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전개형 경량 위성 안테나 반사판의 재료분석 및 형상 최적화
곽도혁(Do Hyuk Kwak),정화영(Hwa Young Jung),이재은(Jae Eun Lee),강광희(Kwang Hee Kang) 한국생산제조학회 2017 한국생산제조학회지 Vol.26 No.2
In this paper, we reviewed major design parameters for a solid type of deployable antenna and its structural design. We performed modal analysis for a single reflector panel made of aluminum and CFRP (carbon fiber reinforced plastic) to confirm the appropriateness of selected materials. We then predicted the elastic modulus of CFRP using the principles of unidirectional composite elasticity stiffness predictions such as the ROM (Rule of Mixture) and HSR (Hart Smith 10% Rule). To optimize the shape of the antenna reflector, a structural stiffness analysis was performed using derived numerical optimization factors. Six structural stiffness analyses were performed using the constructed experimental design method. The resulting optimal shape conditions are proposed to meet the structural stiffness requirements while minimizing weight.