Study on the Multi-Component Test Technology of Solid Rocket Motors

• 作者: ZHU Ziwen QU Youyang HAN Chenglin
• 来源期刊: 中国航天（英文版）
• 年，卷（期）: 2021,（4）
• 所属期刊栏目: RESEARCH
• 页码范围: 42-47
• 页数: 6页
• 语种: 英文
• DOI: 10.3969/j.issn.1671-0940.2021.04.006

摘要

This paper presents a calculation method,and composition of a five-component force test device,to resolve the requirement for solid rocket motor multi-component force test.It compares the difference between two classical algorithms,and summarizes the structure and practical usage of the solid rocket motor multi-component force using soft connection structure measurement.The decoupling method of test data is described,and a reasonable re-search method for solid rocket motor multi-component force is also given in this paper.