E.T.PACK离轨系统的部署机制:功能和鉴定测试

IF 3.1 2区 物理与天体物理 Q1 ENGINEERING, AEROSPACE Acta Astronautica Pub Date : 2024-11-12 DOI:10.1016/j.actaastro.2024.11.008
A. Brunello , G. Anese , S. Chiodini , G. Colombatti , G. Polato , S. Salmistraro , A. Valmorbida , E.C. Lorenzini
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引用次数: 0

摘要

地平线2020 (H2020)未来新兴技术(FET)开放项目E.T.PACK致力于通过开发用于报废卫星脱轨的专用脱轨设备原型来推进电动系绳(EDT)技术。在与E.T.PACK联盟的合作中,帕多瓦大学进行了旨在评估部署机制设计的测试活动。本文概述了这些测试,特别强调了在特定磁带长度上进行的磁带轴检查和部署测试的结果。此外,本文描述了即将到来的端到端部署测试的设置,强调了磁带收集机的集成,以最大限度地减少人工干预。三线圈阀芯成功通过了热真空条件下的资格测试,没有出现冷焊的情况。此外,激振器测试验证了阀芯在不需要额外密封法兰的情况下承受发射条件的能力。此外,该部署机制证明了其在所需速度范围内平滑部署具有不同特性的磁带的熟练程度。此外,按照特定的配置文件,部署过程顺利进行,没有任何并发症。在整个部署过程中保持了一致的连续性,没有出现堵塞或中断的情况。这些测试结果代表了部署机制工程资格模型准备和测试的基本步骤,为后续的端到端部署测试将顺利进行注入信心。为此,将实施一个特定的倒置配置,并设计和制造一台回收机,以方便磁带收集,确保简化和有效的测试过程。本文还提供了端到端部署测试设置的描述,包括回收机。
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The Deployment Mechanism of the E.T.PACK Deorbit System: Functional and Qualification tests
The Horizon 2020 (H2020) Future Emerging Technologies (FET) OPEN Project E.T.PACK is dedicated to advancing Electrodynamic Tether (EDT) technology by developing a specialized Deorbit Device prototype for end-of-life satellite deorbiting. In collaboration with the E.T.PACK consortium, the University of Padova conducted test campaigns aimed at evaluating the Deployment Mechanism design. This paper offers an overview of these tests, with a specific emphasis on the outcomes derived from tape spool examinations and deployment tests conducted on specific tape lengths. Furthermore, the paper delineates the setup for upcoming end-to-end deployment tests, highlighting the integration of a tape collecting machine to minimize manual intervention. The three-coil spool successfully passed qualification tests under thermal-vacuum conditions, exhibiting no instances of cold-welding. Additionally, shaker tests validated the spool ability to withstand launch conditions without requiring additional containment flanges. Furthermore, the Deployment Mechanism demonstrated its proficiency in smoothly deploying tapes with varying characteristics within the desired velocity range. Moreover, the deployment process, following a specific profile, proceeded seamlessly without any complications. Consistent continuity was maintained throughout the deployment processes, with no instances of jams or disruptions observed. These testing outcomes represent a fundamental step in the preparation and testing of the Engineering Qualification Model of the Deployment Mechanism, instilling confidence that subsequent end-to-end deployment tests will progress smoothly. To this end, a specific upside-down configuration will be implemented, and a recollecting machine was designed and manufactured to facilitate tape gathering, ensuring a streamlined and efficient testing process. A description of the end-to-end deployment test setup, including the recollecting machine, is also provided in this paper.
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来源期刊
Acta Astronautica
Acta Astronautica 工程技术-工程:宇航
CiteScore
7.20
自引率
22.90%
发文量
599
审稿时长
53 days
期刊介绍: Acta Astronautica is sponsored by the International Academy of Astronautics. Content is based on original contributions in all fields of basic, engineering, life and social space sciences and of space technology related to: The peaceful scientific exploration of space, Its exploitation for human welfare and progress, Conception, design, development and operation of space-borne and Earth-based systems, In addition to regular issues, the journal publishes selected proceedings of the annual International Astronautical Congress (IAC), transactions of the IAA and special issues on topics of current interest, such as microgravity, space station technology, geostationary orbits, and space economics. Other subject areas include satellite technology, space transportation and communications, space energy, power and propulsion, astrodynamics, extraterrestrial intelligence and Earth observations.
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