2005 EUVL SYMPOSIUM, SAN DIEGO CA, U.S.A Asia … · Asia Pacific Regional Update. 2005 . EUVL...
Transcript of 2005 EUVL SYMPOSIUM, SAN DIEGO CA, U.S.A Asia … · Asia Pacific Regional Update. 2005 . EUVL...
Asia Pacific Asia Pacific Regional Update
2005 2005 EUVL SYMPOSIUM, SAN DIEGO CA, U.S.AEUVL SYMPOSIUM, SAN DIEGO CA, U.S.A
Regional Update
EUVA/ASET (Japan)
Yasuhiro Horiike
(National Institute for Materials Science)
OutlineOutline1. Light source development
1.1 DPP (Discharge Produced Plasma)
1.2 LPP (Laser Produced Plasma)
2. Performances of polishing technologies using IBF (Ion Beam Figuring)
3. Advance in wavefront measurement system
4. Study on origin and control of contamination
5. EUVL process technology development
6. Development of SFET (Small Field Exposure Tool) and α tool
7. Present and future plan for Japan EUVL technology development
8. Summary
Low inductance DPP sourceLow inductance DPP sourceUnify discharge head and magnetic pulse compaction structure
Low inductance Peak current; 40kAPulse width; 140ns
DPP radiation
Xe gasSource power; 190W/2π
IF power:19W
For HVP source, Sn fuel is now being developingMagnetic pulse
compaction
Condenser
Charging terminal
Magnetic core
Conventional
Magnetic compactionstage
High inductance
Electrode
Magnetic coreTansmission
line
Condenser
Insulator Plasma
Low inductance
50kW, 7kHz pulseCompaction type
power source
Debris mitigation of focusing mirror for DPPDebris mitigation of focusing mirror for DPPMirror specimen: Ru/Si
0.00
0.20
0.40
0.60
0.80
1.00
1.20
without debris shield
gas curtain only
gas curtain+foil trap
Relative variation of mirror reflectivity in exposure experiment
type : Ugic-03
20 deg.
30 deg.
20 deg.Aperture
Discharge head
SourceDetector-1
Foil trap
外側ミラー 内側ミラー
Type; Ugic-03N
orm
aliz
ed in
tens
ity ra
tio
Shot number(×106)0 2 4 6 8 10
Gas curtain alone
Gas curtain + Foil trap
Without debris mitigation
The experiment at 107
shots was stopped
Detector-2
Foil trap
Ultrasonic gas curtain
発光点集光点
外側ミラー内側ミラー
スパイダー(ミラー保持)
Source IF
OutsideInside
Spider mirror hold)
Ultrasonic gas curtain
Focusing characteristics at IF planeFocusing characteristics at IF plane
Figure of light source more than 120nm
Distribution of light more than 120nm
Grazing angle incident correctorIntermediate
focus (IF) plane
Distribution of EUV light
Out of band wavelength light does not focus at the IF plane due to lager size of the source point
120-400nm: 3.5%400-750nm: 0.16%750nm> : 0.13%
For in-band EUV light
SnSn source by SnHsource by SnH44 ((StannanStannan) discharge) discharge7kHz pulsed power generator
Stannane supply unit
DPP source chamber
1/e2 size : 1.16 x 10.0
Plasma image (20 deg.)
Stannane (SnH4) fuel :
・ Demonstrated source power➪ 397W /2π at 7kHz
・ Estimated usable IF power➪ 33W /3.3mm2sr
with πsr collectorCalculated focus image
Primary source power
Electrode edge
19.03.4
396.7
205.3
0
50
100
150
200
250
300
350
400
450
0 1 2 3 4 5 6 7 8Pulse repetition rate (kHz)
In-b
and
radi
atio
n po
wer
(W/2
PIsr
) fuel feed rate : fixed
LPP: Efforts to 10W@IF with pulse amp. by RFLPP: Efforts to 10W@IF with pulse amp. by RF--COCO22
Amplification: 3.6 times2.9 timesShort pulse oscillator
100WPre amp.
5kWMain amp.
15kW0.15kW 0.69kW 7.4kW
Pre amp.5kW
2kWMulti-line seeder System:Jan. 2006
>10W@I/F
Multi -lineseed light
Generation of multi-Line seed light
4 lines oscillate
Collaboration with Max Born Institute
Xe Jet
YAG
200nsec
EUV
Plasma
CO2
4.6 times
CO2-8x1010W/cm2 C.E.; 0.6%
Xe droplet plasma
Li target experiment by Miyazaki university demonstrated that double pulses irradiation decreased greatly energy of ions generated from Li plasma
A variety of mass limit targets for debris mitigationA variety of mass limit targets for debris mitigation
Droplets
Cylindrical jet
Plane
laser
Heated Debris region
Source
Plasma Foam shell
Punch-out target(ILE and ILT)
Transparent substrate
Density: 0.5 g/cc (7% of Bulk)
2mm
200µm
Hollow jet(U. of Hyogo)
Punch-outlaser
Sn jet > 500 m/s
1 mmHeat laser
Heater pulse
Ion beam figuring (IBF) for LSFRIon beam figuring (IBF) for LSFR
Panorama of equipment
凸部分
加工点
イオンガン
Ion gun chamber
Load rock chamber
Zerodurinput
Small tool
IBF
Result
0.247nm rms
0.139nm rms
ApertureIon beam
Ion gun
Aspheric surface
5 axes numerical controlled stage
Ion beam
Ion gun
Zerodur
Kaufman type ⇒RF type
11mmmm2 2 areaarea IBF for waviness eliminationIBF for waviness elimination
X
Y
Z
MirrorIon gun
(3axes tilt)
Before: 0.359nm rms
After: 0.132nm rms
Long term excellent stabilityVariation;±1.4%
φ40mm
0.5 mm
Vacuum chamber
Stage
Work holding
EB・IB gun
Interferometer for Interferometer for asphericalaspherical mirror surfacemirror surface
Null lens generating aspherical wave front
Mirror to be measured
Reference lens
Visible light laser
CCD camera
0.00
0.02
0.04
0.06
0.08
0.10
0 200 400 600 800 1000Number of averaging
phase data × Number of avaraging
intensity data
Rep
eata
bilty
(nm
rms) Asphrical mirror (05/03/23)
Asphrical mirror (05/05/25)
0 50 100 150
mm
0 50 100 150
mm
0 50 100 150
mm
Cross sectionBird’s-eye view
Goal of repeatability50pm rms
Pase averaging x intensity averaging Reatability:0.032nm rms
Wavefront measurement system for 6 mirrors optics
LSI (Lateral Shearing Interferometer)PDI (Point Diffraction Interferometer)
3.5m
Observation camera
Stage mechanism for wafer sideStage mechanism for wafer side
Connected to Hygo prefecture Univ.”New Subaru” SR beam line
6 mirrors optics
August, 2006
Measurement system has been established
LDI (Line Diffraction Interferometer)CG-LSI (Cross-Grating Lateral
Shearing Interferometer)
Chamber vacuum, leticle & wafer stages are now completed
Contamination control technologiesContamination control technologies
a) Protection for contamination
a-2) Surface evaluation a-1) Attachment and oxidation
b) Capping layerb-1) Screening of materialsb-2) Film structure and deposition
c) Elimination of contamination c-1) Carbon elimination ratec-2) Surface damage
d) Difference between pulse and CW lights
d-1) Experimental toold-2) Contamination evaluation
New chamber (small HC) Old chamber (High HC)
XPS測定部
X / mm
XPS測定部
X / mm
0.99
0.97
0.95
9.0 9.5 10.0 10.5 11.019.0
19.5
20.0
20.5
21.0
Z / m
m
0.930.950.970.991.01
1.000.98
0.980.96
0.96
0.96
-1.0 -0.5 0.0 0.5 1.0-1.0
-0.5
0.0
0.5
1.0
0.940.960.981.001.01
R / R
0
SiOxRuOx
The new chamber with low hydro-carbon (HC) showed considerable oxidation at irradiated region, but the old one with high HC supressed oxidation
The new chamber with low hydro-carbon (HC) showed considerable oxidation at irradiated region, but the old one with high HC supressed oxidation
SR light irradiation to Ru(2nm)/Si/Mo multi-layer and XPS and reflectivity measurement
0.0E+002.0E-054.0E-056.0E-058.0E-051.0E-041.2E-041.4E-041.6E-041.8E-04
1.E-06 1.E-04 1.E-02Rel
ativ
e re
flect
ivity
(k)
Ru(NTT)Ru(UH)
H2O partial pressure (Pa)
k=b・ln(水分圧)+c
Decrease in refractivity against water partial pressure can be estimated
Cha
nge
in re
frec
tivity
0.97
0.98
0.99
1.00
1.01
0 50 100 150 200 250 300Dose (J/mm2)
Ru(4)Ru(2)Ru(3)Ru(0)Ru(1)
Choice of Ru deposition condition improves anti-oxidation
Research items
Atomic Hydrogen Cleaning of carbon and Atomic Hydrogen Cleaning of carbon and RuRu oxideoxide1
4
7
10
13
16
19 X [mm]
Y4 [mm]
Y2.5 [mm]
Y1 [mm]
Y-0.5 [mm]
Y-2 [mm]
0.010.020.030.040.050.060.070.0
60.0 -70.0
50.0 -60.0
40.0 -50.0
30.0 -40.0
20.0 -30.0
10.0 -20.0
0.0 -10.0
1
5
9
13
17
21
S1
S5
S9
S130.010.020.030.040.050.060.070.0
60.0 -70.0
50.0 -60.0
40.0 -50.0
30.0 -40.0
20.0 -30.0
10.0 -20.0
0.0 -10.0
Carbon cleaning Ru oxide reduction
Binding Energy (eV) Binding Energy (eV)
Ru Oxide
Hot-wire apparatus
Carbon contamination was removed, and reflectivity-loss was recovered almost completely by atomic hydrogen.Ru oxide formed on Ru surface was reduced to metallic Ru by atomic hydrogen treatment.
EUV Process Technology
Resist Exposure with Resist Exposure with HiNAHiNA SetSet--33
Nov.8 8:20, Oizumi, EUVL Symposium 2005
Mask holderIllumination Optics
Projection OpticsWafer Stage
Set-3 optics was installed to HiNA exposure tool at August 2004 in Atsugi Lab.28 nm l/s pattern was replicated using chemically amplified resist.
28-nm L/S35-nm half pitch40-nm hp 30-nm L/S
EUV Process Technology
EUVL Mask FabricationEUVL Mask Fabrication
TaGeN based Mask fabrication process was established in collaboration with DNP.Non printability of AFM-repaired pattern defect was demonstrated.
Example of EUVL mask
19 nm L/S@wafer 25 nm L/S@waferFine pattern fabrication
Program defect Repaired pattern Printed ImagePrintability test of defect repairing
TaGeN
Cr
Etch Profile
EUV Process Technology
SFET (Small Field Exposure Tool) developmentSFET (Small Field Exposure Tool) development
0.11nm rms
0.10 nm rms
Xe recycle system
TMPXe flow
MirrorXe jet
IF
KrF excimer laserWavelength:248nmPower:320WPulse energy:80mJRepetition:4kHz
SFET
Goal:①Verification of source and polishing technologies developed by EUVA
②Resist process development for hp45-32nm
③Evaluation of mask blank defect , etcSpecification: 2 mirrors aspherical mirrors、
NA=0.3、0.5W source、Exposure area of 200×600μm2, Flare less than 7%
SFET mock up
25mm
70mm
M2 mirror (Zerodur)
Leticlestage
Wafer stage
Optics
EUV chamber
June, 2006
Full Field Exposure Tool (EUV1)Full Field Exposure Tool (EUV1)Main Specification
- Field size; 26x33mm- NA; 0.25- Magnification; 1/4 - Flare; less than equal to 10%- Through put; 5-10w/h@300mmΦ- Source type; DPP, 10W@IF
Delivery date- 1H/2007
Current Status- System and Module design: completed- Source: manufacturing by supplier- Projection Optics: proto-typing- Tools for mirror metrology: completed- Stages/Body: start manufacturing
PO boxProto-type
PO mirror M1
Present & future plan for EUVL technology developmentPresent & future plan for EUVL technology development
EUV12002 2003 2004 2005 2006 2007 2008 2009 2010FY
Source
Tool
SFET
α β HVM
(Basic technology development)
2011
Resist process
Module process
SFET
EUVA end hp45nmHVM
Polishing
100W/Sn
50W/Xe/Sn
Tsukuba R&Dcenter
LPP0.5W/Xe
DPP10W/Xe
Evaluation
MXST LPP project
Technology transfer
EUVA
Independent R&D by companies
SummarySummary 1. Japan EUVL technologies advance steadily for source, tool and
process and are now expected as a key lithography for hp45-32 nm LSI devices.
2. DPP source has been developed greatly as a light system and SnH4gas will provide a hopeful source for HVM based on our original debris mitigation technology.
3. Although delay of LPP development depends on CO2 driver laser, 10W IF power will be achieved within two months. Ion mitigation by high magnetic field design and physics & a lot of useful resultsobtained by MEXT LPP projects will realize HVM LPP source.
4. Basic technologies for EUV tool is also developed steadily and SFET and α tool will appear June, 2006 and first half, 2007, respectively.
5. We believe that the EUVL technologies does not only develop the LSI devices moreover, but also offer nano/pico technologies further prosperity of human beings.
AcknowledgementAcknowledgementThe presenter would like to express deep thanks for researchers from EUVA, ASET and Leading Project of MEXT (Ministry of education, sports, culture, science and technology) and financial supports by NEDO (New Energy and Industrial Technology Development Organization) and MEXT.