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Lynx x-ray microcalorimeter

Lynx is an x-ray telescope, one of four large satellite mission concepts currently being studied by NASA to be a flagship mission. One of Lynx’s three instruments is an imaging spectrometer called the Lynx x-ray microcalorimeter (LXM), an x-ray microcalorimeter behind an x-ray optic with an angular...

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Detalles Bibliográficos
Autores principales: Bandler, Simon R., Chervenak, James A., Datesman, Aaron M., Devasia, Archana M., DiPirro, Michael, Sakai, Kazuhiro, Smith, Stephen J., Stevenson, Thomas R., Yoon, Wonsik, Bennett, Douglas, Mates, Benjamin, Swetz, Daniel, Ullom, Joel N., Irwin, Kent D., Eckart, Megan E., Figueroa-Feliciano, Enectali, McCammon, Dan, Ryu, Kevin, Olson, Jeffrey, Zeiger, Ben
Formato: Online Artículo Texto
Lenguaje:English
Publicado: 2019
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7802767/
https://www.ncbi.nlm.nih.gov/pubmed/33442556
http://dx.doi.org/10.1117/1.JATIS.5.2.021017
Descripción
Sumario:Lynx is an x-ray telescope, one of four large satellite mission concepts currently being studied by NASA to be a flagship mission. One of Lynx’s three instruments is an imaging spectrometer called the Lynx x-ray microcalorimeter (LXM), an x-ray microcalorimeter behind an x-ray optic with an angular resolution of 0.5 arc sec and ∼2 m(2) of area at 1 keV. The LXM will provide unparalleled diagnostics of distant extended structures and, in particular, will allow the detailed study of the role of cosmic feedback in the evolution of the Universe. We discuss the baseline design of LXM and some parallel approaches for some of the key technologies. The baseline sensor technology uses transition-edge sensors, but we also consider an alternative approach using metallic magnetic calorimeters. We discuss the requirements for the instrument, the pixel layout, and the baseline readout design, which uses microwave superconducting quantum interference devices and high-electron mobility transistor amplifiers and the cryogenic cooling requirements and strategy for meeting these requirements. For each of these technologies, we discuss the current technology readiness level and our strategy for advancing them to be ready for flight. We also describe the current system design, including the block diagram, and our estimate for the mass, power, and data rate of the instrument.