CARMEN2/MEX: An in-flight laboratory for the observation of radiation effects on electronic devices

Bezerra, F.; Ecoffet, R.; Lorfèvre, E.; Samaras, A.; Deneau, C.

doi:10.1109/radecs.2011.6131430

Cited by 17 publications

(6 citation statements)

References 11 publications

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“…It was launched on June 10, 2011. One of the payloads is the ICARE-NG [10] instrument which was built in the frame of the CARMEN-1 ("CARactérisation et Modélisation de l'ENvironnement") suite (composed of ICARE-NG and SODAD instruments which have been funded by CNES). The ICARE-NG instrument on-board SAC-D began its operation in August 30, 2011 and stopped in June 7 th 2015.…”

Section: A Total Displacement Damage Dose (Ddd) At 660 Km Altitudementioning

confidence: 99%

Benchmarking ionizing space environment models

Bourdarie

Inguimbert

Standarovski

et al. 2017

IEEE Trans. Nucl. Sci.

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In flight feedback data are collected such as displacement damage doses, ionizing doses and cumulated SEUs on board various space vehicles and are compared to predictions performed with (1) proton measurements performed with spectrometers data on board the same spacecraft if any and (2) protons spectrum predicted by the legacy AP8min model and the AP9 and OPAL models. When an accurate representation of the 3D spacecraft shielding as well as appropriate ground calibrations are considered in the calculations such comparisons provide powerful metrics to investigate engineering model accuracy. To describe > 30 MeV trapped protons fluxes, AP8 min model is found to provide closer predictions to observations than AP9 V1.30.001 (Mean and Perturbed mean).

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Section: A Total Displacement Damage Dose (Ddd) At 660 Km Altitudementioning

confidence: 99%

Benchmarking ionizing space environment models

Bourdarie

Inguimbert

Standarovski

et al. 2017

IEEE Trans. Nucl. Sci.

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“…[4] Because of an important number of SEL observed during ion test, SEU data are not workable. [6] In addition, no proton ground tests were performed and no more components are available.…”

Section: ) Hitachi Hm628512c Ground Testmentioning

confidence: 99%

CARMEN-2: In flight observation of non destructive single event phenomena on memories

Samaras

Bezerra

Lorfèvre

et al. 2011

2011 12th European Conference on Radiation and Its Effects on Components and Systems

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This paper presents non destructive SEE data collected in flight on commercial SRAMs, SSRAMs and SDRAMs by MEX module. Detected events are SEU, MCU, SEFI as well as weakened cell. MEX (Module Experience) is a part of CARMEN2 instrument, launched the 22th of June 2008 aboard JASON2 satellite (1335km, 66°). This scientific instrument is dedicated to the study of space radiation effects on electronic devices.

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“…All components are placed inside the ICARE-NG/CARMEN-2 equipment aboard JASON-2 (more precisely on the MEX board), a dedicated instrument to study space radiation and its effects on electronic components developed by EREMS [9]- [10]. Components were intentionally chosen for their high sensitivity to different types of SEE [3]- [4]. Here, we present detailed SEU rate results for the Samsung K7A801800 SSRAM and the IDT IDT71V3558 SSRAM and SEL rate results for the Hitachi HM628512 SRAM.…”

Section: A Component Datamentioning

confidence: 99%

“…Then, the OMERE software combined the sector analysis file together with component radiation test data and the mission's radiation environment to estimate Single Event Rates (SER). These rates are compared to inflight measured rates[3]-[4] during the period between June 2008 and August 2011.…”

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confidence: 99%

Shielding geometry effect on SEE prediction using the new OMERE release: JASON-2 mission case study

Varotsou¹,

Chatry²,

Peyrard³

et al. 2011

2011 12th European Conference on Radiation and Its Effects on Components and Systems

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The 2011 release of the OMERE freeware includes a module that allows to consider the shielding effect of the satellite geometry in the calculation of Single Event Effects (SEE) on electronic devices. This module has been applied to calculations performed for proton induced SEE aboard the JASON-2 satellite. Calculated prediction rates agree with those observed in-flight. The shielding effect has also been studied by "placing" the satellite in a geosynchronous orbit radiation environment, for both "out-of-flare" and "in-flare" configurations. In the "in-flare" case, the shielding geometry of the satellite has a great impact on the calculated rate.Index Terms-Application software, in-flight data, low earth orbit satellites, radiation effects, single event effects.

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CARMEN2/MEX: An in-flight laboratory for the observation of radiation effects on electronic devices

Cited by 17 publications

References 11 publications

Benchmarking ionizing space environment models

Benchmarking ionizing space environment models

CARMEN-2: In flight observation of non destructive single event phenomena on memories

Shielding geometry effect on SEE prediction using the new OMERE release: JASON-2 mission case study

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