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ELEONORA, A 3U CUBESAT FOR THE CANADIAN SATELLITE DESIGN CHALLENGE

机译:Eleonora,Alaadian卫星设计挑战的3U CubeSat

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We present the Eleonora mission. Eleonora is a 3U CubeSat designed by PolyOrbite, a joint team from Polytechnique Montréal (Quebec, Canada) and the University of Bologna (Italy) to compete in the 2012-2014 iteration of the educational programme known as the Canadian Satellite Design Challenge (CSDC). The satellite was designed to carry two payloads: a camera and a deorbiting system based on an aerodynamic drag sail. The main mission of Eleonora is to use its camera to take photos of the Canadian Arctic for the Geocryolab (Laboratory of Geotechnics and Geomorphology of Cold Regions) of the University of Montréal. The secondary mission of Eleonora is to perform a deorbiting manoeuvre using its deployable drag sail. In the context of the CSDC, an inter-university competition, the Eleonora mission was developed over a 20 months timeline. The two teams worked in their respective country but had regular meetings, via teleconference or in person, to review the project. During this period, the two teams first ideated the mission,then designed, produced, integrated, and tested the 3U CubeSat. The CSDC required Eleonora to undergo an informal preliminary design review, a critical design review, and a vibration test of the final design. At the end of the 2012-2014 CSDC, Eleonora obtained the third overall place among teams coming from ten of the major Canadian universities. A considerable success for the young student society PolyOrbite, created at Polytechnique Montréal in 2012 with the specific goal to recruit students who were passionate about space and willing to embark in the CSDC experience. The paper describes the entire experience of creating a CubeSat mission with a team of graduate and undergraduate students coming from different countries: from the design of the satellite, to the results of the environmental tests performed at the David Florida Laboratory of the Canadian Space Agency, passing through the organizational issues and the lessons learned, with a view to the future of the programme.
机译:我们提出了爱莲的使命。爱莲是一个3U的CubeSat旨在通过PolyOrbite,一个联合小组从蒙特利尔理工学院(魁北克,加拿大)和博洛尼亚大学(意大利)在2012 - 2014迭代被称为加拿大的卫星设计挑战赛教育计划的竞争(CSDC) 。该卫星的设计携带两个有效载荷:摄像头和基于空气阻力帆一个脱轨系统。爱莲的主要任务是利用其相机拍摄蒙特利尔大学的加拿大北极地区的Geocryolab(岩土工程和寒冷地区的地貌实验室)的照片。爱莲的次级任务是利用其可部署拖动帆执行脱轨机动。在CSDC,大学间竞争的背景下,爱莲的使命是开发过20个月时间表。两队曾在各自的国家,但有定期举行会议,通过电话或亲自审查项目。在此期间,两队第一ideated任务,然后设计,生产,集成,并测试了3U的CubeSat。该CSDC需要爱莲接受非正式的初步设计审查,一个关键设计评审,并最终设计的振动试验。在2012 - 2014年中海发展的结束,爱莲获得小组从主要的加拿大大学十来间的探花位置。有相当成功的年轻的学生社团PolyOrbite,于2012年在蒙特利尔理工学院创建与特定目标招募谁是关于空间,并愿意在中海发展经验,走上充满激情的学生。本文介绍如何创建一个团队研究生和本科生来自不同国家的一个立方体卫星任务的整个体验:从卫星的设计,在加拿大航天局的戴维·佛罗里达实验室进行环境测试的结果,通过组织问题和取得的经验教训,以期对项目的未来。

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