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1、火箭发动机包覆质量自动检测系统控制系统设计摘要：固体火箭发动机包覆质量是指固体火箭发动机装入推进剂之后，壳体、 绝热层、衬层、推进剂之间的胶接质量。为保证绝热层和衬层在发动机点火时正 常发挥作用，在设计、制造过程中，必须保证各界面的可靠粘接。本文首先在绪论部分介绍了本课题的研究意义、国内外背景，研究内容。然 后在分两章讲述了硬件部分和软件部分的设计过程。本文的主要内容有：1. 硬件设计部分讲述了 AT89C52单片机的功能，各功能模块的设计过程， 控制原理图的绘制。2. 软件设计部分讲述的是部分模块的程序设计。关键词 固体火箭发动机，超声检测，单片机，控制系统Rocket Engine Gab
2、le Quality Automatic Detection SystemsControl System DesignABSTRACT : Solid propellant engine inhibitor quality examination question including two parts: Solid propellant engine inhibitor thickness examination and solid propellant engine inhibitor contact surface cementation condition examination. A
3、fter the solid propellant engine cementation quality is refers the solid propellant engine loads the propellant, between shell, thermal insulation blanket, lining, and propellant glued joint quality.This article first introduced this topic research significance, the domestic and foreign backgrounds
4、in the introduction part, the research content. Then narrated the hardware part and the software part design process in the weight chapter.The article main content includes: 1. hardware designs partially narrated the AT89C52 monolithic integrated circuit function, various functions module design pro
5、cess, control scheme plan. 2. Software designs partial narrations is the partial modules programming.The article primary coverage includes:1. The hardware design part narrated at89C52 monolithic integrated circuit function, various functions module design process, control scheme plan.2. The software design part narration is the partial module programming.Keyword Solid Propellant Engine, Ultrasonic Checks , Single Chip Microcomputer , Control System
