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A prototype for the primary mirror of the ESA ARIEL mission:design and development of an off-axis 1-m diameter aluminum mirror for infrared space applications

机译:ESA ARIEL任务的主镜原型:设计和开发用于红外太空应用的离轴1米直径铝镜

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In this paper the design, analysis and development of an aluminum 1-m diameter prototype mirror for the telescope of the ARIEL (Atmospheric Remote-sensing Infrared Exoplanet Large-survey) mission are described. ARIEL has been selected by the European Space Agency (ESA) as the next medium-class science mission (M4) to be launched in 2028. The aim of the ARIEL mission is to study the atmospheres of a selected sample of exoplanets. The payload is based on a 1-m class telescope ahead of a suite of instruments: two spectrometric channels covering the band 1.95 to 7.80 μm without gaps, three photometric channels working in the range 0.5 to 1.2 μm, and a low-resolution spectrometer in the range 1.25 to 1.95 μm. The telescope layout is conceived as an eccentric pupil two-mirror classic Cassegrain configuration coupled to a tertiary off-axis paraboloidal mirror. The telescope will be realized on-ground, i.e. subjected to gravity and at room temperature, but it shall operate in space, at 0 g, and at a temperature of about 50 K. For this reason, the telescope expected "as-built" in-flight performance has to be determined via a detailed thermo-elastic analysis. A trade-off on the material to be used for manufacturing the 1-m diameter primary mirror (M1) was carried out, and aluminum alloys have been selected as the baseline materials for both the telescope mirrors and structure. The use of metals, like aluminum alloys, is nowadays frequently considered for the fabrication of space telescopes observing in the infrared wavelength range. Small-size aluminum parts have been proved to be popular both for IR mirrors and structural components, but the manufacturing and stability of large metallic optics still have to be demonstrated. The production of a large aluminum mirror such as that of ARIEL is a challenge, and to prove its feasibility a dedicated study and development program has been started. A prototype, with the same size of the M1 flight model but a simpler surface profile, has been realized and tested.
机译:在本文中,描述了用于ARIEL(大气遥感红外系外行星大飞行)任务的望远镜的铝制1米直径原型镜的设计,分析和开发。欧洲航天局(ESA)已将ARIEL选为下一个将于2028年发射的中型科学任务(M4)。ARIEL任务的目的是研究所选系外行星样品的大气。有效载荷基于一套仪器之前的1-m级望远镜:两个覆盖1.95至7.80μm波段的光谱通道(无间隙),三个工作在0.5至1.2μm范围内的光度通道以及一个低分辨率光谱仪。范围为1.25至1.95μm。望远镜的布局被认为是偏心的瞳孔两面镜经典的卡塞格林配置,再加上三轴离轴抛物面镜。该望远镜将在地面上实现,即受到重力作用并处于室温下,但它应在0 g且温度约为50 K的空间中运行。因此,该望远镜应“按原样建造”飞行中的性能必须通过详细的热弹性分析来确定。对用于制造直径为1 m的主镜(M1)的材料进行了权衡,并且已选择铝合金作为望远镜镜和结构的基线材料。如今,人们经常考虑使用金属(如铝合金)来制造在红外波长范围内观测的太空望远镜。事实证明,小型铝制零件已广泛用于红外反射镜和结构部件,但仍需证明大型金属光学器件的制造和稳定性。像ARIEL这样的大铝镜的生产是一个挑战,为了证明其可行性,已经开始了专门的研究和开发计划。已经实现并测试了原型,该原型具有与M1飞行模型相同的尺寸,但具有更简单的表面轮廓。

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