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Fine Optimization of TES Design for the X-IFU Instrument on ATHENAThe X-ray Integral Field Unit (X-IFU) instrument on the Advanced Telescope for High ENergy Astrophysics (ATHENA) is baselined to have 3168 transition-edge sensor (TES) microcalorimeter pixels. These pixels will be DC biased and readout using time division multiplexing. We recently reported a demonstration of the required pixel and readout performance in 252 pixels from a 1 kilo-pixel array (e.g. 2.16 eV resolution for 6.9 keV X-rays). Having achieved the required performance, the 50um square TES design in this demonstration array is considered the baseline pixel design for X-IFU. However, by making small adjustments to the TES design, we may be able to make small but consequential improvements to the instrument performance, while staying within the many constraints of the X-IFU requirements.

In this presentation, we will show results from newly fabricated devices with subtle changes from the baseline TES design to further optimize the performance for X-IFU. We will discuss optimizing the TES sheet resistance, normal metal features, X-ray absorber attachment points, TES aspect ratio, and heat capacity. These minor design changes can have significant effects on thermo-electric time constants, thermal fluctuation noise, resistive transition shape and uniformity, and non-linearity of X-ray event pulses. In addition, full characterization of these new TES designs allows greater understanding of the relevant physics within the TES and gives routes for further optimization.
Document ID
20210019001
Acquisition Source
Goddard Space Flight Center
Document Type
Presentation
Authors
Nick Wakeham
(University of Maryland, Baltimore County Baltimore, Maryland, United States)
J. S. Adams
(University of Maryland, Baltimore County Baltimore, Maryland, United States)
S. R. Bandler
(Goddard Space Flight Center Greenbelt, Maryland, United States)
S. Beaumont
(University of Maryland, Baltimore County Baltimore, Maryland, United States)
J. A. Chervenak
(Goddard Space Flight Center Greenbelt, Maryland, United States)
F. M. Finkbeiner
(Sigma Space (United States) Lanham, Maryland, United States)
J. Y. Ha
(SCIENTIFIC & BIOMEDICAL MICROSYSTEMS )
R. Hummatov
(University of Maryland, Baltimore County Baltimore, Maryland, United States)
R. L. Kelley
(Goddard Space Flight Center Greenbelt, Maryland, United States)
C. A. Kilbourne
(Goddard Space Flight Center Greenbelt, Maryland, United States)
A. M. Miniussi
(University of Maryland, Baltimore County Baltimore, Maryland, United States)
F. S. Porter
(Goddard Space Flight Center Greenbelt, Maryland, United States)
K. Sakai
(University of Maryland, Baltimore County Baltimore, Maryland, United States)
S. J. Smith
(Goddard Space Flight Center Greenbelt, Maryland, United States)
E. J. Wassell
(Science Systems and Applications (United States) Lanham, Maryland, United States)
S. Yoon
(Scientific & Biomedical Microsystem Glen Burnie, Maryland)
Date Acquired
July 22, 2021
Subject Category
Spacecraft Instrumentation and Astrionics
Meeting Information
Meeting: 19th International Workshop on Low Temperature Detectors
Location: Online
Country: US
Start Date: July 19, 2021
End Date: July 29, 2021
Sponsors: National Institute of Standards and Technology
Funding Number(s)
CONTRACT_GRANT: 80GSFC21M0002
CONTRACT_GRANT: 80GSFC17C0003
CONTRACT_GRANT: 80GSFC18C0120
WBS: 244904
CONTRACT_GRANT: 80NSSC21F0911
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Peer Committee
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