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Research on Modal Test Technology of LM-6A Solid-Liquid Strap-On Launch Vehicle
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作者 ZHU Chunyan YANG Bing +2 位作者 DI Wenbin CHANG Dongfang MAO Yuming 《Aerospace China》 2022年第2期25-33,共9页
The LM-6 A new generation solid-liquid strap-on launch vehicle has the structural dynamic characteristics of lower frequencies,denser modes and coupling modes in longitudinal,bending and torsion modal space.During the... The LM-6 A new generation solid-liquid strap-on launch vehicle has the structural dynamic characteristics of lower frequencies,denser modes and coupling modes in longitudinal,bending and torsion modal space.During the development phase of LM-6 A,modal tests of partial stacks and the full vehicle were designed to obtain the structural dynamic properties.The structural dynamic models using the finite element method(FEM)have been verified and calibrated based on the modal test data.This paper describes the pre-test predictions and test execution,and details the comparison between the pre-test predictions and the test data.The successful maiden flight of LM-6 A further confirmed the effectiveness of structural dynamic modeling and modal test for LM-6 A. 展开更多
关键词 LM-6A modal test of full vehicle partial stack modal test
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