We present the as-manufactured design of the cryostat of the Mid-infrared ELT Imager and Spectrograph (METIS) instrument to be operated at ESO’s Extremely Large Telescope (ELT). The cryostat provides the cold optics of the instrument with the required cryo-vacuum environment. The radiation shields of the cryostat are cooled with liquid nitrogen and the cold optics is cooled via pulse-tube coolers down to temperatures between 35 K and 70 K. The cold-warm interface is provided with G10 blades that build together with the top part of the cryostat vessel the structural interface to the cold optics, the warm support structure, and the warm calibration source. The cryostat design is now finalized with most of the parts already produced and final integration on-going. We present in this paper the final design as manufactured, the key design considerations, and highlights from the integration phase.
We present the final design of the cryostat of the Mid-infrared ELT Imager and Spectrograph (METIS) instrument to be operated at ESO’s Extremely Large Telescope (ELT). The cryostat provides the cold optics of the instrument with the required cryo-vacuum environment. The radiation shields of the cryostat are cooled with liquid nitrogen and the cold optics is cooled via pulse-tube coolers down to temperatures between 35 K and 70K. The cold-warm interface is provided with G10 blades that build together with the top part of the cryostat vessel the structural interface to the cold optics, the warm support structure and the warm calibration source. The cryostat development is now complete and the instrument Final Design Review is scheduled for November 2022. We present in this paper the final design status, the key design considerations and the cooling concept.
We present the current design status of the cryostat of the Mid-infrared ELT Imager and Spectrograph (METIS) instrument to be operated at ESO’s Extremely Large Telescope (ELT). The cryostat provides the cold optics of the instrument with the required cryo-vacuum environment. The radiation shields of the cryostat are cooled with liquid nitrogen and the cold optics is cooled via pulse-tube coolers down to temperatures around 35 K. The cold-warm interface is provided with G10 blades that build together with the top part of the cryostat vessel the structural interface to the cold optics, the warm support structure and the warm calibration source. The cryostat development is currently in its final design phase which is planned to conclude in summer 2022. We present in this paper the current design status, the key design considerations and the cooling concept.
We present the design, capabilities and applications of a cryogenic test facility for astronomical instrumentation located at ETH Zurich, Switzerland. This facility was designed, built, and commissioned with the purpose to support opto-mechanical performance measurements of cryo-mechanisms for astronomical instruments. In particular, the facility was developed initially to test the opto-mechanical stability and repeatability of the wheel-mechanisms for the ERIS/VLT instrument that are developed in house. However, the facility has a generic application portfolio and can be used for other development projects as well. The unique setup allows optical access from the warm end with short working distance to the cold elements of only a few millimeters. Electrical, mechanical, and liquid feedthroughs provide a flexible infrastructure for a large variety of thermal, mechanical, electrical and optical tests. To provide maximum mechanical stability, the cooling is provided by a low vibration pulse tube cooler that cools the facility down to approximately 8 K.
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