Predicting the effect of radiation damage on dark current in a space-qualified high performance CMOS image sensor

The CIS115 is a Teledyne-e2v CMOS image sensor with 1504×2000 pixels of 7 μm pitch. It has a high optical quantum efficiency owing to a multi-layer anti-reflective coating and its backside illuminated construction, and low dark current due to its pinned photodiode 4T pixel architecture. The sensor o...

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Veröffentlicht in:Journal of instrumentation 2019-11, Vol.14 (11), p.C11008-C11008
Hauptverfasser: Crews, C., Soman, M.R., Lofthouse-Smith, D-D., Allanwood, E.A.H., Stefanov, K.D., Leese, M., Turner, P., Holland, A.D.
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container_end_page C11008
container_issue 11
container_start_page C11008
container_title Journal of instrumentation
container_volume 14
creator Crews, C.
Soman, M.R.
Lofthouse-Smith, D-D.
Allanwood, E.A.H.
Stefanov, K.D.
Leese, M.
Turner, P.
Holland, A.D.
description The CIS115 is a Teledyne-e2v CMOS image sensor with 1504×2000 pixels of 7 μm pitch. It has a high optical quantum efficiency owing to a multi-layer anti-reflective coating and its backside illuminated construction, and low dark current due to its pinned photodiode 4T pixel architecture. The sensor operates in rolling shutter mode with a frame rate of up to 7.5 fps (if using the whole array), and has a low readout noise of ∼5 electrons rms. The CIS115 has been selected for use within the JANUS instrument, which is a high resolution camera due to launch on board ESA's JUpiter ICy moons Explorer (JUICE) spacecraft in 2022. After an interplanetary transit time of over 7 years, JUICE will spend 3.5 years touring the Jovian system, studying three of the Galilean moons in particular: Ganymede, Callisto and Europa. During this latter part of the mission, the spacecraft and hence the CIS115 sensor will be subjected to the significant levels of trapped radiation surrounding Jupiter. Gamma and proton irradiation campaigns have therefore been undertaken in order to evaluate both ionising and non-ionising dose effects on the CIS115's dark current performance. Characterisations were carried out at expected mission operating temperatures (−35±10ˆC) both prior to and post-irradiation. Models of the resulting degradation in dark current behaviour will be combined with expected doses during the JUICE mission in order to predict the performance of the CIS115 at the mission end-of-life.
doi_str_mv 10.1088/1748-0221/14/11/C11008
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subjects Antireflection coatings
Callisto
CMOS
Dark current
Europa
Galilean satellites
Ganymede
Icy satellites
Jupiter
Jupiter satellites
Multilayers
Operating temperature
Photodiodes
Pixels
Proton irradiation
Quantum efficiency
Radiation damage
Radiation effects
Sensors
Spacecraft
Transit time
title Predicting the effect of radiation damage on dark current in a space-qualified high performance CMOS image sensor
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