运载火箭子系统嵌入式环境应力记录仪

Maria George, R. Sethunadh, H. Saleem, S. Athula Devi
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引用次数: 0

摘要

本文介绍了一种用于运载火箭分系统的小型、高效环境应力记录仪的设计与实现。该系统可以监测和记录运载火箭各子系统在实现、储存和运输过程中所经历的温度、湿度、振动和冲击等各种环境应力,并带有时间标签。该系统坚固耐用,足以承受极端环境条件。该系统有内置传感器来感知各种参数,处理电子来分析和从大带宽信号中提取有用的信息,并有存储器来存储数据。该产品重量轻,功耗低,易于安装。系统的数据很容易检索,并且已经开发了一个分析软件,它将在笔记本电脑或个人电脑上运行,并将系统在实现和评估阶段所经历的压力作为输入。通过对产品进行各种环境试验,对其进行了成功的评价。产品评估表明,数据和分析可用于确保子系统不发生意外应力或处理问题,从而有助于在运载火箭系统实现的各个层面上保证质量。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Embedded Environmental Stress Recorder for Launch Vehicle Subsystems
The design and implementation details of a compact and efficient environmental stress recorder for launch vehicle sub systems are presented here. The proposed system can monitor and record various environmental stresses like temperature, humidity, vibration and shock experienced by launch vehicle subsystems during their realization, storage and transportation phases with a time tag. The system is rugged enough to withstand extreme environmental conditions. The system has built-in sensors to sense various parameters, processing electronics to analyze and extract useful information from large bandwidth signals and memory to store the data. The product has low weight, low power consumption and is easily mountable. The data from the system is easily retrievable and an analysis software has been developed which will run in a laptop or PC and takes as input the stresses that the system has undergone during the realization and evaluation phases. The product was evaluated successfully by subjecting it to various environmental tests. The product evaluation showed that the data and the analysis can be used to ensure that no unintentional stresses or handling issues have happened for the subsystems thereby aiding quality assurance at each level of launch vehicle system realization.
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