本文將針對微微衛星之結構次系統，進行完整之設計與分析。由微微衛星之概念性介紹、任務需求、次系統定義及各個元件之功能需求為前導，在瞭解衛星各部功能後，進而設計衛星內部之配置、空間運用、固定方式、組裝方法及天線展開機構等，且必須能承受微微衛星在發射過程中所經歷的加速度與振動。最後設計出結構主體各個元件之實際尺寸。
　　文中將使用電腦軟體進行微微衛星PACE結構主體之設計與分析。首先運用軟體將設計想法以CAD軟體CATIA建出實體模型，進行組裝方式模擬，再以MSC Patran 及MSC Nastran 進行有限元素分析，在各種條件限制下，設計出能夠符合需求之微微衛星結構主體。

　　This research will aim at the preliminary design and analysis on a satellite structures. We introduce the concept of the satellite, subsystem definition, duty demand, and functions of each part. After understanding the functions of each part, we consider about interior space, components fixed way, assembly, antenna deployment mechanism and so on. The structures that can endure the acceleration and vibration during the launch process would be designed. Then, we’ll decide an actual size of each part in the satellite.
　　In this study, we use the computer software for design and analyze main structures of the Pico-satellite－PACE. CATIA is the CAD software that makes each part of structures from an ideal model to a visualize model. It provides assembly function by simulation. Then the model would be analyzed by the Finite Element Method to compute the stress and model shape by MSC Patran and MSC Nastran. Finally, we design the main structures of satellite to satisfy any kind of constrain conditions.

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