ESEO电力系统

A. Tambini, F. Antonini, A. De Luca, J. Szabó, H. Carbonnier, A. Bánfalvi, L. Csurgai-Horváth, Z. Váradi
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引用次数: 0

摘要

ESEO(欧洲学生地球轨道飞行器)航天器是一个微型卫星平台,于2018年12月3日发射,搭载在美国加利福尼亚州范登堡空军基地的专用拼车任务SSO-A (SmallSat Express)上。ESEO是欧空局学院实践空间计划的一部分,旨在为欧洲各地的大学生提供独特的机会,获得在真实空间项目的设计、开发、发射和运营方面的重要实践经验。主工业承包商SITAEL开发了卫星平台,执行了整个航天器的装配集成和测试,包括学生建造的有效载荷和子系统的集成,并在欧空局的协调下为学生团队提供技术支持。ESEO任务对相关行业具有特殊价值,因为它在轨道上验证了SITAEL S-50平台(包括有效载荷为50公斤),这是SITAEL产品组合中最小的平台,代表了设计、开发和制造创新多用途小型卫星平台的密集工作的关键里程碑。电力系统(PS)的设计利用了与布达佩斯技术与经济大学(BME)和欧空局(ESA)卓有成效的合作,前者负责配电单元(PDU),后者作为项目协调员提供专家。PS的设计指导方针是在所有平台模式下实现可靠性最大化和单故障容忍度,同时始终考虑降低总体成本。此外,这个微平台的体积和尺寸的减小对设计师来说是一个额外的挑战。由于在许多欧空局任务中采用了经过验证的空间解决方案,并选择了具有空间遗产的工业或军事级组件,因此实现了这些目标。在简要概述ESEO任务之后,重点将转移到PS架构描述、冗余策略和设计方法上。
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ESEO Power System
The ESEO (European Student Earth Orbiter) spacecraft is a microsatellite platform launched on 3rd of December 2018, on board the Spaceflight's SSO-A (SmallSat Express), the dedicated rideshare mission from the Vandenberg Air Force Base in California (US). ESEO is part of ESA Academy's hands-on space programme designed to provide university students across Europe with the unique opportunity to gain significant practical experience in the design, development, launch and operations of a real space project. The Prime Industrial contractor, SITAEL, developed the satellite platform, performed the assembly integration and testing of the whole spacecraft, including the integration of the student-built payload and subsystems, and provided technical support to the student teams under ESA's coordination. The ESEO mission has a special value for the industry involved, since it validates in-orbit the SITAEL S-50 platform (50 kg including the payload), the smallest within the SITAEL products portfolio, representing a crucial milestone of the intensive work in designing, developing and manufacturing innovative multipurpose small satellites platforms. The Power System (PS) design has taken the advantage of a fruitful collaboration with the Budapest University of Technology and Economics (BME), who was in charge of the Power Distribution Unit (PDU), and with ESA as program coordinator who made available its experts. The PS design guidelines have been the reliability maximization in all platform modes and the single failure tolerance, with the overall cost reduction always in mind. Further, the reduced volume and size of this micro-platform represented an additional challenge to designers. The achievement of these objectives has been obtained thanks to the union of proven space solutions, adopted in many ESA missions, and the selection of industrial or military grade components with space heritage. After a brief overview of the ESEO mission, the focus will be moved to the PS architecture description, redundancies strategy and design approaches.
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