CAJ | 학술논문

随着航天技术的发展，模块化航天器的设计应用已经成为研究热点，快速、有效运载不同功能模块进入太空将成为亟待解决的问题。设计了搭载适配器结构，利用火箭发射卫星时的剩余空间，实现模块的快速搭载发射。分析了搭载适配器的应用模式，利用 Pro/E 软件设计了搭载适配器的机械结构，并利用 ANSYS 软件对结构进行了有限元分析。
수착항천기술적발전，모괴화항천기적설계응용이경성위연구열점，쾌속、유효운재불동공능모괴진입태공장성위극대해결적문제。설계료탑재괄배기결구，이용화전발사위성시적잉여공간，실현모괴적쾌속탑재발사。분석료탑재괄배기적응용모식，이용 Pro/E 연건설계료탑재괄배기적궤계결구，병이용 ANSYS 연건대결구진행료유한원분석。
With the development of space technology,modular spacecraft design and its applica-tion has become one of the research hotspots.And how to launch different functional module into space quickly and effectively will become an urgent problem to be solved.Aiming at this problem, with the structure design of an equipped adapter,which can use the surplus space of the rocket effec-tively when launching a satellite,and realize the rapid launch of the module.This paper analyses the application mode of equipped adapter,using Pro/E software to design the mechanical structure of equipped adapter,then finite element analysis was carried out by using ANSYS software.