Preliminary results of the Single Event Effect testing for the ULTRASAT sensors

Fuente: arXiv
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Autores principales: Berlea, Vlad Dumitru, Asif, Arooj, Barschke, Merlin F., Berge, David, Crespo, Juan Maria Haces, Giavitto, Gianluca, Kumar, Shashank, Porelli, Andrea, de Simone, Nicola, Watson, Jason, Worm, Steven, Zappon, Francesco, Birman, Adi, Alfassi, Shay, Feningstein, Amos, Waxman, Eli, Netzer, Udi, Liran, Tuvia, Lapid, Ofer, Algranatti, Viktor M., Schvartzvald, Yossi
Formato: Preprint
Publicado: 2024
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author Berlea, Vlad Dumitru
Asif, Arooj
Barschke, Merlin F.
Berge, David
Crespo, Juan Maria Haces
Giavitto, Gianluca
Kumar, Shashank
Porelli, Andrea
de Simone, Nicola
Watson, Jason
Worm, Steven
Zappon, Francesco
Birman, Adi
Alfassi, Shay
Feningstein, Amos
Waxman, Eli
Netzer, Udi
Liran, Tuvia
Lapid, Ofer
Algranatti, Viktor M.
Schvartzvald, Yossi
author_facet Berlea, Vlad Dumitru
Asif, Arooj
Barschke, Merlin F.
Berge, David
Crespo, Juan Maria Haces
Giavitto, Gianluca
Kumar, Shashank
Porelli, Andrea
de Simone, Nicola
Watson, Jason
Worm, Steven
Zappon, Francesco
Birman, Adi
Alfassi, Shay
Feningstein, Amos
Waxman, Eli
Netzer, Udi
Liran, Tuvia
Lapid, Ofer
Algranatti, Viktor M.
Schvartzvald, Yossi
contents ULTRASAT (ULtra-violet TRansient Astronomy SATellite) is a wide-angle space telescope that will perform a deep time-resolved all-sky survey in the near-ultraviolet (NUV) spectrum. The science objectives are the detection of counterparts to short-lived transient astronomical events such as gravitational wave sources and supernovae. The mission is led by the Weizmann Institute of Science and is planned for launch in 2026 in collaboration with the Israeli Space Agency and NASA. DESY will provide the UV camera, composed by the detector assembly located in the telescope focal plane and the remote electronics unit. The camera is composed out of four back-metallized CMOS Image Sensors (CIS) manufactured in the 4T, dual gain Tower process. As part of the radiation qualification of the camera, Single Event Effect (SEE) testing has been performed by irradiating the sensor with heavy ions at the RADEF, Jyvaskyla facility. Preliminary results of both Single Event Upset (SEU) and Single Event Latch-up (SEL) occurrence rate in the sensor are presented. Additionally, an in-orbit SEE rate simulation has been performed in order to gain preliminary knowledge about the expected effect of SEE on the mission.
format Preprint
id arxiv_https___arxiv_org_abs_2407_03789
institution arXiv
publishDate 2024
record_format arxiv
spellingShingle Preliminary results of the Single Event Effect testing for the ULTRASAT sensors
Berlea, Vlad Dumitru
Asif, Arooj
Barschke, Merlin F.
Berge, David
Crespo, Juan Maria Haces
Giavitto, Gianluca
Kumar, Shashank
Porelli, Andrea
de Simone, Nicola
Watson, Jason
Worm, Steven
Zappon, Francesco
Birman, Adi
Alfassi, Shay
Feningstein, Amos
Waxman, Eli
Netzer, Udi
Liran, Tuvia
Lapid, Ofer
Algranatti, Viktor M.
Schvartzvald, Yossi
Instrumentation and Methods for Astrophysics
Instrumentation and Detectors
ULTRASAT (ULtra-violet TRansient Astronomy SATellite) is a wide-angle space telescope that will perform a deep time-resolved all-sky survey in the near-ultraviolet (NUV) spectrum. The science objectives are the detection of counterparts to short-lived transient astronomical events such as gravitational wave sources and supernovae. The mission is led by the Weizmann Institute of Science and is planned for launch in 2026 in collaboration with the Israeli Space Agency and NASA. DESY will provide the UV camera, composed by the detector assembly located in the telescope focal plane and the remote electronics unit. The camera is composed out of four back-metallized CMOS Image Sensors (CIS) manufactured in the 4T, dual gain Tower process. As part of the radiation qualification of the camera, Single Event Effect (SEE) testing has been performed by irradiating the sensor with heavy ions at the RADEF, Jyvaskyla facility. Preliminary results of both Single Event Upset (SEU) and Single Event Latch-up (SEL) occurrence rate in the sensor are presented. Additionally, an in-orbit SEE rate simulation has been performed in order to gain preliminary knowledge about the expected effect of SEE on the mission.
title Preliminary results of the Single Event Effect testing for the ULTRASAT sensors
topic Instrumentation and Methods for Astrophysics
Instrumentation and Detectors
url https://arxiv.org/abs/2407.03789