SearcharxivSearch

arXiv · 2502.10866

The X-ray Integral Field Unit at the end of the Athena reformulation phase

Philippe Peille·Didier Barret·Edoardo Cucchetti·Vincent Albouys·Luigi Piro·Aurora Simionescu·Massimo Cappi·Elise Bellouard·Céline Cénac-Morthé·Christophe Daniel·Alice Pradines·Alexis Finoguenov·Richard Kelley·J. Miguel Mas-Hesse·Stéphane Paltani·Gregor Rauw·Agata Rozanska·Jiri Svoboda·Joern Wilms·Marc Audard·Enrico Bozzo·Elisa Costantini·Mauro Dadina·Thomas Dauser·Anne Decourchelle·Jan-Willem den Herder·Andrea Goldwurm·Peter Jonker·Alex Markowitz·Mariano Mendez·Giovanni Miniutti·Silvano Molendi·Fabrizio Nicastro·François Pajot·Etienne Pointecouteau·Gabriel W. Pratt·Joop Schaye·Jacco Vink·Natalie Webb·Simon Bandler·Marco Barbera·Maria Teresa Ceballos·Ivan Charles·Roland den Hartog·W. Bertrand Doriese·Jean-Marc Duval·Flavio Gatti·Brian Jackson·Caroline Kilbourne·Claudio Macculi·Sylvain Martin·Yann Parot·Frederick Porter·Damien Prêle·Laurent Ravera·Stephen Smith·Jan Soucek·Tanguy Thibert·Eija Tuominen·Fabio Acero·Stefano Ettori·Nicolas Grosso·Jelle Kaastra·Pasquale Mazzotta·Jon Miller·Salvatore Sciortino·Sophie Beaumont·Matteo D'Andrea·Jelle de Plaa·Megan Eckart·Luciano Gottardi·Maurice Leutenegger·Simone Lotti·Alexei Molin·Lorenzo Natalucci·Muhammad Qazi Adil·Andrea Argan·Elisabetta Cavazzuti·Mauro Fiorini·Pourya Khosropanah·Eduardo Medinaceli Villegas·Gabriele Minervini·James Perry·Frederic Pinsard·Desi Raulin·Manuela Rigano·Peter Roelfsema·Denis Schwander·Santiago Terron·Guido Torrioli·Joel Ullom·Monika Zuchniak·Laurence Chaoul·Jose Miguel Torrejon·Frank Brachet·Beatriz Cobo·Malcolm Durkin·Valentina Fioretti·Hervé Geoffray·Lionel Jacques

Abstract

The Athena mission entered a redefinition phase in July 2022, driven by the imperative to reduce the mission cost at completion for the European Space Agency below an acceptable target, while maintaining the flagship nature of its science return. This notably called for a complete redesign of the X-ray Integral Field Unit (X-IFU) cryogenic architecture towards a simpler active cooling chain. Passive cooling via successive radiative panels at spacecraft level is now used to provide a 50 K thermal environment to an X-IFU owned cryostat. 4.5 K cooling is achieved via a single remote active cryocooler unit, while a multi-stage Adiabatic Demagnetization Refrigerator ensures heat lift down to the 50 mK required by the detectors. Amidst these changes, the core concept of the readout chain remains robust, employing Transition Edge Sensor microcalorimeters and a SQUID-based Time-Division Multiplexing scheme. Noteworthy is the introduction of a slower pixel. This enables an increase in the multiplexing factor (from 34 to 48) without compromising the instrument energy resolution, hence keeping significant system margins to the new 4 eV resolution requirement. This allows reducing the number of channels by more than a factor two, and thus the resource demands on the system, while keeping a 4' field of view (compared to 5' before). In this article, we will give an overview of this new architecture, before detailing its anticipated performances. Finally, we will present the new X-IFU schedule, with its short term focus on demonstration activities towards a mission adoption in early 2027.

Explore related subjects

Keep this discovery

BibTeXRIS

Philippe Peille, Didier Barret, Edoardo Cucchetti, Vincent Albouys, Luigi Piro, Aurora Simionescu, Massimo Cappi, Elise Bellouard, Céline Cénac-Morthé, Christophe Daniel, Alice Pradines, Alexis Finoguenov, Richard Kelley, J. Miguel Mas-Hesse, Stéphane Paltani, Gregor Rauw, Agata Rozanska, Jiri Svoboda, Joern Wilms, Marc Audard, Enrico Bozzo, Elisa Costantini, Mauro Dadina, Thomas Dauser, Anne Decourchelle, Jan-Willem den Herder, Andrea Goldwurm, Peter Jonker, Alex Markowitz, Mariano Mendez, Giovanni Miniutti, Silvano Molendi, Fabrizio Nicastro, François Pajot, Etienne Pointecouteau, Gabriel W. Pratt, Joop Schaye, Jacco Vink, Natalie Webb, Simon Bandler, Marco Barbera, Maria Teresa Ceballos, Ivan Charles, Roland den Hartog, W. Bertrand Doriese, Jean-Marc Duval, Flavio Gatti, Brian Jackson, Caroline Kilbourne, Claudio Macculi, Sylvain Martin, Yann Parot, Frederick Porter, Damien Prêle, Laurent Ravera, Stephen Smith, Jan Soucek, Tanguy Thibert, Eija Tuominen, Fabio Acero, Stefano Ettori, Nicolas Grosso, Jelle Kaastra, Pasquale Mazzotta, Jon Miller, Salvatore Sciortino, Sophie Beaumont, Matteo D'Andrea, Jelle de Plaa, Megan Eckart, Luciano Gottardi, Maurice Leutenegger, Simone Lotti, Alexei Molin, Lorenzo Natalucci, Muhammad Qazi Adil, Andrea Argan, Elisabetta Cavazzuti, Mauro Fiorini, Pourya Khosropanah, Eduardo Medinaceli Villegas, Gabriele Minervini, James Perry, Frederic Pinsard, Desi Raulin, Manuela Rigano, Peter Roelfsema, Denis Schwander, Santiago Terron, Guido Torrioli, Joel Ullom, Monika Zuchniak, Laurence Chaoul, Jose Miguel Torrejon, Frank Brachet, Beatriz Cobo, Malcolm Durkin, Valentina Fioretti, Hervé Geoffray, Lionel Jacques. 2025-02-15. The X-ray Integral Field Unit at the end of the Athena reformulation phase. https://arxiv.org/abs/2502.10866

Cite the original work for its findings. Save a collection to share your selection of sources.

KEEP EXPLORING

Related papers

The EDD Radio Astronomy Backend Framework

Modern digital radio astronomy receivers produce increasingly wide-bandwidth, high bit-rate data streams that necessitate the development of flexible, scalable, and maintainable backend processing and recording systems. Historically, such backend instrumentation has been tightly coupled to telescope observing modes, limiting reuse between observatories and science cases. We present the Effelsberg Direct Digitisation (EDD) backend framework, a software-defined architecture for constructing real-time radio astronomy backends on commodity off-the-shelf computing infrastructure. We describe its design, implementation, supported observing modes, and operational deployments. EDD separates a common core framework from plugin-provided observing capabilities. The core provides orchestration, telescope interfaces, pipeline lifecycle management, monitoring, and deployment tooling, while plugins implement processing pipelines for specific observing modes. The framework is designed to support both single-dish and interferometric instruments through site-specific configuration and plugin selection. EDD currently supports spectroscopy and spectropolarimetry, pulsar timing and searching, baseband recording, very long baseline interferometry, correlation, and beamforming. Operational deployments include the Effelsberg 100-m telescope, the SKA-MPI prototype dish, the Thai National Radio Telescope, and the ARGOS interferometric prototype array. By separating common services, observing-mode plugins, and site-specific configuration, it allows backend capabilities to be deployed across heterogeneous telescope environments and provides a community resource for broadband radio astronomy instrumentation.

astro-ph.IM

Bayesian Superiority in On/Off analysis

We present a detailed comparison of Bayesian criteria with three non-informative priors - flat, Jeffreys, and scale-invariant - for testing a signal against an unknown background and compare them with the classical frequentist Li-Ma approach in the On/Off problem. We perform Monte Carlo simulations for various background levels and evaluate the Li-Ma and Bayesian criteria by their Type I error rates. We then simulate a nonzero signal and compare the criteria in terms of Type II error rates. We find that the Bayesian criterion with the Jeffreys prior yields lower Type I and Type II error rates than the Li-Ma criterion. In addition, we show that the Bayesian criteria are more robust than the Li-Ma criterion when the background distribution is overdispersed relative to the Poisson distribution.

astro-ph.IM

An RFSoC-based Backend and Timing System for the Balloon-borne Very Long Baseline Interferometry Experiment

We present the design and performance characterization of the digital backend and precision-timing system for the Balloon-borne Very Long Baseline Interferometry Experiment (BVEX), a pathfinder for high-frequency stratospheric VLBI at 22 GHz. The backend uses one of the four 14-bit analog-to-digital converter inputs on an AMD-Xilinx RFSoC 4x2. Although the converters support sampling rates up to 5 GSPS, the flight configuration digitizes the 2-4 GHz intermediate frequency at 4.096 GSPS. CASPER firmware provides both a high-resolution spectrometer for pointing and receiver verification, and a VLBI acquisition chain with two-bit requantization that records at a rate of about 8.2 Gbps. The timestamped data packets are sent over 100 Gigabit Ethernet (GbE) to a 16 TB NVMe array in a storage computer that draws approximately 70-80 W. The timing chain uses a Rakon oven-controlled crystal oscillator as a timing reference while a time-interval counter measures its drift relative to a GPS reference with approximately 60 ps resolution. This is the first deployment of an RFSoC-based VLBI backend and precision-timing system on a stratospheric balloon. Ground tests validated the backend, spectrometer, and timing chain. The August 2025 CSA STRATOS flight ended before reaching the target float altitude because of a balloon failure, and as a result no science observations were obtained. For the planned 2027 reflight, we are developing a conduction-cooled data storage computer with 24 TB of NVMe capacity and a direct data path from the 100 GbE interface to the NVMe array.

astro-ph.IM