CAJ | 학술논문

该文中的卫星采用新型框架面板式构型，该构型卫星与运载采用新型四点连接的方式，而不是传统的包带连接方式。对该文中的卫星进行模态分析及试验，采用不同的安装基础进行多次模态试验，找出其中的差异，并进行相关比对分析。根据分析及试验获得框架面板式卫星的模态特性，判读卫星的模态特性是否满足运载要求，同时根据试验结果完善相关航天试验规范。
해문중적위성채용신형광가면판식구형，해구형위성여운재채용신형사점련접적방식，이불시전통적포대련접방식。대해문중적위성진행모태분석급시험，채용불동적안장기출진행다차모태시험，조출기중적차이，병진행상관비대분석。근거분석급시험획득광가면판식위성적모태특성，판독위성적모태특성시부만족운재요구，동시근거시험결과완선상관항천시험규범。
Different from the traditional clamp band of connecting mode, the satelite in this study adopts a new mode of configuration to connect the rocket with four joint points. With different instalation supporting structures, the study carries out several mode experiments on the new configuration to find differences and make comparative analyses. Based on the results of experiments, it aims to determine whether the mode parameters meet the needs of rockets and to improve the relative research criterions in the aerospace field.