Fly-around-the-World Near-Space Picosatellite for Cost-Effective School Space Projects

Pirada Techavijit, Polkit Sukchalerm, Natthapong Wongphuangfuthaworn, Sureepon Kiyapaet
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Abstract

This research presents the design and development of a near-space picosatellite platform intended to operate at high altitudes between 20–40 km above sea level. These picosatellites function similarly to orbital satellites but float and travel with the wind in the atmosphere instead of orbiting the Earth. The platform utilizes a super-pressure balloon to provide buoyancy, allowing the picosatellite to remain airborne and operational for several days to months, capable of flying around the world multiple times. This study focuses on the cost-effective design of high-altitude platforms, telecommunication systems, and energy consumption for the picosatellite, enabling it to communicate with ground stations from anywhere in the world while consuming low power. The use of common COTS (Commercial Off-The-Shelf) equipment aims to enhance accessibility for educational applications. This research gathered data from our previous studies for over 20 high-altitude platform flights, analyzed the necessary factors for whole system design, and developed a new prototype that has been successfully built and tested.
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用于低成本高效益学校空间项目的环绕地球飞行近地皮卡卫星
这项研究介绍了近空间皮卫星平台的设计和开发情况,该平台旨在海拔 20-40 千米的高空运行。这些皮卫星的功能与轨道卫星类似,但漂浮在大气层中随风飘动,而不是围绕地球运行。该平台利用超压气球提供浮力,使皮卡卫星能够在空中飞行数天至数月,并能够多次环绕地球飞行。这项研究的重点是高空平台、电信系统和皮卫星能耗的成本效益设计,使其能够在低功耗的情况下与世界任何地方的地面站进行通信。使用常见的 COTS(现成商用)设备旨在提高教育应用的可及性。这项研究收集了我们之前 20 多次高空平台飞行的研究数据,分析了整个系统设计的必要因素,并开发了一个新的原型,该原型已成功建造并进行了测试。
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