TY - GEN
T1 - The design of a UV CMOS sensor for the ULTRASAT space telescope
AU - Liran, Tuvia
AU - Shvartzvald, Yossi
AU - Lapid, Ofer
AU - Ben-Ami, Sagi
AU - Waxman, Eli
AU - Netzer, Ehud
AU - Ofek, Eran
AU - Gal-Yam, Avishay
AU - Zappon, Francesco
AU - Barschke, Merlin F.
AU - Worm, Steven
AU - Vasilev, Mikhail
AU - Bühler, Rolf
AU - Berge, David
AU - Koifman, Vladimir
AU - Miller, Avi
AU - Mordakhay, Anatoli
AU - Lehana, Gadi
AU - Lempel, Yosef
AU - Levi, Andrei
AU - Ben-David, Oshrit
AU - Galambos, Tiberiu
AU - Birman, Adi
AU - Fenigstein, Amos
AU - Alfassi, Shay
AU - Katz, Omer
AU - Reshef, Raz
N1 - Publisher Copyright: © 2022 SPIE. All rights reserved.
PY - 2022
Y1 - 2022
N2 - ULTRASAT is a scientific satellite carrying a near UV telescope with high sensitivity and large field of view. The mission, led by the Weizmann Institute of Science and the Israeli Space Agency in collaboration with Deutsches Elektronen-Synchrotron (DESY), is expected to be launched in 2025 by NASA. ULTRASAT will revolutionize our understanding of the high energy transient universe and will have a broad scientific impact across the fields of gravitational wave (GW) sources, supernovae, variable and flare stars, active galactic nuclei, tidal disruption events, compact objects, and galaxies. The ULTRASAT camera, developed by DESY, is based on a custom imager, developed by Analog Value and Tower Semiconductors, and manufactured by Tower Semiconductor in Israel. The focal plane array is composed of four independent sensors with an effective area of ~45 x 45 mm2 each, providing graceful degradation capabilities. Each sensor array has ~22,450M pixels, with pixel size of 9.5 x 9.5 μm2. The sensor implements backside illumination and an anti-reflective coating optimized for the wavelength range 230 to 290nm, achieving high quantum efficiency of >60%. Low dark noise of <0.026 e/sec/pixel is needed to meet the required sensitivity. This is achieved by both operating at - 73oC, and by a special design including advanced pixel architecture, optical trench between the array of pixels and surrounding circuits and a low noise design of the digital electronics. High dynamic range (HDR) capability is achieved by dual gain 5T pixels. The design of the sensor includes one analog to digital converter (ADC) per column architecture and low voltage differential signal (LVDS) output buffers. The operation is controlled by a dedicated microcontroller and configuration registers. The design employs techniques for mitigating space radiation effects, enabling an operation lifetime of 6 years in GEO.
AB - ULTRASAT is a scientific satellite carrying a near UV telescope with high sensitivity and large field of view. The mission, led by the Weizmann Institute of Science and the Israeli Space Agency in collaboration with Deutsches Elektronen-Synchrotron (DESY), is expected to be launched in 2025 by NASA. ULTRASAT will revolutionize our understanding of the high energy transient universe and will have a broad scientific impact across the fields of gravitational wave (GW) sources, supernovae, variable and flare stars, active galactic nuclei, tidal disruption events, compact objects, and galaxies. The ULTRASAT camera, developed by DESY, is based on a custom imager, developed by Analog Value and Tower Semiconductors, and manufactured by Tower Semiconductor in Israel. The focal plane array is composed of four independent sensors with an effective area of ~45 x 45 mm2 each, providing graceful degradation capabilities. Each sensor array has ~22,450M pixels, with pixel size of 9.5 x 9.5 μm2. The sensor implements backside illumination and an anti-reflective coating optimized for the wavelength range 230 to 290nm, achieving high quantum efficiency of >60%. Low dark noise of <0.026 e/sec/pixel is needed to meet the required sensitivity. This is achieved by both operating at - 73oC, and by a special design including advanced pixel architecture, optical trench between the array of pixels and surrounding circuits and a low noise design of the digital electronics. High dynamic range (HDR) capability is achieved by dual gain 5T pixels. The design of the sensor includes one analog to digital converter (ADC) per column architecture and low voltage differential signal (LVDS) output buffers. The operation is controlled by a dedicated microcontroller and configuration registers. The design employs techniques for mitigating space radiation effects, enabling an operation lifetime of 6 years in GEO.
UR - http://www.scopus.com/inward/record.url?scp=85140469739&partnerID=8YFLogxK
U2 - 10.1117/12.2629867
DO - 10.1117/12.2629867
M3 - منشور من مؤتمر
T3 - Proceedings of SPIE - The International Society for Optical Engineering
BT - Space Telescopes and Instrumentation 2022
A2 - den Herder, Jan-Willem A.
A2 - Nikzad, Shouleh
A2 - Nakazawa, Kazuhiro
PB - SPIE
T2 - Space Telescopes and Instrumentation 2022: Ultraviolet to Gamma Ray
Y2 - 17 July 2022 through 22 July 2022
ER -