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EXOMARS RAMAN LASER SPECTROMETER SCIENTIFIC PERFORMANCES CHECK WITH A BREADBOARD

机译:EXOMARS拉曼激光光谱仪通过面包板检查科学性能

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The Raman Laser Spectrometer (RLS) is one of the Pasteur Payload instruments, within the ESA's Aurora Exploration Programme, ExoMars mission. It will perform Raman spectroscopy on crushed powered samples deposited on a small container after crushing the cores obtained by the Rover's drill system. For being able to check that the Instrument fulfils main scientific requirements, a breadboard which verifies the TRL5 (Technology Readiness Level 5) achievement by the Instrument, has been developed. With results obtained from that model campaign, it has been demonstrated that the Instrument satisfies scientific functionality in a relevant environment. The Instrument breadboard has kept all optical critical parameters, interfaces between units, and relevant functionalities. The RLS is composed by the following units: SPU (Spectrometer Unit): a spectrometer concept based on a single transmission holographic grating, used as dispersion element; and with a thermally controlled CCD detection. iOH: (Internal Optical Head): an optical unit which focus (autofocus mechanism capability) the laser excitation light over the sample through the excitation path, and filters the scattered Raman signal for its processing at the SPU through the reception path. ICEU (Instrument Control and Excitation Unit): within this unit it is housed the high stability laser source, the Front End Electronics; and the power and processor modules. A breadboard unit was developed and tested for each of the previous subsystems; and finally integrated and tested at Instrument level (designed as modular as possible in order to be able to upgrade the breadboard in a step by step process), for checking main scientific requirements for significant samples identification. The Instrument breadboard programme has been developed for two years, and has been able to achieve the following objectives: verify RLS critical scientific performances: spectral resolution, spectral accuracy, SNR... validate the System Radiometric Model validate RLS critical functionalities, such as: CCD control and commanding, iOH autofocus... confirm the overall concept of the Instrument operation: spectra extraction, operation timing, operation algorithms... After RLS breadboard campaign, Instrument scientific critical performances have been verified, allowing go on with future Instrument models. And also, with the radiometric model validation it will be easy to predict how future possible Instrument design modifications could affect to Instrument final performances.
机译:拉曼激光光谱仪(RLS)是巴斯德有效载荷仪器之一,属于ESA ExoMars任务的欧罗Aurora勘探计划。在粉碎流动站钻探系统获得的岩心后,它将对沉积在一个小容器上的粉碎的动力样品进行拉曼光谱分析。为了能够检查仪器是否满足主要的科学要求,开发了一种面包板,用于验证仪器达到TRL5(技术就绪级别5)的要求。从该模拟活动中获得的结果表明,该仪器满足了相关环境中的科学功能。仪器面包板保留了所有光学关键参数,单元之间的接口以及相关功能。 RLS由以下单元组成:SPU(光谱仪单元):基于单个透射全息光栅的光谱仪概念,用作色散元素;并具有热控CCD检测功能。 iOH :(内部光学头):一种光学单元,它通过激发路径将激光激发光聚焦(自动聚焦机制功能)到样品上,并通过接收路径对散射的拉曼信号进行滤波以在SPU上进行处理。 ICEU(仪器控制和激励单元):在该单元内装有高稳定性激光源,即前端电子设备;以及电源和处理器模块。为每个先前的子系统开发并测试了一个面包板单元;最终在仪器级别进行集成和测试(设计为尽可能模块化,以便能够逐步升级面包板),以检查对重要样品鉴定的主要科学要求。仪器面包板计划已经开发了两年,并且能够实现以下目标:验证RLS关键的科学性能:光谱分辨率,光谱准确性,SNR ...验证系统辐射度模型验证RLS关键功能,例如: CCD控制和命令,iOH自动对焦...确认仪器操作的总体概念:光谱提取,操作时序,操作算法...在RLS面包板运动之后,仪器科学的关键性能得到了验证,可以继续使用将来的仪器模型。而且,通过辐射度模型验证,可以很容易地预测将来可能进行的仪器设计修改将如何影响仪器的最终性能。

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