도무기의 점화안전장치 조립체 성능시험 방법 개선 연구

Abstract

In this study, the performance test method of the ignition safety device assembly of a surface-to-air anti-missile was improved. The testing items of the ignition stabilizer assembly performance test measure maximum pressure and total combustion time, and use a pressure sensor for measurement. The ignition safety device assembly is a product that performs a critical function of igniting the propulsion engine when launching a guided missile, and it is important to secure normal performance. In fact, after measuring the maximum pressure and total combustion time using a pressure sensor during the performance test, a quantitative standard is required for each data value analysis and a pressure sensor that can minimize errors should be used. Therefore, this study presents a method to quantify and analyze the maximum pressure and total combustion time measurement data for the ignition safety device assembly performance test, and verify the optimal type of pressure sensor to exclude measurement errors.