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本文叙述了小型科学卫星从方案设计到发射以及飞行后分析的许多设计原则和方法。它包括下列内容:卫星外形的确定、结构部件和附件的设计载荷、设计技术和材料使用、自旋稳定卫星的动态稳定准则、卫星的力学试验及组装、各类卫星及其功用、飞行星的管理和运输、发射现场的工作和发射后的分析等。文中的一些计算范例可以帮助结构设计人员设计和试验附件、转动惯量试验装置、哟-哟消旋系统、动载荷计算和断面系数的确定等等,本文还推荐了一些卫星管理及运输方面的知识.
This article describes many design principles and methods for small scientific satellites from project design to launch and post-flight analysis. It includes the following: satellite shape determination, design loads of structural components and accessories, design techniques and material usage, dynamic stability criteria for spin-stabilized satellites, mechanical testing and assembly of satellites, various types of satellites and their functions, flying stars Management and transport, launch site operations and post-launch analysis. Some computational examples in this paper can help structural designers to design and test attachments, moment of inertia test equipment, yo-yo raceway systems, dynamic load calculations, and the determination of cross-section coefficients. Some recommended satellite management and transportation .