% IMPORTANT: The following is UTF-8 encoded. This means that in the presence
% of non-ASCII characters, it will not work with BibTeX 0.99 or older.
% Instead, you should use an up-to-date BibTeX implementation like “bibtex8” or
% “biber”.
@INPROCEEDINGS{Berlea:611550,
author = {Berlea, Vlad Dumitru and Asif, Arooj and Barschke, Merlin
and Berge, David and Crespo, Juan Maria Haces and Giavitto,
Gianluca and Kumar, Shashank and Porelli, Andrea and De
Simone, Nicola and Watson, Jason John and Steve, Worm and
Zappon, Francesco and Birman, Adi and Alfassi, Shay and
Fenigstein, Amos and Waxmann, Eli and Netzer, Udi and Liran,
Tuvia and Lapid, Ofer and Algranatti, Vikto M. and
Schvartzvald, Yossi},
title = {{P}reliminary results of the {S}ingle {E}vent {E}ffect
testing for the {ULTRASAT} sensors},
journal = {Nuclear instruments $\&$ methods in physics research /
Section A},
volume = {1068},
issn = {0168-9002},
address = {[Amsterdam]},
publisher = {Elsevier},
reportid = {PUBDB-2024-04968, arXiv:2407.03789},
pages = {169754},
year = {2024},
abstract = {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.},
month = {May},
date = {2024-05-26},
organization = {PM2024 - 16th Pisa Meeting on Advanced
Detectors, Isola de Elba (Italy), 26
May 2024 - 1 Jun 2024},
cin = {$Z_DET$},
ddc = {530},
cid = {$I:(DE-H253)Z_DET-20201126$},
pnm = {622 - Detector Technologies and Systems (POF4-622) /
RADNEXT - RADiation facility Network for the EXploration of
effects for indusTry and research (101008126)},
pid = {G:(DE-HGF)POF4-622 / G:(EU-Grant)101008126},
experiment = {EXP:(DE-H253)ULTRASAT-20211201},
typ = {PUB:(DE-HGF)16 / PUB:(DE-HGF)8},
eprint = {2407.03789},
howpublished = {arXiv:2407.03789},
archivePrefix = {arXiv},
SLACcitation = {$\%\%CITATION$ = $arXiv:2407.03789;\%\%$},
UT = {WOS:001301406000001},
doi = {10.1016/j.nima.2024.169754},
url = {https://bib-pubdb1.desy.de/record/611550},
}