ESA & CNES Final Presentations : Space Environments and Radiation Effects on EEE components

6 Mar 2017, 08:40 → 9 Mar 2017, 14:10 Europe/Amsterdam

Newton2 (ESA/ESTEC)

The ESA-CNES Radiation Final Presentation Days, organised by ESA's Space Environments and Effects (TEC-EPS) section and Component Space Evaluation and Radiation Effects (TEC-QEC) section, will take place from 6th to 9th March, 2017 at ESTEC in the Newton2 conference room.

 

The event will for the first time combine presentations on Space Environments and Radiation Effects on EEE components covering ESA and CNES recent results from R&D activities

• The first two days will be dedicated to Space Environments activities on radiation monitors development and space environment modelling, analysis and simulation tools.
• The second two days will address subjects such as EEE Component irradiation characterization and radiation harness assurance tools and guidelines.

 

==============================================

Instructions for webex connection:

A webex audio and slides streaming will begin each day 5 minutes before the session starts. 

Title: FPD2017
Every day, from Monday, March 6, 2017, to Thursday, March 9, 2017
9:00 pm  |  Europe Time (Amsterdam, GMT+01:00)  |  10 hrs
Meeting number (access code): 844 441 325

When it's time, join the meeting.   

Join by phone
Global call-in numbers

==============================================

Monday 6 March

Webex streaming: will be available for the whole conference

Space Environments and Effects

1 Introduction & Executive summary

Speaker: Dr Veronique Ferlet-Cavrois (ESA)

Slides 2017-03-06_and_07_SE&E_FPdays__Intro_v1.pdf

2 ESABASE2: Overview, Maintenance and Distribution Summary and Recent Developments

Speaker: Dr Karl Dietrich Bunte (etamax space GmbH)

Slides 26-028-123pre_01_00_ESABASE2_Extension_FP.pdf 26-028-123pre_01_00_ESABASE2_Extension_FP.pptx (Protected)

11:10 Coffee break

3 Space debris from spacecraft degradation products

Speaker: Dr Paulo Gordo (FCUL)

Slides 2017-03_FP_Space_Debris_from_Spacecraft_Degradation_Products_-_Final_presentation_rev_3.pdf introdution Slides to "Space Debris from Spacecraft Degradation Products" project

4 Multi-Needle Langmuir Probe (M-NLP) development

Speaker: Tore André Bekkeng (EIDEL)

Slides m-NLP_-_Development_Status_-_Bekkeng.pptx

5 In-flight data from POLAR

Speaker: Dr Hualin Xiao (PSI)

Slides 2017POLAR_ESATEC.pdf

13:00 Lunch

Space Environments and Effects: TEC-EPS

6 Dust electrostatic charging, transport and contamination model for Lunar Lander and human exploration missions

Speaker: Mr Benjamin RUARD (Artenum)

Slides ESA-SPIS-DUST-ccn-fpdays-2017-03_BJR007.pdf

7 Numerical simulations of Solar Orbiter at its perihelion: spacecraft charging, effects on RPW and SWA-EAS instruments

Speaker: Dr Stanislas Guillemant (LESIA)

Slides SGUILLEMANT_Solar_Orbiter_v4.pdf

8 ODI databases maintenance

Upgrade of Open Data Interface (ODI) D. Heynderickx, DH Consultancy, Leuven, Belgium P. Wintoft, Solar Analytics, SE H. Evans, ESA/ESTEC, Noordwijk, The Netherlands ODI is a MySQL database framework developed for streamlined ingestion and storage of time series of spacecraft and ground based data. The latest upgrades of the framework consist of: - functionality for ingesting netCDF data files - support of SPASE metadata - development of a Python native client interface - development of reporting, plotting and status tools - enhancements of the REST interface - upgrade of the Excel client connection - support for new datasets (e.g. DSCOVR)

Speaker: Dr Daniel Heynderickx (DH Consultancy BVBA)

Slides ODI database maintenance

15:30 Coffee break

9 PAMELA Data Exploitation

Speaker: Dr Alessandro Bruno (Università degli Studi di Bari, Italy)

Slides A.Bruno_ESA_final_presentation.pdf

10 Two new ESA projects for radiation belt modelling

New ESA Projects of Radiation Belt Modelling D. Heynderickx, DH Consultancy, Leuven, Belgium F. Lei, RadMod Research, Camberley, UK I. Sandberg, IASA & SPARC, Athens, Greece I. Daglis, IASA, Athens, Greece M. Cyamukungu, CSR/UCL, Belgium E. de Donder, BIRA-IASB, Belgium P. Truscott, Kallisto Consultancy, Farnborough, UK H. Evans, P. Jiggens, D. Rodgers, ESA/ESTEC, Noordwijk, The Netherlands Two contracts on radiation belt modelling have been initiated by ESA recently: VALIRENE is a two year project (ESA Contract No 4000117974/16/NL/LF) to: 1) perform a detailed evaluation of the IRENE models against in situ datasets and other radiation environment models (including ECSS); 2) consolidate and (cross-) calibrate in situ datasets; 3) perform a detailed evaluation and comparison of the UNILIB and IRBEM libraries; 4) develop a toolkit to facilitate model validation activities. European space industry will be briefed and consulted throughout the activity. RENELLA - Radiation Environment at Extremely Low Latitude and Altitude (ESA Contract No 4000118058/16/NL/LF/hh): 1) XIPE environment specification validation; 2) dataset selection, acquisition and cross calibration; 3) development of algorithms of flux spectra propagation to lower altitudes; 4) development of a Low Altitude Radiation Belt (LARB) Model. Both projects started very recently. As such, no results are available yet, and the current presentation aims at announcing the activity to the radiation belt community and to foster collaboration.

Speaker: Dr Daniel Heynderickx (DH Consultancy BVBA)

Slides VAL_&_REN_FPD_2017.pptx

Tuesday 7 March

Space Environments and Effects: ESA (TEC-EPS)

11 SSA programme update

Speaker: Mr Juha-Pekka Luntama (ESA)

Slides SSA_SWE_Period_3.pdf

12 SSA Space Weather Elements Radiation Expert Service Centre overview and coordination with TEC Space Environments and Effects activities

Speaker: Dr Alexi Glover (ESA)

Slides SWE_Space_Radiation_Expert_Service_Centre_P3.pdf

13 Non-Ionsing Energy Loss (NIEL) calculation software and verification

Speaker: Dr Pier Giorgio Rancoita (INFN sez. di Milano Bicocca)

Slides PGR_Slides_ESA_7_3_2017.pdf PGR_Slides_ESA_7_3_2017.pptx

14 High LET radiation effects on DNA in water

Speaker: Dr Christian Schwarz (ESA)

Slides KPB_ESA_CNES_2017_I_CS.pdf

10:50 Coffee break

15 Recent vulnerability and hardening studies of optical systems, fibers and fiber sensors at high radiation doses

Speaker: Sylvain Girard

Transparents ESA-PresentationDays-2017-Girard(invited).pdf

Space Environments and Effects: CNES

16 CNES Introduction

Speakers: Mrs Françoise BEZERRA (CNES), Mr Robert ECOFFET (CNES)

Slides FP_Days_CNES_Introductionl_-_Ecoffet_-_07032017.pdf

17 Results from the ICARE-NG detectors onboard SAC-D, JASON 2 and JASON 3 satellites

15 years ago, CNES and ONERA developed a low mass and low power solid state detector named ICARE-NG. This monitor has been flying on the SAC-D and JASON 2 satellites and is currently monitoring the Earth radiation belts onboard JASON-3 spacecraft. We review here the benefits of such a detector (much simpler than a scientific one) providing multi-spacecraft measurements in Low Earth Orbit. In particular, these monitors are a rare opportunity to observe both long term variations in LEO and gradients between orbits.

Speaker: Dr Vincent Maget (ONERA)

Slides ONERA_MAGET_ICAREdata.pdf

18 Highly energetic electrons in the inner zone

The existence of high energy (E>1MeV) electrons in the inner zone is always a debate issue. We tried with several clues to solve the problem they arise. First, using NOAA measurements and in particular a proton channel contaminated by E>1.2MeV electrons, the slot filling was studied over solar cycles. Then the found profiles were compared to the CRRES and SAMPEX measurements. Finally, using a simplistic physical model derived from Salammbô, the variations were estimated to understand the long term behavior of the electrons in the inner belt.

Speaker: Dr Vincent Maget (ONERA)

Slides ONERA_MAGET_EnergeticElectrons.pdf

13:10 Lunch

19 Impact of the consideration of the LEO trapped proton anisotropy on dose calculation at component level

Trapped proton fluxes are anisotropic at Low Earth Orbits (LEO). However, this characteristic is not taken into account in the radiation environment specification of space missions. The goal of the study was to show if such a consideration has an impact on the radiation analysis results. The proton anisotropy was considered and doses were calculated at component level taking into account the orientation and full geometry of the satellite.

Speaker: Dr Athina Varotsou (TRAD)

Slides Impact_of_the_consideration_of_the_LEO_trapped_proton_anisotropy_Varotsou_07032017_1-14.pdf

20 A New Proton Model for Low Altitude High Energy Specification (OPAL)

A model of high energy protons for low altitude (below 800 km) mission specification has been developed at ONERA. This model is based on the long duration NOAA measurement series. We used only the highest omnidirectional channel from SEM on board the old NOAA satellites, and the corresponding channel from SEM-2 on board the new NOAA ones, as the other channels are contaminated by electrons. This gives us a basis for the model for >82 MeV protons. This model was extended in energy by using ICARE-NG measurements on board JASON-2 and HEPAD measurements on board NOAA-6. It gives integrated proton flux in the range 80-600 MeV at altitudes lower than 800 km along the solar cycle.

Speaker: Mrs Angélica SICARD-PIET (ONERA)

Slides Sicard_OPAL.pdf

21 A new Global Radiation Earth Environement (GREEN) model

The well known AP8 and AE8 NASA models are commonly used in the industry to specify the radiation belt environment. Unfortunately, there are some limitations in the use of these models, first due to the covered energy range, but also because in some regions of space, there are discrepancies between the predicted average values and the measurements. Therefore, a new model has been developped at ONERA, GREEN (Global Radiation Earth ENvironement) covering a large region of space and energy, from LEO altitudes to GEO and above, and from plasma to relativistic particles and depending of the year of the solar cycle. The aim for the first version of this new model is to correct the AP8 and AE8 models where they are deficient or not defined, by using local models as IGE-2006, Slot model, OZONE, OPAL,...

Speaker: Mrs Angélica SICARD-PIET (ONERA)

Slides Sicard_GREEN.pdf

15:15 Coffee Break

22 Impact of the consideration of AE9/AP9 models on the space radiation environment specification

AE9/AP9 radiation belt models were developed to substitute the commonly used AE8/AP8 models for trapped particles. This study explored the impact of the integration of these new models into environment specifications. Multiple mission types were considered such as LEO, MEO and electrical orbital rising trajectories. Dose and displacement damage calculations were performed using FASTRAD® and applying both Ray Tracing and Reverse Monte Carlo methods on actual satellite radiation models.

Speaker: Dr Athina Varotsou (TRAD)

Slides Impact_of_the_consideration_of_AE9_AP9_models_Varotsou_07032017.pdf

23 Benchmarking Ionising Space Environment models

In flight feedback data are collected such as displacement damage doses, ionizing doses, cumulated SEUs, and DSNU on Star Tracker 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).

Speaker: Dr Sebastien Bourdarie (ONERA)

Slides Benchmark_FPdaysMarch2017.pdf

24 Data assimilation technique applied to electron Earth radiation belts

An Ensemble Kalman filter combined with the Salammbô 3D tool has been used to produce a re-analysis data base of the electron radiation belt from September 2012 to end of 2015. RBSP-A&B/MagEis data, GOES-13/MagEd and GOES-13/SEM data were ingested by the system. So far only omni-directional fluxes have been considered in this study. The time resolution of the re-analysis data base is 10 minutes and covers electron energies above 300 keV. The results obtained are compared/validated against INTEGRAL/SREM data. Performance of the data assimilation tool will be discussed as well as ways of improvement for the future.

Speaker: Dr Sebastien Bourdarie (ONERA)

Slides FPdays_Assimilation_SBourdarie.pdf

25 Impact of the mission definition parameters on the space radiation environment specification

For the definition of the space radiation environment, missions are usually defined with a standard number of orbits and number of points per orbit. It has been shown that the modification of these parameters can induce differences on the results. The purpose of this study was to determine the impact of the definition of the mission parameters on the fluxes of particles but also on the calculated dose and displacement damage. Six representative orbits were selected but also six cases of electrical orbital rising trajectories were studied. The results allow to make recommendations for each mission type.

Speaker: Dr Athina Varotsou (TRAD)

Slides Impact_of_the_mission_definition_parameters_Varotsou_07032017.pdf

26 OMERE space radiation environment and effects tool: new developments and new interface

OMERE is a freely distributed tool allowing to perform radiation environment and effects calculations (TID, TNID, SEE) for space missions. OMERE is developed by the engineering department of TRAD with the support from the CNES and it is used by engineers from the private and public sector all over world. The new developments and new interface of the latest OMERE version will be presented.

Speaker: Dr Athina Varotsou (TRAD)

Slides OMERE_space_radiation_environment_and_effects_tool_Varotsou_07032017.pdf

Wednesday 8 March

Radiation Effects on EEE components: CNES

27 Impact of the detector definition on the Reverse Monte Carlo calculation result

Different types of detectors are used for the TID calculation based on the RMC method: points and volumes. The impact of their location, their dimensions and their shape has been studied taking into account different geometric models with an increasing complexity. The impact depends on the particle environment and on whether the detector is located inside or at the surface of the spacecraft.

Speaker: Mr Pierre Pourrouquet (TRAD)

Slides Impact_of_detector_definition_on_RMC_calculation.pdf

28 Comparison of TNID calculation methods

Different types of shielding geometry are considered as input for a TNID sector analysis calculation: sphere and slab. TNID calculations using the Reverse Monte Carlo method have also been performed. Analysis of the results allows to make recommendations on the choice of the calculation method based on the complexity of the radiation model.

Speaker: Mr Pierre Pourrouquet (TRAD)

Slides Comparison_of_TNID_calculation_methods_(1).pdf

29 Introduction to "CNES Radiation Effects on EEE components" Session

Speaker: Mrs Françoise BEZERRA (CNES)

Slides RFPD2017_Intro_FB.pdf

30 Electron SEE- background and current status

A brief overwiew of on-going actions, an example of harmonized R&D.

Speaker: Mr Robert ECOFFET (CNES)

Slides Electron_SEU_-_08032017_final.pdf

31 Proton direct ionisation

The aim of this study is to investigate the proton direct ionization sensitivity of integrated circuits. This work includes the development of a calculation methodology to assess the direct ionization contribution to the proton SEE rate, the experimental characterization of a 45nm CMOS SRAM-based FPGA under low energy proton, as well as the space environment and calculation parameter impact on the presented methodology.

Speaker: Mr Nicolas Sukhaseum (TRAD)

Slides Proton_direct_ionization.pdf

11:00 Coffee break

32 TRADCARE: tool for SEE prediction in a radiation environment

TRADCARE (Tool for RADiation Constraints Analysis and Reliability Enhancement) is a tool allowing to predict SEE sensitivity of ASIC during its design phase. It is composed of interchangeable modules for each calculation step, starting from the whole IC design up to the SEE reliability prediction. Application cases will be presented.

Speaker: Mr Pierre Pourrouquet (TRAD)

Slides TRADCARE_Tool_for_SEE_prediction_in_a_radiation_environment.pdf

33 Recoil atom flux calculation in electronic components by Monte Carlo method

The evolution in the microelectronic field leads to the presence of high Z materials close to the sensitive volume of electronic components. Through interactions with highly energetic protons, as is the case in irradiation facilities or in space, recoil atoms can reach these sensitive volumes with high LET. Based on worst case hypotheses, this study showed the presence of high LET recoil particles in the component sensitive area, displayed their LET distribution and located their volume of origin.

Speaker: Mr Pierre Pourrouquet (TRAD)

Slides Recoil_atom_flux_calculation_in_electronic_components_by_Monte_Carlo_method.pdf

34 Weakened Cell /stuck bit

Status on the various actions on this subject and latest results

Speakers: Mrs Françoise BEZERRA (CNES), Ms Natalie Chatry (TRAD)

Slides RFPD2017_ISB_FB.pdf RFPD2017_ISB_NC_(part_2).pdf

35 Flash TID/SEE

This study is based on the work of Kay et al. [2012][2013] and investigates the effects of preliminary multiple write cycles on the radiation hardness of NAND Flash memories. This work includes the experimental characterization of 2 references under TID and heavy ions, and the test data post-treatment and analysis.

Speaker: Mr Nicolas Sukhaseum (TRAD)

Slides Multiple_write_cycles_on_flash_devices.pdf

36 Test facilities

This contribution will focus on recent prospective actions on « new » test facilities, e.g. 6-20 MeV electrons at Carcassonne Hopital, France, CHARM (CERN), new ion cocktail at UCL, etc…

Speaker: Mrs Françoise BEZERRA (CNES)

Slides RFPD2017_Facilities_FB.pdf

13:00 Lunch

Radiation Effects on EEE components: ESA (TEC-QEC)

37 Introduction

Speaker: Ali Zadeh (ESA)

Slides CNES_ESA_final_presentation_days.pdf

38 Displacement Damage test guideline

Speaker: Mr Thierry Nuns (ONERA)

Slides T._Nuns_DD_Guidelines_FP_Days_2017.ppt

39 Validation of NIEL for high energy (> 1MeV) electrons in Silicon

Speaker: Mr Thierry Nuns (ONERA)

Slides T._Nuns_Electron_NIEL_FP_Days_2017.ppt

40 ______________________schedule updated to include 20min delay

41 Verification of Co-60 TID testing representativeness for EEE components flown in the Jupiter environment

Speaker: Mr Marco Pinto (LIP)

Slides ESA_CNES_Final_Presentation_ECo60_v6.pdf

42 Part to part and lot to lot variability study of TID effects in bipolar linear devices

Speaker: Mr Nicolas Sukhaseum (TRAD)

Slides Part-to-part_and_lot-to-lot_variability.pdf

15:50 Coffee Break

43 Radiation characterization of European EEE components for space applications

Speaker: Dr Pierre Garcia (TRAD)

Transparents Presentation__ESA_CNES_2017_COO6.ppt

44 Test methods for SEE evaluations of ADCs and DACs

Speaker: Mr françois-xavier guerre (hirex engineering)

Slides ESA_-_ADCs_and_DAC_results.pdf

45 TID testing of state of the art NAND flash memories

Speaker: Dr Bendy Tanios (HIREX ENGINEERING)

Slides ESA_-_NAND_FLASHs_JUICE_Total_dose_summary_results_3.pdf

46 Heavy-Ion Micro Beam and Simulation Study of a Flash-Based FPGA Microcontroller Implementation

Speaker: Mr Carlos Urbina Ortega (ESA)

Slides Heavy-Ion_Micro_Beam_and_Simulation_Study_of_a_Flash-Based_FPGA_Microcontroller_Implementation_v1.1.pptx Heavy-Ion_Micro_Beam_and_Simulation_Study_of_a_Flash-Based_FPGA_Microcontroller_Implementation_v2.0_-_FINAL.pptx

Thursday 9 March

Radiation Effects on EEE components: ESA (TEC-QEC)

47 Irradiation characterisation of 2D imaging devices, memories and FPGAs for future ESA missions

Speaker: Mr ENOAL LE GOULVEN (TRAD)

Transparents ELG_ESA_CNES_Heavy_Ion_SEE_Testing_of_Kintex7_from_Xilinx.ppt

48 Radiation Evaluation of Digital Isolators

Speaker: Dr Michael Wind (Seibersdorf Laboratories)

Slides windm_REDI__PPT_FP_v1.0_pdf.pdf

49 Survey of total ionising dose tolerance of power bipolar transistors and Silicon Carbide devices for JUICE

Speaker: Dr Michael Steffens (Fraunhofer INT)

Slides PowerBipolar-SiC-TID-INT.pdf PowerBipolar-SiC-TID-INT.pptx

50 Total Ionizing Dose influence on the single event effect sensitivity of active EEE components

Speaker: Mr Lionel SALVY (TRAD)

Slides Synergy_ESA-CNE-0317.pdf

51 ESA supported Radiation Facility

Speakers: Dr Heikki Kettunen (University of Jyväskylä, Department of Physics), Mr Laurent Standaert (Université catholique de Louvain), Dr Wojtek Hajdas (PSI)

Transparents

• PIF2016_Summary_FPD_ESTEC2017.03.09.pptx.pdf
• RADEF_Status_Report_2017.pdf
• UCL_radiation_days_2017.pdf

10:50 Coffee Break

52 Risk assessment of SEE events due to high energy electrons during the JUICE mission

Speaker: Mr Nicolas Sukhaseum (TRAD)

Slides Electron_SEE_risk_assessment.pdf

53 Single Event Burnout testing of high power schottky diodes

Speaker: Dr Pierre Garcia (TRAD)

Transparents Presentation__ESA_CNES_2017_Schottky.ppt

54 Re-issue Radiation Characterisation of GaAs power devices in support of European Radiation Hardness

Speaker: Mr Jeffrey Chuan (Thales Alenia Space España)

Slides SEE_testing_on_GaAs_test_vehicles_ESTEC_9-3-17.pdf SEE_testing_on_GaAs_test_vehicles_ESTEC_9-3-17.pptx

55 Laser Study of SETs in 65nm Bulk Technology

In this presentation, we review current work on SET measurement including on-chip and off-chip techniques. We present test results for SET measurements using the SPA laser at the CNES, Toulouse and the TPA laser at NRL, Washington. Results are presented for SETs in elementary transistors, logic gates as as for complex digital circuits

Speaker: Mr Adrian Evans (IROC Technologies)

Slides EVANS_PRESN_1.pdf

56 Comprehensive SEE Component Qualification

This presentation provides a snapshot of the AO8191 TRP activity which involves the comprehensive radiative characterization of 6 components (4 SRAMs, 1 SoC and 1 FPGA) using heavy-ions, high- and low-energy protons and electrons. The test setups and methodologies will be presented as well as initial heavy-ion test results. In one SRAM component, an unusual SEFI failure mode was identified and was investigated in detail using the SPA laser at the CNES, Toulouse.

Speaker: Mr Adrian Evans (IROC Technologies)

Slides EVANS_PRESN_2.pdf