CAJ | 학술논문

为实现固体火箭轻质化设计，采用传统机械结构优化的方法能力十分有限。多功能结构优化设计方法，由于采用机、电、热一体化的系统工程级设计思路，为提升火箭整体性能开辟了一个全新的方向。介绍多功能结构设计方法及思路，结合一种新型箭载记录设备原型样机的研制，对多功能结构在固体火箭领域应用的前景进行深入探讨。
위실현고체화전경질화설계，채용전통궤계결구우화적방법능력십분유한。다공능결구우화설계방법，유우채용궤、전、열일체화적계통공정급설계사로，위제승화전정체성능개벽료일개전신적방향。개소다공능결구설계방법급사로，결합일충신형전재기록설비원형양궤적연제，대다공능결구재고체화전영역응용적전경진행심입탐토。
It was very limited to realize light-weight design for solid rocket adopting traditional mechanical structure optimization method. Due to the design philosophy of mechanical, electrical, thermal integration, multi-functional structure design broke a new path for solid rocket performance promotion. The method and thought of multi-functional structure design were introduced systematically. Combining with the development of a new onboard recording equipment prototype, the application prospect of multi-functional structure was discussed deeply on solid rocket area.