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ATL-INDET-PROC-2011-042 03 December 2011 Overview of Silicon Pixel Sensor Development for the ATLAS Insertable B-Layer (IBL) S. Grinstein * , on behalf of the ATLAS Collaboration * Institut de F´ ısica d’Altes Energies (IFAE) and ICREA. Universitat Aut´ onoma de Barcelona (UAB), E-08193 Bellaterra (Barcelona), Spain Abstract—The ATLAS Pixel Detector is the innermost part of the ATLAS tracking system and is critical for track and vertex reconstruction. In order to preserve the tracking performance notwithstanding the increasing instantaneous luminosity deliv- ered by the LHC, ATLAS plans to introduce a new pixel layer (IBL) mounted directly on a reduced diameter beam pipe. The IBL will have to sustain an estimated radiation dose, including safety factors, of 5 × 10 15 neq /cm 2 . Two sensor technologies are currently being considered for the IBL, planar n-on-n slim edge and 3D double sided designs. Results of the characterization, irradiation and beam test studies of IBL pixel devices are presented. Index Terms—ATLAS upgrade, pixel detectors, 3D pixels, radiation hardness, high energy physics I. I NTRODUCTION T HE ATLAS [1] Inner Detector (ID) [2] provides charged particle tracking with high efficiency. With three cylin- drical barrel layers between 50 and 120 mm around the beam axis (and three forward and backward endcap disks), the Pixel Detector [3] significantly enhances track impact parameter resolution, and therefore, vertex reconstruction and b-tagging. These in turn are critical for several ATLAS analyses like searches for the Higgs boson or super-symmetric particles. To further improve the performance of the silicon system and to compensate the possible deterioration that the innermost layer of the pixel detector may suffer after the first few years of operation, the ATLAS Collaboration will insert an additional pixel layer (Insertable B-Layer or IBL [4]) inside the current Pixel Detector during the LHC shutdown planned for 2013- 2014. Until complete replacement of the entire inner detector for the high luminosity LHC, the IBL will have to sustain an estimated radiation dose of 5 × 10 15 n eq /cm 2 , where n eq represents a particle with the non-ionizing energy loss of a 1 MeV neutron. The baseline design of the IBL is a barrel layer consisting of 14 staves mounted directly on a new (smaller) beam pipe with a tilt angle of 14 (see Fig. 1). The average radius of the sensitive area is 33 mm. Each stave is equipped with 16 to 32 modules depending on the final sensor layout. Two sensor technologies are currently under investigation for the IBL modules, planar and 3D sensors. Planar modules are interconnected to two front-end chips doubling their length in the z direction with respect to the 3D modules, which are read out by a single chip. A stave layout being considered combines planar and 3D sensors as shown in Fig. 1. The IBL design foresees a material budget of X/X 0 =1.5% at z =0 cm for Fig. 1. Cross section detail of the IBL (top). The 14 staves are mounted directly on the beam pipe. The figure below shows a possible stave layout which combines planar and 3D sensor technologies. the loaded stave. Due to space restrictions the IBL modules will have no overlap in the z direction, making imperative the need of very small inactive edges to minimize efficiency losses. The IBL design assumes an integral luminosity of 550 fb -1 and a peak luminosity of 3 × 10 34 cm -2 s -1 to determine the sensor requirements. Including conservative safety factors, this translates into a NIEL dose of 5 × 10 15 n eq /cm 2 and an ionization dose of 250 Mrad. Up to this fluency, IBL modules are required to provide a hit efficiency in the active area > 97% and a r - φ resolution better than 10μm for minimum ionization particles. Other constraints to achieve this efficiency are the operational temperature, set at -15 C, and the maximum bias voltage, set at 1000 V. The power dissipation should not exceed 200 mW/cm 2 at the nominal temperature. Finally, the sensor design has to minimize the dead regions, in order to achieve this both planar and 3D sensors target inactive edges of 200μm.
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Page 1: Overview of Silicon Pixel Sensor Development for the ATLAS …inspirehep.net/record/1196901/files/ATL-INDET-PROC-2011... · 2012-11-16 · (Germany) which also supplied ATLAS with

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Overview of Silicon Pixel Sensor Developmentfor the ATLAS Insertable B-Layer (IBL)

S. Grinstein∗, on behalf of the ATLAS Collaboration∗Institut de Fısica d’Altes Energies (IFAE) and ICREA. Universitat Autonoma de Barcelona (UAB), E-08193

Bellaterra (Barcelona), Spain

Abstract—The ATLAS Pixel Detector is the innermost part ofthe ATLAS tracking system and is critical for track and vertexreconstruction. In order to preserve the tracking performancenotwithstanding the increasing instantaneous luminosity deliv-ered by the LHC, ATLAS plans to introduce a new pixel layer(IBL) mounted directly on a reduced diameter beam pipe. TheIBL will have to sustain an estimated radiation dose, includingsafety factors, of 5× 1015 neq/cm2. Two sensor technologies arecurrently being considered for the IBL, planar n-on-n slim edgeand 3D double sided designs. Results of the characterization,irradiation and beam test studies of IBL pixel devices arepresented.

Index Terms—ATLAS upgrade, pixel detectors, 3D pixels,radiation hardness, high energy physics

I. INTRODUCTION

THE ATLAS [1] Inner Detector (ID) [2] provides chargedparticle tracking with high efficiency. With three cylin-

drical barrel layers between 50 and 120 mm around the beamaxis (and three forward and backward endcap disks), the PixelDetector [3] significantly enhances track impact parameterresolution, and therefore, vertex reconstruction and b-tagging.These in turn are critical for several ATLAS analyses likesearches for the Higgs boson or super-symmetric particles. Tofurther improve the performance of the silicon system and tocompensate the possible deterioration that the innermost layerof the pixel detector may suffer after the first few years ofoperation, the ATLAS Collaboration will insert an additionalpixel layer (Insertable B-Layer or IBL [4]) inside the currentPixel Detector during the LHC shutdown planned for 2013-2014. Until complete replacement of the entire inner detectorfor the high luminosity LHC, the IBL will have to sustainan estimated radiation dose of 5 × 1015 neq/cm2, where neq

represents a particle with the non-ionizing energy loss of a1 MeV neutron.

The baseline design of the IBL is a barrel layer consistingof 14 staves mounted directly on a new (smaller) beam pipewith a tilt angle of 14◦ (see Fig. 1). The average radius ofthe sensitive area is 33 mm. Each stave is equipped with16 to 32 modules depending on the final sensor layout. Twosensor technologies are currently under investigation for theIBL modules, planar and 3D sensors. Planar modules areinterconnected to two front-end chips doubling their length inthe z direction with respect to the 3D modules, which are readout by a single chip. A stave layout being considered combinesplanar and 3D sensors as shown in Fig. 1. The IBL designforesees a material budget of X/X0 = 1.5% at z = 0 cm for

Fig. 1. Cross section detail of the IBL (top). The 14 staves are mounteddirectly on the beam pipe. The figure below shows a possible stave layoutwhich combines planar and 3D sensor technologies.

the loaded stave. Due to space restrictions the IBL moduleswill have no overlap in the z direction, making imperativethe need of very small inactive edges to minimize efficiencylosses.

The IBL design assumes an integral luminosity of 550 fb−1

and a peak luminosity of 3 × 1034 cm−2s−1 to determinethe sensor requirements. Including conservative safety factors,this translates into a NIEL dose of 5 × 1015 neq/cm2 andan ionization dose of 250 Mrad. Up to this fluency, IBLmodules are required to provide a hit efficiency in the activearea > 97% and a r − φ resolution better than 10µm forminimum ionization particles. Other constraints to achievethis efficiency are the operational temperature, set at −15◦ C,and the maximum bias voltage, set at 1000 V. The powerdissipation should not exceed 200 mW/cm2 at the nominaltemperature. Finally, the sensor design has to minimize thedead regions, in order to achieve this both planar and 3Dsensors target inactive edges of 200µm.

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II. THE FRONT-END CHIP FOR THE IBL

To face the challenges of the radiation and high occupancyenvironment of the inner radii of the ATLAS ID, while alsoimproving the physics performance of the current system, thefront-end readout electronics and the sensor technology used inthe present Pixel Detector have to be upgraded and the materialbudget subjected to tight requirements. The readout chip usedin the present detector, the FE-I3 [5], was excluded from theIBL design because its active footprint is too small and its hitrate capability not high enough [4]. The IBL will utilize theFE-I4 integrated circuit [6], designed in 130 nm technologywhich features an array of 80×336 pixels with a pixel size of50× 250 µm2, The large size of the chip, 20.2× 19.0 mm2,leads to a larger active fraction than its predecessor (89%vs 74%). The sensors will be DC coupled to the chip withnegative charge collection. Each readout channel containsan independent amplification stage with adjustable shaping,followed by a discriminator with independently adjustablethreshold. The chip operates with an externally supplied clock,nominally 40 MHz. The time over threshold (ToT) with 4-bitresolution together with the firing time are stored for a latencyinterval until a trigger decision is taken. The primary outputrate is 160 Mb/s, four times faster than the output rate of theFE-I3 chip.

III. PIXEL SENSORS FOR THE IBL

Two sensor technologies are being considered for the IBL,planar and 3D sensors. Planar modules consist of 2-chipassemblies while 3D modules consist of a single chip. Bothmodule designs offer similar nominal acceptance. However,the requirements of the two technologies in terms of tem-perature and bias voltage differ, being less restrictive for3D sensors. Both technologies have to demonstrate that theysatisfy the IBL requirements in terms of performance afterirradiation to 5×1015 neq/cm2. Planar and 3D sensors with theIBL design have been fabricated, and have been interconnected(bump-bonded) with the FE-I4 read out chip. These planar and3D bare assemblies were wire-bonded to an electronic card tocarry out the characterization and test-beam studies need toevaluate the technologies. The wire-bonded devices are alsoreferred to as single chip assemblies.

A. Planar Sensors

The IBL planar sensors rely on the proven technology ofthe current ATLAS Pixel Detector [7] [8], n-on-n pixels ona diffusion oxygenated float-zone silicon bulk. The chosenthickness for the substrate is 200 µm, a sizable reduction fromthe 256 µm featured in the current Pixel Detector. Isolationbetween the n+ implants is obtained through the moderated p-spray technique. A bias grid [7] is integrated into the design todetermine the sensor electrical quality before bump-bonding.In order to reduce the inactive edges, the planar IBL designshifts the guard rings on the ohmic side beneath the outerpixels. To keep the sensor length constant, the edge pixels areextended to 500 µm (see Fig 2). A distortion on the electricfield on the sensor edge will be introduced by this layout, butthe charge collection after irradiation occurs primarily in the

Fig. 2. Planar sensor IBL design [4]. Planar modules consist of two frontend readout chips. The detail on the left shows the edge pixels which extendover the ohmic side guard rings to provide an inactive edge of about 200µm.

region directly beneath the n+ implant. The inactive edge ofplanar devices achieved with this design is around 200 µm(see Section VII).

The planar IBL sensors have been produced at CiS [9](Germany) which also supplied ATLAS with sensors for thecurrent Pixel Detector.

B. 3D Sensors

The 3D pixel sensor design exploits recent silicon technol-ogy advances to produce column-like electrodes that penetratethe substrate, instead of being implanted on the wafer sur-face [10]. The depletion region thus grows parallel to the wafersurface. The ∼ 10 µm diameter columns are alternatively n-and p-type doped defining the pixel configuration. The 3Ddesign is intrinsically radiation hard since it decouples theelectrode distance from the bulk thickness, making possiblethe reduction of the charge collection path without reducingthe amount of sensor material the charge particles traverse.

IBL 3D sensors have been manufactured in two productionfacilities, CNM [11] (Spain) and FBK [12] (Italy), with thesame specifications (see also Section IV). The sensors areproduced on a 230µm thick wafer with a double sided process,i.e. the n- and p-type columns are etched from the oppositesides of the substrate. The pixel configuration consists of twon-type readout electrodes connected at the wafer surface alongthe 250 µm long pixel direction, surrounded by six p-typeelectrodes which are shared with the neighboring pixels, seeFig. 3.

The CNM 3D sensor design features 210 µm long columnswhich are isolated on the n+ side with p-stop implants. Theedge isolation is accomplished with a combination of a n+

3D guard ring, which is grounded, and fences which are atthe bias voltage potential from the ohmic side (see Fig. 3).The inactive edge region is about 200 µm long. The sensorquality before wafer dicing is evaluated on the 3D guard ring.

The FBK 3D sensor design presents pass-through columnsisolated on the junction side with the p-spray technique. A200 µm long ohmic fence isolates the pixel area from theedges in the z direction. The sensor quality is evaluated beforedicing using a temporary metal line that connects 336 pixelsinto a strip, see Fig. 4. A total of 80 strips that are connected toa probing pad located outside the active region of the sensor,allow to evaluate the electrical characteristics of the device.

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Fig. 3. Design of the CNM 3D sensors (top) [13]. The electrodes do notpenetrate the full thickness of the sensor. Below a detail of the productionmask is shown. The two electrode configuration is visible as well as the 3Dguard fence.

Fig. 4. Detail of the FBK 3D design [14]. The temporary metal strips are usedto evaluate the electrical characteristics of the device before bump-bonding.

After the measurements are completed the temporary metallayer is removed.

IV. SELECTION OF SENSORS FOR THE IBL

Both planar and 3D sensors have to meet the IBL waferquality and electrical specifications [4]. The most criticalparameters to determine the sensor quality are the leakagecurrent and the breakdown voltage. Planar sensors are expectedto be fully depleted at 30 V, and required to have a breakdownvoltage greater than 60 V. Fig. 5 shows the current versus biasvoltage (”I-V”) measurements at room temperature for severalunirradiated planar sensors after dicing. The entire sensor isbaised uniformly through the bias grid structure [7].

The depletion voltage for the IBL 3D sensors is ∼ 5−10 Vand the breakdown voltage is required to be greater than 25 V.The CNM sensors are evaluated by measuring the I-V behavioron the 3D guard ring. Fig. 6 shows the I-V characteristicsof two sensors, before dicing and after bump-bonding. Thebreakdown voltage improves in the bump-bonded assembliesprobably due to the reduction of the stress across the substrate

Fig. 5. Planar I-V curves for several sensors measured at room temperatureafter dicing. The vertical line indicates the minimum breakdown voltagerequired (60 V).

Fig. 6. Leakage current measured at room temperature before dicing andafter bump-bonding for two CNM 3D sensors (top). The bottom plot shows theleakage current distribution measured in a bump-bonded device. The currentdistribution is along the edges, where the 3D guard fence is located.

after dicing. The I-V curves can not be directly comparedsince the measurement after bump-bonding is done on the fullsensor. However, the measurement on the 3D guard ring isfound to be very indicative of the behavior of the full sensor,since the current is largest on the edge region where the 3Dguard ring is located. This has been verified by mapping theleakage current along the bump-bonded assemblies as shownin Fig. 6.

The devices produced at FBK are tested using 80 temporarymetal lines that allow to detect fabrication defects on the fullsensor before dicing. Fig. 7 shows the I-V characteristics ofall the strips in an FBK sensor, the breakdown voltage for thisdevice is above 50V.

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Fig. 7. I-V curves measured at room temperature on the the 80 temporarymetal lines of an FBK device.

TABLE IPLANAR AND 3D SAMPLES USED TO EVALUATE THE TECHNOLOGIES ATLABORATORY AND BEAM TESTS. THE ESTIMATED FLUENCIES HAVE AN

ERROR OF ABOUT 20%. THE PLANAR CONSERVATIVE DESIGN FEATURESAN INACTIVE EDGE OF APPROXIMATELY 1 MM. THE EDGE DESIGNS ARE

DISCUSSED IN SECTION III.

Name Technology, Thickness Edge Design Fluency (neq /cm2)

LUB2 Planar, 250 µm Slim 4E15 {n}SCC60 Planar, 200 µm Slim 5E15 {p}SCC24 Planar, 200 µm Conservative 6E15 {p}CNM81 CNM 3D, 230 µm GR+Fences 5E15 {n}CNM34 CNM 3D, 230 µm GR+Fences 5E15 {p}FBK11 FBK 3D, 230 µm Fences 5E15 {p}FBK13 FBK 3D, 230 µm Fences Unirradiated

V. IRRADIATION OF IBL DEVICES

In order to investigate the behavior of the devices afterthe radiation doses required for the IBL, several planar and3D assemblies were irradiated. The irradiation program wascarried out at the Karlsruhe Institute of Technology (Germany)using a 23 GeV proton beam, and at the Jozef Stefan Institute(Slovenia) with reactor neutrons. Though the assemblies wereexposed to different fluencies, only results with samples irra-diated to fluencies close to the IBL target of 5×1015 neq/cm2

will be included below. All the samples were annealed for2 hours at 60 C, accounting for different previous annealinghistory between the devices when possible. Table I summarizesthe samples used in the results presented in the next sections.

VI. CHARACTERIZATION OF IBL DEVICES

Before the performance of the devices is studied in beam-tests, it is necessary to determine the operational parametersin terms of electronics threshold settings, bias voltage andnoise. A low threshold setting is desirable to increase de-tection efficiency, however, the associated increase in noisecould deteriorate the overall performance. Similarly, high biasvoltages will increment the collected charge, but the increaseon the leakage current could raise the device noise beyondacceptable levels.

A priori, each sensor technology has different character-istics, that may influence the operational parameters, for

Fig. 8. Noise occupancy versus electronic threshold for a planar proton irra-diated device (SCC24, see Table I). Below ∼ 1000 electrons the occupancybecomes too large to operate the device.

Fig. 9. Charge collection and noise occupancy versus the effective biasvoltage (corrected for the drop across the high voltage filter) for a protonirradiated CNM device (CNM34). A bias voltage of 160 V provides a chargecollection close to the plateau, while maintaining a low level of noise.

example the input capacitance presented to the electronics.However, both planar and 3D devices were found to be ableto operate at thresholds as low as 1000 electrons with similarnoise levels of around 150 electrons. Fig. 8 shows the deviceoccupancy as a function of the electronic threshold for a planardevice. A 1500 electron threshold was used for beam-test ofboth planar and 3D devices (see Section VII), allowing a500 electron safety margin in order to ensure low noise levels.

In the case of the planar device the bias voltage limit isgiven by the electrical engineering constraints. In principle, itshould be as high as possible to increase charge collection.Thus planar devices will be operated at 1000 V after beingirradiated to the IBL fluency. In the case of 3D sensors, theelectrical constraints of IBL are easily met. However, theoperational voltage has to be optimized to ensure good chargecollection while maintaining acceptable noise levels. Fig. 9shows the charge collection and noise occupancy for a protonirradiated CNM device (CNM34) as a function of the biasvoltage corrected for the voltage drop across the electronichigh voltage filter. The optimal voltage setting of 160 Vensures high charge collection efficiency while maintaining thenoise level low. Both CNM and FBK devices were operatedat 140-160 V during the test beam studies presented in thisarticle (see Section VII).

VII. TEST-BEAM STUDIES OF IBL DEVICES

Critical performance parameters, such as hit efficiency andposition resolution, can only be determined at beam tests. Pla-

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Fig. 10. Planar and 3D devices mounted between the EUDET telescope [15]planes during the 2011 IBL beam tests at CERN.

nar and 3D IBL devices were studied in the CERN north areawith a 120 GeV π-beam from the Super Proton Synchrotronduring June and September 2011. The EUDET [15] beam tele-scope was used for tracking purposes. The telescope consistsof six Mimosa tracking planes, the trigger hardware and thereadout data acquisition system, and provides a ∼ 3µm trackpointing resolution. The devices under tests are placed betweenthe telescope planes. Data at different incidence angles, 0◦ and15◦, have been recorded to evaluate the device performance.The 15◦ data, taken with the devices rotated in the long pixeldirection, correspond to the approximate expected incidenceangle for the IBL configuration. The devices under test werecooled down to the IBL operational temperature by meansof dry ice and a heating system was used to regulate thetemperature. Fig. 10 shows four devices mounted between thetelescope planes and rotated by 15◦ in the long pixel directionwith respect to the incoming particle beam.

The hit efficiency is determined from extrapolated trackson the devices, after track quality cuts have been applied. Ahit on the device under test is searched for in a 3 × 3 pixelwindow around the track position.

The hit efficiency for a planar proton irradiated device(SCC60) is shown in Fig. 11 (top). The device was operatedat 1000 V and the sensor temperature estimated at −15◦ C.The plot shows the efficiency as a function of the track hitposition folded into a two by two cell in order to highlight thepixel structure. Noisy and dead pixels are not considered in theefficiency calculation. The overall efficiency was 97.6% at 15◦

incidence angle. The apparent loss of efficiency in the left sideof the pixel is associated to the bias grid structure. Also shownin Fig. 11 (bottom) is the efficiency of the pixels of the edge ofthe device, in this case for the planar device LUB2. The plotshows the efficiency along the long pixel direction, the lengthof the inactive edge region in this direction is of ∼ 200µmwhile the overall efficiency is 99.0%. Again, the efficiencyloss resulting from the punch through structure associated tothe bias grid can be observed.

The hit efficiency for some 3D devices is shown in Fig. 12.The top plot shows the efficiency for a CNM neutron irradiated

Fig. 11. Hit efficiency for a planar proton irradiated device (SCC60) foldedinto a two by two pixel area at a 15◦ incidence angle. The overall efficiencyfor this device with a bias voltage of 1000 V was 97.6% (see text for details).

Fig. 12. Hit efficiency pixel maps for three 3D devices. The plot on the topshows the hit efficiency for perpendicular tracks for a neutron irradiated CNMdevice (CNM81) operated at 160 V. The overall efficiency for this device is97.5%. The middle plot shows the efficiency for a proton irradiated deviceoperated at 160 V (CNM34). The track incidence is 15◦ and the overallefficiency is 98.7%. The bottom plot shows the efificiency for an unirradiatedFBK device operated at 20 V. For normal incidence tracks the efficiency is98.8%. The pass through electrodes are clearly visible.

device (CNM81) operated at a bias voltage of 160 V. Forperpendicular tracks the inefficient areas associated to the p+

electrodes are clearly visible. This is not the case for thereadout electrodes, which at this voltage, collect enough chargefrom the region that separates the electrode from the ohmicside to detect the passing particles. The overall efficiency forCNM81 under this configuration is 97.5%. The efficiency losscaused by the electrodes is expected to be larger at normalincidence. The middle plot of Fig. 12 shows the efficiencyof a proton irradiated CNM device (CNM34) at 15◦ trackincidence angle, operated at 160 V. The associated efficiencyfor this device in this configuration is 98.7%. The effect ofthe pass-through electrodes can be seen in the bottom plot ofFig. 12, which shows the efficiency for an unirradiated FBKdevice (FBK13) at normal incidence and operated at 20 V.As expected for the FBK design, both electrodes show similarregions of lower efficiency. The overall hit efficiency for thedevice is 98.8%.

The position resolution of the IBL detector will be criticalfor the physics program A preliminary estimation of the posi-tion resolution of the IBL devices has been carried out basedon the residual distribution in two pixel clusters. The position

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Fig. 13. Two hit cluster resolution for a proton irradiated FBK device(FBK11). The data was taken with tracks with an incident angle of 15◦ andwith the device operated at 140 V. The estimated resolution is of 9.5µmincluding the contribution from the track resolution and residual systemmisalignment.

of the device hit has been estimated by using the ToT weightedmean of the clusters. Fig.13 shows the residual distribution fora proton irradiated FBK device (FBK11) operated at 140 Vfor data taken at an incidence angle of 15◦. The estimateddevice position resolution of 9.5µm includes the contributionfrom the track resolution and any residual misalignment of thesystem.

VIII. CONCLUSIONS

The ATLAS Collaboration will install a fourth pixel layer in2013-2014. The IBL will be mounted directly on a new beam-pipe at an average radius of 3.3 cm. Two pixel technologies arebeing evaluated for the IBL, planar and 3D sensors. A possiblelayout that combines both technologies is under consideration.Planar and 3D sensor pre-productions have been completedand the devices have been characterized and investigatedwith beam tests. Both technologies performed within the IBLrequirements after irradiation to fluencies of 5×1015 neq/cm2.Final planar and 3D sensor productions are underway.

REFERENCES

[1] The ATLAS Collaboration, ”The ATLAS Experiment at the CERN LargeHadron Collider”, JINST 3 S08003 (2008).

[2] ATLAS Collaboration, ”The ATLAS Inner Detector commissioning andcalibration”, EPJC 70 (2010) 787.

[3] G. Aad et al., ”ATLAS Pixel Detector electronics and sensors”, JINST 3P07007 (2008).

[4] The ATLAS IBL Collaboration, ”ATLAS Insertable B-Layer TechnicalDesign Report”, CERN-LHCC-2010-013, 2010.

[5] I. Peric, et al., Nucl. Instrum. Methods in Phys. Res. A 565, 178 (2006).[6] M. Garcia-Sciveres, et al., Nucl. Instrum. Methods Phys. Res. A 636,

S155 (2011).[7] M.S. Alam, et al., Nucl. Instrum. Methods Phys. Res. A 456, 217 (2001).[8] G. Aad, et al., Journal of Instrumentation, 3(07):P07007, 2008.[9] CiS, Erfurt (Germany), http://www.cismst.orgi/en/.[10] S. Parker, C. Kenney, and J. Segal, Nucl. Instrum. Methods Phys. Res.

A 395, 328 (1997).[11] Centro Nacional de Microelectronica (CNM), Barcelona (Spain),

http://www.imb-cnm.csic.es/.[12] Fondazione Bruno Kessler (FBK), Trento (Italy), http://www.fbk.eu/.[13] G. Pellegrini, et al., Nucl. Instrum. Methods Phys. Res. A 592, 38 (2008).[14] G. Della Betta, et al., Nuclear Science Symposium Conference Record

(NSS/MIC), 2010 IEEE, 382 (2010).

[15] E. Corrin, Nuclear Science Symposium Conference Record (NSS/MIC),2009 IEEE, 816 (2009).


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