航天器部件真空检漏试验管理系统的设计

航天器部件真空检漏试验管理系统是航天器件特殊环境试验管理系统的一个重要组成部分。文章根据航天器部件真空检漏试验管理的需求,结合软件设计开发流程规范,对试验技术流程进行了分析,设计出系统总体框架和功能模块:系统总体框架分为数据资源层、业务逻辑层和客户层;功能模块分为试验任务管理模块、个人任务管理模块、试验数据管理模块、试验归档管理模块、试验资源管理模块、基础配置管理模块和系统管理模块。该试验管理系统将使航天器部件真空检漏试验管理工作更加高效、合理。

Design of vacuum leak testing management system for spacecraft component test

The design method of the vacuum leak testing management system for spacecraft components is discussed in this paper. The vacuum leak testing management system for spacecraft components is an essential subsystem of the special environment test management system for spacecraft components. According to the requirements of the vacuum leak testing management system for spacecraft components and the software development process, the test processes are analyzed and the overall structure and various functionality modules are designed. The testing management system is divided into three mutually supporting levels： the user service tier, the business logic tier and the data resources tier. There are seven functional modules in the spacecraft component vacuum leak testing management system, including the test task management, the personal task management, the test data management, the test file management, the test resource management, the configuration management and the system management. This system would be helpful to a more efficient and reasonable management of vacuum leak testing for spacecraft components.