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Fabrication of Feedhorn-Coupled Transition Edge Sensor Arrays for Measurement of the Cosmic Microwave Background PolarizationCharacterization of the minute cosmic microwave background (CMB) polarization signature requires multi-frequency high-throughput precision instrument systems. We have previously described the detector fabrication of a 40 gigahertz focal plane and now describe the fabrication of a 37-element dual-polarization detector module for measurement of the CMB at 90 gigahertz. The 72-TES (Transition Edge Sensor)-based bolometers in each module are coupled to a niobium-based planar orthomode transducer with integrated band defining filters implemented in microstrip transmission line. A single crystal silicon dielectric substrate serves as microstrip dielectric and as a thermal link between the membrane isolated MoAu TES operating at 150 millikelvins and the heat bath. A short silicon leg between the heat bath and the TES bolometer is designed for ballistic phonon transport and provides improved process control and uniformity of thermal conductance in the presence of phonon scattering on roughened surfaces. Micro-machined structures are used to realize the orthomode transducer backshort, provide out of band signal rejection, and a silicon photonic choke for feedhorn coupling are described. The backshort, choke wafer, and detector wafer are indium bump-bonded to create a single 37-element dual-polarization detector module. Fourteen such hexagonally shaped modules each 80 millimeters in size comprise two focal planes. These, along with the recently delivered 40 gigahertz focal plane, will survey a large fraction of the sky as part of the Johns Hopkins University-led ground-based CLASS (Cosmology Large Angular Scale Surveyor) telescope.
Document ID
20150019755
Acquisition Source
Goddard Space Flight Center
Document Type
Presentation
Authors
Denis, K. L.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Ali, A.
(Johns Hopkins Univ. Baltimore, MD, United States)
Appel, J.
(Johns Hopkins Univ. Baltimore, MD, United States)
Bennett, C. L.
(Johns Hopkins Univ. Baltimore, MD, United States)
Chang, M. P.
(Stinger Ghaffarian Technologies, Inc. (SGT, Inc.) Greenbelt, MD, United States)
Chuss, D. T.
(Villanova Univ. PA, United States)
Colazo, F. A.
(Adnet Systems, Inc. Greenbelt, MD, United States)
Costen, N.
(Stinger Ghaffarian Technologies, Inc. (SGT, Inc.) Greenbelt, MD, United States)
Essinger-Hileman, T.
(Johns Hopkins Univ. Baltimore, MD, United States)
Hu, R.
(ASRC Aerospace Corp. Greenbelt, MD, United States)
Marriage, T.
(Johns Hopkins Univ. Baltimore, MD, United States)
Rostem, K.
(Johns Hopkins Univ. Baltimore, MD, United States)
U-Yen, K.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Wollack, E. J.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Date Acquired
October 27, 2015
Publication Date
July 20, 2015
Subject Category
Electronics And Electrical Engineering
Instrumentation And Photography
Space Radiation
Report/Patent Number
GSFC-E-DAA-TN24619
Meeting Information
Meeting: International Workshop on Low Temperature Detectors
Location: Grenoble
Country: France
Start Date: July 20, 2015
End Date: July 24, 2015
Sponsors: Universite Grenoble Alpes, Centre National de la Recherche Scientifique, Institut de Radio Astronomie Millimetrique, Commissariat a l'Energie Atomique
Funding Number(s)
CONTRACT_GRANT: NNX14AB76A
CONTRACT_GRANT: NNG12PL17C
CONTRACT_GRANT: NNG13CR48C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Detectors
Characterization
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