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Optics for the imaging x-ray polarimetry explorer
Author(s) -
Brian D. Ramsey
Publication year - 2017
Publication title -
nasa sti repository (national aeronautics and space administration)
Language(s) - English
Resource type - Conference proceedings
DOI - 10.1117/12.2275502
Subject(s) - polarimetry , optics , detector , aerospace , physics , fabrication , field of view , satellite , aerospace engineering , polarization (electrochemistry) , remote sensing , astronomy , engineering , scattering , geology , medicine , chemistry , alternative medicine , pathology
The Imaging X-ray Polarimetry Explorer (IXPE) was recently selected by NASA for flight in late 2020. IXPE features three identical x-ray telescopes each comprised of a 4-m-focal length mirror module assembly, fabricated at MSFC, that focuses x-rays onto a polarization-sensitive, imaging detector, contributed by Italy. Mirrors and detectors are separated by a deployable boom that sits atop a Ball-Aerospace-provided satellite bus. This presentation will give a brief overview of the IXPE mission with particular emphasis on the mirror module assembly design, fabrication approach, and expected performance. Trades performed to optimize the design within mass and launch-vehicle fairing constraints will be discussed, along with finite element analyses run to optimize the mechanical design. The presentation will also touch on modeling of leakage radiation from off-axis sources outside of the field of view.

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