Light transmittance measurement method of solid rocket motor plume based on laser modulation spectrum analysis

固体燃料火箭 透射率 推进剂 材料科学 光学 羽流 激光器 火箭(武器) 信号(编程语言) 光电子学 航空航天工程 物理 工程类 气象学 计算机科学 程序设计语言
作者
Bin Yang,M. Ye,Kejie Qiang,Jinxin Tao,Si-Hua Chen,Jiahui Chen,Zhixin Wang
出处
期刊:Propellants, Explosives, Pyrotechnics [Wiley]
卷期号:49 (3)
标识
DOI:10.1002/prep.202300224
摘要

Abstract The light transmittance measurement method, which is used to characterize smoke characteristic signal of solid rocket motor plume, can provide important reference for development and design of low smoke characteristic signal solid propellants and motors. The light transmittance measurement method of solid rocket motor plume based on laser modulation spectrum analysis is proposed in this paper. By using a 405 nm laser as the light source and a narrow‐band filter detection method, the influence of plume radiation on the measurement of light transmittance of solid rocket motor plume smoke can be minimized. Additionally, combined with the laser modulation spectrum analysis technology, the signal amplitude is selected by the laser modulation frequency to improve the signal‐to‐noise ratio of the signal. Compared with the laser constant current measuring mode, laser high‐frequency modulation measuring mode with spectrum analysis effectively improves the optical transmittance measurement accuracy. Based on this, a solid rocket motor plume smoke transmittance test system is developed to measure the plume smoke of standard test motors with different propellants and combustion chamber pressures. The results demonstrate that the system can effectively measure the light transmittance of the plume smoke. The light transmittance of solid rocket motor plume can be increased by reducing the aluminum content of solid propellant or increasing the pressure of the combustion chamber. Thus, this research provides an effective measuring tool for evaluating smoke concentration of solid rocket motor plume, which is beneficial to develop low smoke characteristic signal solid propellants and motors.

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