Can silicon operate beyond 10 n/cmn/cmssd-rd.web.cern.ch/ssd-rd/rd/talks/watts-rd-2001.pdf ·...
Transcript of Can silicon operate beyond 10 n/cmn/cmssd-rd.web.cern.ch/ssd-rd/rd/talks/watts-rd-2001.pdf ·...
Can silicon operate beyond 10Can silicon operate beyond 101515 n/cmn/cm22 ??DEFECT ENGINEERING DEFECT ENGINEERING –– Oxygen Oxygen Dimer SiDimer Si
S. J. Watts, C. Da Via', A. Karpenko, A. Kok, Brunel University UK
OUTLINEOUTLINE
11-- BACKGROUNDBACKGROUND22-- KEY ISSUE KEY ISSUE –– signal efficiency in irradiated detectorssignal efficiency in irradiated detectors33-- SOLUTIONSSOLUTIONS
aa OPERATING CONDITIONS OPERATING CONDITIONS ( T, Forward/Reverse Bias ? )( T, Forward/Reverse Bias ? )bb DEFECT ENGINEERING DEFECT ENGINEERING ( ( Dimer Dimer oxygenated oxygenated SiSi))cc DEVICE ENGINEERING ( e.g. 3D Sherwood Parker)DEVICE ENGINEERING ( e.g. 3D Sherwood Parker)
44-- CONCLUSIONSCONCLUSIONS
qqV is weighting potentialV is weighting potentialVVxx
VVcc
Signal = q xSignal = q x PPqcqc(x) x CORR x ((x) x CORR x (VVcc –– VVxx))
Drift Time = d/Drift Time = d/µµEE
ττTT = ( = ( NNTTσσVVth th ) ) --11
tteffeff and and µµ varyvarywith temperaturewith temperature
PPqiqi = 1 = 1 –– PPqcqc
PPqi qi prop. 1/prop. 1/tteffeff
RAMO’sRAMO’s theorem + trappingtheorem + trapping
0
0.02
0.04
0.06
0.08
0.1
10-11
10-10
10-9
10-8
10-7
10-6
10-5
10-4
0.001
50 100 150 200 250 300 350
Signal density = 1016 cm-3, Trap density = 1015 cm-3
Pqi
Time C
onstant (s)
Temperature ( K)
Vacancy-Oxygenτ
τ
e
τ
τ
T
c
ττcc = (n= (nss σ σ vvthth) ) --11
ττTT = (N= (NTT σσ vvthth) ) --11
ττee prop. exp(prop. exp(∆∆E/E/kTkT))
1/1/ττ = 1/= 1/ττee + 1/+ 1/ττcc
Same theory as usedSame theory as usedin in CCD’sCCD’s
For depletion case (Reverse Bias)For depletion case (Reverse Bias)T < 200K Trapping ControlledT < 200K Trapping ControlledT > 200K Emission ControlledT > 200K Emission Controlled
For Forward BiasFor Forward BiasAlways Trapping ControlledAlways Trapping Controlled
0
0.05
0.1
0.15
0.2
0.25
100 150 200 250 300
Pqi
Temperature (K)
VO
V2
Cluster
Neutron
Proton
NT
= 1015 cm-3
For electron trapping For electron trapping –– ttDD = 10 ns= 10 nsConclusionConclusion
NIEL ViolationNIEL Violation
Charged hadrons worseCharged hadrons worse
Aside :Aside :PPqiqi = (= (ττ//ττTT) x (1 ) x (1 ––exp(exp(--ttDD//ττ))))Same in Same in CCDsCCDs
Introduction rates ( cmIntroduction rates ( cm--1 1 ) ) nn ppVOVO 0.60.6 0.96 0.96 V2 + ClusterV2 + Cluster 1.21.2 1.2 1.2
0
1
2
3
4
5
6
7
8
50 100 150 200 250 300 350
k = (
t eff x
Fluen
ce )-1
( 10
-16 ns
-1 cm
2 )
Temperature (K)
Protons
Neutrons
Data from 220K to 300K from -
Kramberger et al.ROSE TN01-01 Submitted to NIMA
Electron Trapping - calculation scaled to Kramberger data at 250K
Note:Note:
Kramberger Kramberger et al.et al.See NIEL ViolationSee NIEL Violationn/p trapping NOT the n/p trapping NOT the same for same equiv.same for same equiv.1 1 MeV MeV n n fluencefluence..
Conclusion:Conclusion:VO causes this differenceVO causes this difference
NOTE : Below 200K this parameter is the same forNOTE : Below 200K this parameter is the same forForward and Reverse biasForward and Reverse bias
0
500
1000
1500
2000
2500
50 100 150 200 250 300 350
FOR FLUENCE = 1014 cm-2
E = 104 V cm-1
Eff
ectiv
e Tr
appi
ng L
engt
h ( m
icro
ns)
Temperature (K)
Neutron
Neutron
Proton
Proton
Electrons
Holes
10
15
20
25
30
2 106
4 106
6 106
8 106
1 107
1.2 107
50 100 150 200 250 300 350
teffnteffnh
VdeVdh
Eff
ectiv
e Tr
appi
ng T
ime
(ns) D
rift Velocity (cm
s-1)
Temperature (K)
E = 104 V cm-1 ( 1V/micron)
1014 n cm-2
neutronsneutrons
Data for neutron and protons for effective trapping time 220KData for neutron and protons for effective trapping time 220K--300K from300K fromKrambergerKramberger et alet al
VOVO
LLeffeff == ττeffeff xx VVdriftdrift
EFFECTIVE DRIFT LENGTHEFFECTIVE DRIFT LENGTH
SIGNAL FORMATION SIGNAL FORMATION -- RAMO'S THEOREMRAMO'S THEOREM
IMPORTANCE OF THE WEIGHTING POTENTIALIMPORTANCE OF THE WEIGHTING POTENTIAL
PADS AND SEGMENTED DETECTORS ARE VERY DIFFERENTPADS AND SEGMENTED DETECTORS ARE VERY DIFFERENT
Holes Holes ElectronsElectrons
0
0.2
0.4
0.6
0.8
1
0 0.005 0.01 0.015 0.02 0.025 0.03 0.035
1E14 ncm-2 200KSig
nal e
/ Sig
nal h
/ Sig
nal T
otal
Distance (cm)
p+ n+
CO
LLEC
TION
ELE
CTR
OD
E
Weighting Potential
PAD DETECTOR
Signal e
Signal h
Signal Total
0
0.2
0.4
0.6
0.8
1
0 0.005 0.01 0.015 0.02 0.025 0.03 0.035
1E15 n cm-2 200K
Sig
nal e
/ Sig
nal h
/ Sig
nal T
otal
Distance (cm)
p+ n+
CO
LLEC
TION
ELE
CTR
OD
E
STRIP DETECTOR
Weighting Potential
Signal h
Signal e
Signal Total
0
20
40
60
80
100
0 1 1015 2 1015 3 1015 4 1015 5 1015 6 1015
200K Simulation 104 V/cm 300 Micron detector
PAD e+h
STRIP e+h
STRIP e+h n+
"CC
E"
Fluence n cm-2
PROTONS
Note:Note:Pad results samePad results samewhether you collectwhether you collectAt n+ or p+ contactAt n+ or p+ contact
CONCLUSION CONCLUSION –– collect electrons !!!!!collect electrons !!!!!If one can remove VO then we should do betterIf one can remove VO then we should do better
SOLUTIONS (b) DEFECT ENGINEERING SOLUTIONS (b) DEFECT ENGINEERING -- O DIMERO DIMER
OOii
OOii
SiSiSiSi
HIGH TEMPERATURE 60Co γ IRRADIATIONAT T > 350 0C VO BECOMES MOBILE AND CAUSES OXYGEN TO CLUSTER
QUASI CHEMICAL REACTIONS:
V+Oi => VOi
VOi + Oi => VO2i
I + VO2i => O2i
SiSiSiSi
OOi SiSii
OXYGEN INTERSTITIALOXYGEN INTERSTITIAL OXYGEN DIMEROXYGEN DIMER
Method variation on L. Lindstroem work
VOVO ----------------> VO> VO22 NEUTRALNEUTRALVV22OO ----------------> V> V22OO22 NEUTRALNEUTRAL
EXPECT CHANGE IN MACROSCOPIC EFFECTSEXPECT CHANGE IN MACROSCOPIC EFFECTSSHOULD IMPROVE CCE FOR ELECTRONSSHOULD IMPROVE CCE FOR ELECTRONS
ALSO ALSO –– OO2i2i diffuses very rapidly. Possibility of lowdiffuses very rapidly. Possibility of low--temp diffusion For DOFZ !!!!temp diffusion For DOFZ !!!!
-7 10 11
-6 10 11
-5 10 11
-4 10 11
-3 10 11
-2 10 11
-1 10 11
0
1 1011
100 150 200 250 300
366D309D
Con
cent
ratio
n (c
m-3
)
Temperature (K)
E(170)0
4 1011
8 1011
1.2 10 12
1.6 10 12
100 150 200 250 300
309D
Con
cent
ratio
n ( c
m-3
)
Temperature (K)
H(200)
H(144)
H(80?)
DEFECTS IN “DIMERED” MATERIAL
309D Oxygenated and “309D Oxygenated and “dimereddimered””366D Standard and “366D Standard and “dimereddimered””
Electron (E) or Hole (H) trap Energy Level (eV) Identification
E(170) Ec - 0.32 Probably VOH [11]
H(200) Ev + 0.36 CiOi (0/+) Charge state [1]
H(144) Ev + 0.2 Unknown
H(80?) Approx. Ev + 0.1 Not fully resolved. Unknown.
EXPERIMENTAL RESULTS EXPERIMENTAL RESULTS IV and NIV and Neffeff AFTER AFTER 2424GeV/c pGeV/c p−−irradiationirradiation
0.0 100
5.0 1011
1.0 1012
1.5 1012
2.0 1012
2.5 1012
3.0 1012
3.5 1012
4.0 1012
0 5 1013 1 1014 1.5 1014 2 1014 2.5 1014 3 1014 3.5 1014 4 1014
S
SD
O
OD
Nef
f (cm
-3)
Fluence (protons/cm2)
24 GeV/c proton irradiation - CERN scenario
0.0 100
2.0 10-3
4.0 10-3
6.0 10-3
8.0 10-3
1.0 10-2
1.2 10-2
1.4 10-2
0 5 1013 1 1014 1.5 1014 2 1014 2.5 1014 3 1014 3.5 1014 4 1014
S
SD
O
OD
Vol
ume
curr
ent (
Acm
-3)
Fluence (p/cm2)
309
366
Oxygenation shows normal improvement Leakage current looks the same in all samples.α~ 3E-17 A cm-1
0.0
50.0
100.0
150.0
200.0
250.0
0 10 20 30 40 50 60 70 80
94K FORW ARD BIAS - PAD DETECTOR
309p
309pd
x-ra
y pe
ak p
ositi
on (A
U)
Voltage (V)
309p Oxygenated309pd Oxygenated + Dimered
4 1014 24 GeV/c protons/cm2
Small improvement Small improvement –– do not expect anything spectaculardo not expect anything spectacularat this at this fluence fluence –– also a PAD detectoralso a PAD detector
5.0 1011
6.0 1011
7.0 1011
8.0 1011
9.0 1011
1.0 1012
1.1 1012
1.2 1012
1.3 1012
80 100 120 140 160 180
Nef
f [cm
-3]
T [K]
CONTROL OF THE SPACE CHARGECONTROL OF THE SPACE CHARGEWITH TEMPERATUREWITH TEMPERATURE
Phosphorus doping levelPhosphorus doping level
energy level occupancy ~ eenergy level occupancy ~ e-- ∆∆E/E/kTkT
MCA2us shapingX-ray source
detector
Li N
Temperature 85K to 300K
241Am
T [K]T [K]
NNef
f ef
f [c m[cm
-- 33]]
depleted
p+ n+
undepleted
X-RAY source
1x101x1014 14 n/cmn/cm2 2 > type inverted : > type inverted : --veve SCSC
CC DaDa ViaViaTo be publishedTo be published
++veve SCSC
0 .0
2 0 0 .0
4 0 0 .0
6 0 0 .0
8 0 0 .0
1 0 0 0 .0
1 2 0 0 .0
1 4 0 0 .0
1 6 0 0 .0
0 0 .0 0 5 0 .0 1 0 .0 1 5 0 .0 2 0 .0 2 5 0 .0 3 0 .0 3 5
1 2 0 K1 4 0 K1 6 0 K1 8 0 K
-E [V
/cm
]
D is ta n c e [ c m ]
ELECTRIC FIELD DISTRIBUTIONELECTRIC FIELD DISTRIBUTIONVERSUS TEMPERATURE AFTER 1E14 n/cmVERSUS TEMPERATURE AFTER 1E14 n/cm22
p+ n+
OXYGEN DIMERED SILICON OXYGEN DIMERED SILICON AFTER 24GeV/c PROTON IRRADIATIONAFTER 24GeV/c PROTON IRRADIATION
i
1.1x101.1x101111 p/cmp/cm22 4x104x1014 14 p/cmp/cm22
Radiation induced trapsRadiation induced trapsDLTS spectraDLTS spectra
SC after reverse annealingSC after reverse annealingMeasurements at 220K Measurements at 220K
-2.5 1011
-2 1011
-1.5 1011
-1 1011
-5 1010
0
5 1010
100 150 200 250 300
366p309p366Dp309Dp
Con
cent
ratio
n (c
m-3
)
Temperature (K)
E(90)E(170)
E(225)
~3y~3y50.0
100.0
150.0
200.0
250.0
300.0
0 200 400 600 800 1 103 1.2 10
309p366p366pd309pd
depl
eton
vol
tage
(V)
annealing time (min)
T=220
Anneal at 80 Anneal at 80 ooC C –– Equiv. to about 13 yr RTEquiv. to about 13 yr RT
Depletion voltages in various samples before and after annealing
Material VDep
300KVolts Note 1
VDep 223K ∆V RA
300KVolts Note 3
∆V RA
223KVolts Note 4
Standard 288 200 975 65
Oxygenated 189 100 740 40
Standard Dimered 288 90 - 0 to 10
OxygenatedDimered
180 100 - 40
Volts Note 2
Note 1: Inferred from CV measurement at room temperature Note 2: Inferred from x-ray count-rate measurement as function of voltage at 223K.Note 3: Calculated using Hamburg parameterisation of standard and oxygenated silicon.Note 4: Inferred from x-ray count-rate measurement as function of voltage.
TEMPERATURE DEPENDENCE OF DEPLETION VOLTAGE
Occupancy prop. Exp(∆E/kT)
SRH ∆E = Eg - 2ET
Inter-Centre Charge Transfer (ICT) ∆E = Eg - 2ET + ED
For V2 ∆E = -0.28 eV SRH, ∆E = -0.08 eV ICTEEgg
EETT
EETT
EEgg
EEDD
Temp. Dependence of RA part of depletion voltage = -0.2 eV
Temp. Dependence of Non -RA part of depletion voltageApprox -0.06 eV (depends on material )
CORRELATION BETWEEN RA - CLUSTER INTRO. RATE & TEMPDEPENDENCE OF DEPLETION VOLTAGE (PRIOR TO RA)
0
10
20
30
40
50
60
70
-0.1
-0.09
-0.08
-0.07
-0.06
-0.05
-0.04
-0.03
-0.02
0.8 1 1.2 1.4 1.6 1.8 2
Max
. Dep
letio
n V
olta
ge C
hang
e (V
olts
)
Activation E
nergy (eV) - S
ee Caption
Introduction Rate for E(225) DLTS Peak (cm -1)
SD
O & OD
S
ReverseReverseAnnealingAnnealing
BADBAD
GOODGOOD
Temp. Temp. DependenceDependenceof space chargeof space charge
Slow Slow VVdepchange with Tchange with T
FastFast VVdepdepchange with Tchange with T
Prior to RAPrior to RA
dep
CobaltCobalt--60 Irradiation Measure Minority Carrier Lifetime60 Irradiation Measure Minority Carrier LifetimeExpect VO to be important in standard Expect VO to be important in standard SiSi
3400
3600
3800
4000
4200
4400
4600
0 2 1013 4 1013 6 1013 8 1013 1 1014 1.2 1014
Minority Carrier Lifetime in differnt samples
1/tau S1/tau SD
1/ta
u (s
-1)
Fluence (gamma cm-2)
1Krad = 2.25E12 1Krad = 2.25E12 γγcmcm--22
1/1/ττ = 1/= 1/ττ00 + + φφ/K/Kττ
ττ00
KKττ
S S SDSD287287µµss 258258µµss
(1.0+/(1.0+/--0.1)0.1)*1E11*1E11
(2.0+/(2.0+/--0.2)0.2)*1E11*1E11
Units Units γγscmscm--22
Steps: 0, 15, 30, 45 Steps: 0, 15, 30, 45 KradKrad
Factor 2 better for standard Factor 2 better for standard dimered dimered siliconsilicon
VERY PRELIMINARY CONCLUSIONS VERY PRELIMINARY CONCLUSIONS FOR DIMER OXYGENATED SILICONFOR DIMER OXYGENATED SILICON
Evidence Evidence
•• That charge trapping has been improvedThat charge trapping has been improved•• That reverse annealing is suppressed in low [O] That reverse annealing is suppressed in low [O] dimered Sidimered Si•• Reverse annealing seems to be correlated with E(225) “cluster” Reverse annealing seems to be correlated with E(225) “cluster” peakpeak•• That space charge temperature dependence is different in low [OThat space charge temperature dependence is different in low [O] ] dimered Sidimered Si•• Temperature dependence of depletion voltage BEFORE RA correlatTemperature dependence of depletion voltage BEFORE RA correlated to theed to thesize of voltage change after RA !!!size of voltage change after RA !!!•• Better damage parameter for minority carrier lifetime in low [OBetter damage parameter for minority carrier lifetime in low [O] ] dimered Sidimered Siafter gamma irradiation.after gamma irradiation.
LOT OF THINGS TO DO YETLOT OF THINGS TO DO YET
NB: First look at how reverse annealing amplitude varies with teNB: First look at how reverse annealing amplitude varies with temperature.mperature.This may help to identify the defect causing RAThis may help to identify the defect causing RALots of possibilities Lots of possibilities OOii to Oto O2i2i to Oto O3i3i during processing. during processing. Low [O] and high [O] materialLow [O] and high [O] material