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Focus mechanism for EXOMARS mission: Lessons learned from preliminary design to space flight model delivery

机译:ExoMars Mission的重点机制:从初步设计到太空飞行模型交付的经验教训

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The CLUPI (CLose-UP Imager) instrument is a high-resolution camera mounted onto the Drill of the ExoMars 2020 rover mission carried out by the European Space Agency (ESA) and Roscosmos. The CLUPI development is under the responsibility of Thales Alenia Space Switzerland whereas the Principal Investigator is Dr. Jean-Luc Josset from the Space Exploration Institute. In the frame of the development CLUPI instrument, the CSEM developed and delivered three models of a flexure-based Focus Mechanism. The CLUPI Focus Mechanism (CFM) design utilizes flexure guides to allow very accurate frictionless adjustment of the focal distance of the imager. Such design must also comply with very stringent requirement from the ExoMars mission, especially regarding the low Martian temperatures and the launch/landing load environment. This article presents the three main challenges encountered during the development of the mechanism and how these were addressed: resilience, performance and reliability. This article then draws the lessons learnt from this development including potential design improvements for a similar design and general rules to applicable to any development involving compliant mechanism.
机译:Clupi(特写成像器)仪器是安装在欧洲航天局(ESA)和Roscosmos的exoMars 2020 Rover任务的钻头上的高分辨率摄像头。 Clupi开发是艾丽尼亚空间瑞士的责任,而主要调查员是来自太空勘探学院的Jean-Luc Josset博士。在开发CLUPI仪器的框架中,CSEM开发并交付了三种基于柔性的焦点机制的模型。 Clupi焦点机制(CFM)设计利用挠性指南来允许非常准确的成像器的焦距调整成像仪的焦距。这种设计还必须符合exoMars使命的非常严格的要求,特别是关于低火星温度和发射/着陆负荷环境。本文介绍了在制定机制和这些问题期间遇到的三项主要挑战以及如何解决:恢复力,性能和可靠性。然后,本文从该开发中吸取的经验教训,包括类似设计和一般规则的潜在设计改进,以适用于涉及兼容机制的任何发展。

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