8:30 – 9:00 research and educational objectives / spanos
DESCRIPTION
3rd Annual SFR Workshop, November 8, 2000. 8:30 – 9:00 Research and Educational Objectives / Spanos 9:00 – 9:50 Plasma, Diffusion / Graves, Lieberman, Cheung, Haller 9:50 – 10:10 break 10:10 – 11:00 Lithography / Spanos, Neureuther, Bokor - PowerPoint PPT PresentationTRANSCRIPT
8:30 – 9:00 Research and Educational Objectives / Spanos
9:00 – 9:50 Plasma, Diffusion / Graves, Lieberman, Cheung, Haller
9:50 – 10:10 break10:10 – 11:00 Lithography / Spanos, Neureuther, Bokor 11:00 – 11:50 Sensors & Metrology / Aydil, Poolla, Smith, Dunn
12:00 – 1:00 lunch 1:00 – 1:50 CMP / 1:00 – 1:50 CMP / Dornfeld, Talbot, SpanosDornfeld, Talbot, Spanos
1:50 – 2:40 Integration and Control / Poolla, Spanos
2:40 – 4:30 Poster Session and Discussion, 411, 611, 651 Soda 3:30 – 4:30 Steering Committee Meeting in room 373 Soda 4:30 – 5:30 Feedback Session
3rd Annual SFR Workshop, November 8, 2000
11/8/2000
2
Chemical Mechanical Planarization
SFR Workshop
November 8, 2000
Andrew Chang, Tiger Chang, David Dornfeld, Tanuja Gopal, Edward I. Hwang, Jianfeng Luo, Zhoujie Mao, Costas Spanos,
Jan Talbot
Berkeley, CA
11/8/2000
3
CMP Milestones
• September 30th, 2001– Build integrated CMP model for basic mechanical and chemical
elements. Develop periodic grating metrology (Dornfeld, Talbot, Spanos).
• September 30th, 2002– Integrate initial chemical models into basic CMP model. Validate
predicted pattern development. (Dornfeld, Talbot) .
• September 30th, 2003– Develop comprehensive chemical and mechanical model. Perform
experimental and metrological validation. (Dornfeld, Talbot, Spanos)
11/8/2000
4
Abstract2001 Milestone: Build integrated CMP model for basic
mechanical and chemical elements. Develop periodic grating metrology
Key elements involved in this are:– Chemical Aspects of CMP (J. Talbot and T.Gopal)– Particle Size Distribution in CMP: Modeling and Verification (J.
Luo) – Slurry Flow Analysis and Integrated CMP Model (Z. Mao)– Scratch Testing of Silicon Wafers for Surface Characterization (E.
Hwang)– Process Monitoring of CMP using Acoustic Emission (A. Chang)– Development of periodic grating metrology (C. Spanos and T.
Chang)
We will review the recent activities in these areas
11/8/2000
5
OverviewModel Structure & Development Basic
Process Mechanism
Model Validation
Metrology, Process Control, &
OptimizationChem Mech
Chemical Aspects (JT/TG)
X X X
Particle Size Distribution (JL)
X X X
Slurry Flow (ZM) X X XSurface Effects (EH) XProcess Monitoring (AC)
X X
Grating Metrology (CS/TC)
X
Process control(KP) X
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Contact Pressure
ModelModel of
Active Abrasive
Number N
Model of Material
Removal VOL
by a Single Abrasive
Physical Mechanism; MRR: N´VOL
Slurry Concentration,
Abrasive Shape, Density,
Size and Distribution
Slurry Chemicals
Chemical Reaction
Model (RR0)chem
Pad Roughness
Pad Hardness
Wafer, Pattern,Pad and
Polishing Head Geometry
and Material
Pressure and Velocity
Distribution Model
(FEA and Dynamics)
Down Pressure
Relative Velocity
Wafer Hardness
Dishing &
Erosion
Preston’s Coefficient Ke (RR0 )mech
WIWNUSurface
Damage WIDNU
WIWNU
MRR
Fluid Model
Overview of Integrated Model
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7
Chemical Aspects of CMP Role of Chemistry - Tanuja Gopal, Jan Talbot UCSD
• Chemical and electrochemical reactions between material (metal, glass) and constituents of the slurry (oxidizers, complexing agents, pH) – Dissolution and passivation
• Solubility• Adsorption of dissolved species on the abrasive
particles• Colloidal effects• Change of mechanical properties by diffusion &
reaction of surface
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8
Mass Transfer Processes• (a) movement of solvent
into the surface layer under load imposed by abrasive particle
• (b) surface dissolution under load
• (c) adsorption of dissolution products onto abrasive particle surface
• (d) re-adsorption of dissolution products
• (e) surface dissolution without a load
Ref. L. M. Cook, J. Non-Crystalline Solids, 120, 152 (1990).
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Reaction Chemistries
• Dissolution of glass
(SiO2)x + 2H2O = (SiO2 )x-1 + Si(OH)4R+(glass) + H2O = H+(glass) + ROH
W + 6Fe(CN)6-3 + 4H2O WO4
-2 + 6Fe(CN)6-4 + 8H+
W + 6Fe(CN)6-3 + 3H2O WO3 + 6Fe(CN)6
-4 + 6H+
• Dissolution and passivation of W
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Generic Chemical Reactions
• Dissolution: M(s) + A > M(aq) + B M(s) + A > Mn+ + ne-
+ B
• Oxidation: M(s) + O >M-oxide(s)
• Oxide dissolution: M-oxide(s) + A > M(aq) + B
M-oxide(s) + A > Mn+ + ne- + B• Complexation (to enhance solubility)
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Colloidal Effects
• Surface charge (zeta potential or isoelectric point, IEP, the pH where the surface charge is
neutral) of polished surface and abrasive particle is important
(Malik et al.)
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Colloidal effects
• Maximum polishing rates for glass observed compound IEP ~ solution pH > surface IEP(Cook, 1990)
• Polishing rate dependent upon colloidal particle - W in KIO3 slurries (Stein et al., J. Electrochem. Soc. 1999)
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Experimental Program
• Electrochemical/chemical experiments with rotating disk electrode with and without abrasion
• Measurement of zeta potential of abrasives as function of pH (IEP) and solution chemistry
RDE
CounterElectrode
Reference Electrode
Polishing Pad
Potentiostat
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Modeling of Chemical Effects
• Electrochemical/chemical dissolution and passivation of surface constituents
• Colloidal effects (adsorption of dissolved surface to particles or re-adsorption)
• Solubility changes • Change of mechanical properties (hardness, stress)
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Contact Pressure
ModelModel of
Active Abrasive
Number N
Model of Material
Removal VOL
by a Single Abrasive
Physical Mechanism; MRR: N´VOL
Slurry Concentration,
Abrasive Shape, Density,
Size and Distribution
Slurry Chemicals
Chemical Reaction
Model (RR0)chem
Pad Roughness
Pad Hardness
Wafer, Pattern,Pad and
Polishing Head Geometry
and Material
Pressure and Velocity
Distribution Model
(FEA and Dynamics)
Down Pressure
Relative Velocity
Wafer Hardness
Dishing &
Erosion
Preston’s Coefficient Ke (RR0 )mech
WIWNUSurface
Damage WIDNU
WIWNU
MRR
Fluid Model
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Synergistic Effects
• MRR = kchem (RRmech)o + kmech (RRchem)o
(RRmech)o = mechanical wear = Ke PV (RRchem)o = chem. dissolution = kr exp(-E/RT)Ci
n
Ke affected by surface chemical modification Ci affected by mass transport (i.e., V)
Ref.: Y. Gokis & R. Kistler, ECS Meeting Abstract 496, Phoenix, Oct. 2000.
11/8/2000
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Potential Results for Chemical MP Modeling
• Selective chemical slurries:1) control reaction chemistry 2) control colloidal properties of abrasives and removed material3) enhance solubility of removed material
• Material wear properties (eg, hardness)
• Chemically active pads
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Chemical Effects of CMP
• Synergistically enhances the rate of material removal with mechanical polishing
• Influences the colloidal stability of the abrasive particles
• Undesired effects are unwanted etching and dishing of features and increased surface roughness
DishingErosion
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Effect of Particle Size Distribution in CMP Modeling Abrasive Geometry and Size - J. Luo UCB
Two Abrasive Geometries
• Spherical Shape for Obtuse Abrasives• Conical Shape for Sharp Abrasives
0
10
20
30
40
50
60
-8 -6 -4 -2 0 2 4 6 8
Xavg
y
SEM Picture of Slurry Abrasives for Si CMP (Moon, PhD Thesis, 1999)
Abrasive Size and Size Distribution
• Nano-Scale Size X• Normal Distribution (Xavg , ) and p((Xavg , )
• Xavg, Xmax and Standard Deviation
Schematic of Spherical and Conical Abrasive Shapes in the Model
X
100nm
Schematic of Abrasive Size Distribution
X
Portion of Active Abrasive
Xmax
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V = Vol
a12= F2/Hw
1
Chemical Reaction
Schematic of Wafer-Chemical-Abrasive-Pad Interaction to
Model the Volume Removed by A Single Abrasive
Contact Mechanics( Pad Topography/Abrasive Size/Pressure )
Ab
rasi
ve
Ge
om
etr
y
a22= F2/Hp
Xmax-Y=2
Abrasive Geometry
Pad Hardness
Schematic of Wafer-Abrasive-Pad Interaction to Model the Number of Active Abrasive Number
Contact Mechanics( Pad Topography/Abrasive Size/Pressure )
Ab
rasi
ve S
ize
D
istr
ibu
tion N
Material Removal Rate Function:MRR= N Vol= C1Hw
-3/2 {1-(1-
C2P01/3}P0
1/2V. Correct on both average scale &
local single points
Role of Abrasive Size in the Architecture of the Integrated CMP
Model
Detailed Fluid Model
?
-40-30
-20-10
010
2030
40
-7000-6000-5000
-4000
-3000
-2000
-1000
0
1000
2000
3000
4000
5000
6000
7000
8000
-40
-30-20
-100
1020
3040
Z A
xis
(A)
Y Axis
(mm
)
X Axis (mm)
Pressure and velocity distribution over wafer-
scale
Pattern Density
Surface Damage
Slurry pH Value and so on
WIWNU
WIDNUn
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21
MRR As A Function of Particle Size Distribution Before Saturation (Luo & Dornfeld, 2000)
2
4
4
433
33
33
331
avg
avg
avgavg
avgX
C
XCp
XX
CX
C
Contribution of Active Particle
Number
Contribution of Total Number of Particles over the
Wafer-Pad Interface
MRR=MRR as A Function of Down Pressure and Velocity: MRR= N Vol= C1Hw
-3/2 {1-(1-C2P01/3}P0
1/2V.
MRR as A Function of Particle Size and Size Distribution
C3: A Function of Down Pressure, Velocity, Weight Concentration etc.C4: 0.25(4/3)2/3(1/Hp)Ep
2/3/b1P01/3 A
Function of Down Pressure, Pad Hardness and Pad Topography.
Function p: The probability of the appearance of abrasive sizeFunction : Probability density function.
Contribution of Active Particle
Size (Larger than Xavg)
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22
Particle Size Distribution Measurement (II)
Dynamical Light Scattering
0.2887680.88AA07
0.2106330.60AKP15
1.0561972.00AA2
0.1189590.38AKP30
0.0702220.29AKP50
Standard Deviation (m)
Mean Size (m)
*Bielmann et. al. 1999
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y = 325.1x-0.6411
y = 314.77x-0.6695
0
100
200
300
400
500
600
700
800
0 0.5 1 1.5 2 2.5
Particle Size (10-6m)
Mate
rial R
em
oval R
ate
(nm
/min
)
Experimental Mean MRR
Prediction of the Model
Power (Experimental Mean MRR)
Power (Prediction of the Model)
Particle Size Dependence on MRR: Experiment VS. Model Predictions
C4: 0.25(4/3)2/3(1/Hp)Ep2/3/b1P0
1/3= 0.015
(0.29, 0.07022)
(0.38, 0.118959)
(0.60, 0.210633)
(0.88, 0.288768)
(2.0, 1.056197)
* Bielmann et. al. 1999
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Fraction of Active Particles Based on Model Prediction
[0.726, 0.737m] 0.1827%
[1.213, 1.231m] 0.1798%
[1.720, 1.746m] 0.1815%
[5.091, 5.169m] 0.1719%
[0.49, 0.50m] 0.19105%
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25
0
0.2
0.4
0.6
0.8
1
1.2
1.4
1.6
1.8
2
0 0.05 0.1 0.15 0.2 0.25 0.3
Standard Deviation (10-6m)
Nor
mal
ized
Mat
eria
l R
emov
al R
ate Xavg= 0.29um
Xavg=0.38um
Xavg=0.60um
Xavg=0.88um
Xavg=2um
Relationship between Standard Deviation and MRR Based on Model Prediction
Size Dominant Region
Number Dominant Region
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Wafer
Down Pressure
H
H
a
Smaller contact area
Larger contact area
2002 & 2003 GoalsDevelop comprehensive chemical and mechanical model. Perform experimental and metrological validation, by 9/30/2003.
11/8/2000
27
Slurry Flow Analysis and Integrated CMP Model Zhoujie Mao UCB
Motivation
• Study the effects of slurry flow on the material removal in CMP
• Develop integrated process model for CMP to provide insight into the MRR and WIWNU
• Develop process model for environmental impact analysis for CMP
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Overall Picture of Slurry Flow in CMP
Side view
Polishing plate
Polishing pad
Wafer
Carrier film
Carrier Slurry Slurry feeder
• Two flow stages: slurry flow on the polishing pad, slurry flow between wafer and polishing pad
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Slurry Flow on the pad
Polishing pad
Slurry
Abrasive particle
• Estimate the abrasive particle settling mechanism on the polishing pad
• Study the effects of slurry supply rate and slurry delivery position on the material removal rate
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Abrasive Particle Settling Rate Vs. Slurry Supply Rate
0 20 40 60 80 100 120 140 160 180 2000
1
2
3
4
5
6
7
8x 10
15
Radius (mm)
Ra
te o
f d
ep
os
itio
n (
n/m2 /s
ec
)
Q=50ml/min Q=100ml/minQ=150ml/min
Radius (mm)
Rat
e of
Dep
osit
ion
(n/m
2 /s)
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31
Abrasive Particle Settling Rate Vs. Delivery Position
100 120 140 160 180 200 220 240 260 280 3001
2
3
4
5
6
7
8x 10
16 Average Settling Rate Underneath Wafer
Raidial Position (mm)
Av
era
ge
Se
ttlin
g R
ate
(n
/m2 /s)
e=0mm e=100mme=200mm
Eccentricity
Average Settling Rate Beneath Wafer
Ave
rage
Set
tlin
g R
ate
(n/m
2 /s)
Radial Position (mm)
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32
Integrated Slurry Flow Model
• Slurry flow between wafer and polishing pad• Slurry flow inside polishing pad• Deformation of wafer• Deformation of polishing pad
h(x)
Pad
hp(x)
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33
2002 & 2003 Goals
Develop comprehensive chemical and mechanical model. Perform experimental and metrological validation, by 9/30/2003.
•Simulation of Integrated CMP model
•Experimental verification of integrated CMP model (role of active abrasives in mechanical material removal)
11/8/2000
34
Scratch Testing of Silicon Wafers for Surface Characterization
Edward Hwang UCB
Motivation
• Wafer surface characterization is important to understand and model the material removal mechanism in CMP
- Scratch testing supports the identification and verification of surface characteristics of the wafer representative of the CMP process
- Scratch testing can give insight on the stress levels occurring during the CMP Process
11/8/2000
35
Actual CMP Situations
Cross Section View
polishing pad
Si wafer
bulk
not affected by the process
layer 1(order of a few nm )
highly hydrated, loosely bound network
– lower densityTrogolo et al “Near Surface Modification of Silica Structure Induced by Chemical/Mechanical Polishing”, J. Materials Science 29 (1994) pp. 4554 - 4558
layer 2(order of 20 nm )
plastically compressed network
– higher density
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Experimental Setup
•Workpiece: Silicon wafer <100> p-typePre-CMP Wafers & Post-CMP Wafers
• Diamond tool: Nose radius: 48μm• Feed rate: V=399μm/s• Tilt angles: 0.06 degrees.• Acoustic emission sensor: DECI Pico-Z AE sensor• Data collection: 50kHz sampling rate
11/8/2000
37
Layers vs. AE Signals (1)
Pre-CMP Wafers
0.00 0.05 0.10 0.15 0.20 0.25 0.30 0.35-1.0
-0.8
-0.6
-0.4
-0.2
0.0
0.2
0.4
0.6
0.8
1.0
AE
sig
nal
s (v
olt
s)
time(s)
AE signals are proportional to the depth of cut in
11/8/2000
38
Layers vs. AE Signals (2)
Post-CMP Wafers
0.35
0.00 0.05 0.10 0.15 0.20 0.25 0.30-1.0
-0.8
-0.6
-0.4
-0.2
0.0
0.2
0.4
0.6
0.8
1.0
time(s)
AE
Raw
Sig
nal
s (v
olt
s)
Air-cut + Layer 1
Layer 2 Bulk
Unlike the pre-CMP wafers, post-CMP wafers show discontinuous transitions in the AE signal due to penetration of Layer 2.
11/8/2000
39
Results
• Observation of distinct signal changes for transitions between Layer 1 Layer 2 bulk supports surface characterization
• Signal for Layer 2 is observed up to 20 nm depth of cut• Highly compressed Layer 2 is more ductile than bulk :
- Plastic deformation dominates the material removal mechanism in this regime and should relate to removal rate during CMP
• SEM images support the verification of the multi-layered wafer surface
11/8/2000
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2002 & 2003 Goals
• Replicate the scratch testing with AFM machine in order to be closer to actual CMP situations
• Quantify the wafer surface characteristics in CMP
Develop comprehensive chemical and mechanical model. Perform experimental and metrological validation, by 9/30/2003.
11/8/2000
41
Process Monitoring of CMP using Acoustic EmissionAndrew Chang UCB
Motivation
• AE monitoring is an applicable diagnostic tool for studying abrasive interaction during CMP
• Experimental verification for abrasive particle interaction is needed for CMP modeling
• Alternative sensing methods are in-direct (motor current, pad temperature, etc.) or limited to localized areas of the wafer
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42
Acoustic Emission Sources in CMP
• Acoustic emission is highly sensitive to abrasive particle interaction between wafer and pad
11/8/2000
43
Experimental Setup
PC Data Acquisition Pre-amplifier(60 dB)
Amplifier(40 dB)RMS Filter
Raw Sampling Rate = 2 MHzRMS Sampling Rate = 5 kHz
RMS AE
Raw AEAE Transducer
Wafer
Pressure = ~ 1 psiTable Speed = 20 – 80 RPMSlurry flowrate = 150 ml/min
Polishing Conditions
IC 1000/Suba IV stacked padPad type
ILD 1300, abrasive size (~100 nm)W-Slurry, abrasive size (~37 nm)Alumina slurry, abrasive size (~100 nm)
Slurry type
Oxide, aluminum, tungsten, copper blanket wafersTest Wafers
Toyoda Float Polishing MachineCMP Tool
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44
AE Ratio Signal ProcessingHFpeak
t
ASL
LFpeak
t
High Pass Filter>100 kHz
Ratio = HFpeak
LFpeakLow Pass Filter20-60 kHz
ASL
Raw AE Signal
AE Ratio for Oxide Wafer
0.5
0.7
0.9
1.1
1.3
1.5
1.7
0 20 40 60 80 100Table RPM
HF
/LF
Rat
io
Oxide-DIW
Oxide-Slurry
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45
AE Signal for Varied Materials
High Frequency Average Signal Level during CMP Polishing
0
1000
2000
3000
4000
0 20 40 60 80 100
Table RPM
AE
AS
L (
mV
)
BackgroundNoise
Oxide
Aluminum
Tungsten
Copper
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AE Ratio for Oxide Polishing
0.35
0.4
0.45
0.5
0.55
0.6
0.65
0 50 100 150 200
Time (sec)
AE
Ra
tio
Oxide begins to clear
Oxide cleared
Application to Endpoint Detection• The sensitivity of acoustic emission to various materials
during polishing is ideal for endpoint detection in CMP
Oxide Wafer
Pad
Pad
Pad
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Sensitivity to CMP Process
• Background noise characterization• AE is insensitive to low-frequency (audible) noise from CMP
tool (motors, belts, etc.)
• Sensor location (backside of wafer is ideal) isolates signal from process and filters noise
• Signal from process is sensitive to abrasive particle interaction
• Signal comparison between deionized water and abrasive slurry
• Sensitivity to different materials
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2002 & 2003 Goals
Develop comprehensive chemical and mechanical model. Perform experimental and metrological validation, by 9/30/2003.
•Future tests planned with industrial CMP tool manufacturer
•Further experimental tests for validation of integrated CMP model (role of active abrasives in mechanical material removal)
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49
Pattern density mask - MIT 96.4
Feature size 10 mDie size 20mm by 20mmPattern density ranges from 4% to 100%
Establishing full-profile metrology for CMP modelingCostas Spanos & Tiger Chang UCB
11/8/2000
50
Process Flow
The final structure
Get the mask files
Design contact mask
Make emulsion mask
Aluminum 0.7 m
PECVD oxide ~2m
CMP
PSG deposition 1 m
Pattern Aluminum
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Results of Experiment (typical)
0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 13000
3500
4000
4500
5000
5500
6000
6500
7000
effective Pattern Density
Oxi
de
Re
mo
val R
ate
A/3
min
ute
sWafer #2 r=0.9807 PL=2.450mm
The characteristic length is about 2~3mm; this motivates a new mask design
11/8/2000
52
New Mask Design
• The size of the metrology cell is 250m by 250m
• 2m pitch with 50% pattern density
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53
Key ideas
SubstrateOxide
• Use Scatterometry to monitor the profile evolution• The results can be used for better CMP modeling
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54
Current status
• Done mask design and processing in the Lab, 12 wafers are ready to polish
• Before the characterization experiments, we want to know – Is the scatterometer signal sensitive enough for the profile
evolution?• Simulated a conceptual profile evolution
– How does the initial profile look like?• LEO can give a cross section SEM view (we need to cut the
wafer, then can’t do CMP on this wafer anymore!)
• AFM can give a smooth profile (it needs reliable de-convolution)
11/8/2000
55
CMP Profile evolution used in GTK simulation
0 500 1000 1500 20000
0.05
0.1
0.15
0.2
0.25
0.3
0.35
0.4
0.45
0.5Profile Evolution during CMP
Oxide (nm)
pro
file
(m
icro
n)
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56
GTK Metrology Simulation Results
• We simulated 1 m feature size, 2 m pitch and 500nm initial step height, as it polishes.
• The simulation shows that the response difference was fairly strong and detectable.
Tan PSI Response to Profile Evolution
0
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
240
280
320
360
400
440
480
520
560
600
640
680
720
760
Wavelength(nm)
tan
PS
I
tan PSI 500nm
tan PSI 400nm
tan PSI 300nm
tan PSI 200nm
tan PSI 100nm
tan PSI Flat Surface
Cos DEL Response to Profile Evolution
-1.5
-1
-0.5
0
0.5
1
1.5
240
280
320
360
400
440
480
520
560
600
640
680
720
760
Wavelength(nm)
cos
DE
L
cos DEL 500nm
cos DEL 400nm
cos DEL 300nm
cos DEL 200nm
cos DEL 100nm
cos DEL Flat Surface
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Immediate Metrology Objectives
• Do measurements using Sopra for the initial structures, compare results with the AFM measurements
• Build a pseudo response library• Design experiments, polish finished wafers and do
scatterometry measurements• AFM measurements at AMD, refine the library
11/8/2000
59
Conclusions
• Chemical effects model and synergy with mechanical effects being developed
• Integrated model validated for abrasive size and activity• Fluid modeling of particle behavior corroborates abrasive
activity• Extent and behavior of surface modified layer being
characterized• Sensing system for process monitoring and basic process
studies being validated• Scatterometry metrology sensitivity study indicates suitability
for observing profile evolution