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![Page 1: Sapphire Test Masses ACIGA/UWA High lights of research at UWA Alternative approach to suspensions High power test facility Cryogenic applications Mark.](https://reader035.fdocuments.us/reader035/viewer/2022062719/56649ee75503460f94bf8828/html5/thumbnails/1.jpg)
Sapphire Test MassesACIGA/UWA
•High lights of research at UWA
•Alternative approach to suspensions
•High power test facility
•Cryogenic applications
Mark Baker*,Fetah Benabid*, David Blair Ju Li Darren PagetMitsuru Taniwaki*Colin Taylor
LIGO-G010166-00-Z
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Summary of work in UWA (ACIGA) on Sapphire
in collaboration withLIGO: B. Barish, S. Witcomb, D. Reitze, A. Alexandrovski
VIRGO: J. Mackowski, A. Brillet, C. Man, F. Bondu, F. Cleva, V. Loriette, C. Boccara
Year system results Ref
1996 Thermal expansion CryogenicSapphire cavity =210-10 (5K)
IEEE Trans.Instrum. Meas.46, 188 (1997)
1996 AbsorptionVIRGO, Paris
3ppm/cm (one sample)20-50ppm/cm typical
Opt. Mat.8, 233 (1997)
1997 Sapphire mirrorsCSIRO, polishingVIRGO, Lyon, coating
Roughness < 0.1nm;Coating scatter 1ppm;Surface scatter 13ppm
Appl. Opt.36, 337 (1997)
1998Q-factorAcoustic Loss &suspension systems
Nb microcantilever suspensionsLIGO, VIRGO & UWAsamples
Q~5107
Quantitative losspredictions confirmed
Phys. Lett. A,246, 37 (1998)
1998 Birefringencehomogeniety
PEM Birefringence mapping <0.03 /cm Phys. Lett. A237, 337 (1998)
1999 Rayleigh scattering Imaging Scatterometer 12.6ppm Opt. Commun.167, 7 (1999)
2000 x-ray inducedabsorptionre-annealing
VIRGO, ParisPartially reversed byannealing
J. Phys. D33, 589 (2000)
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History of CSI Whiteand Hemex-Ultrasapphire samples
EXPERIMENT RESULTS
Hemex Ultra
abs(ppm/cm)
55+/-4
Al (50.98%)O (47.8%)Si (0.615)P (0.055%)Ca (0.038)Signature(<10-4)of :Cu, S, Mo, F.
abs(ppm/cm)
~140(Stanford)
~80(UWA)
after annealing
24(UWA)
Csi-White
abs(ppm/cm)3. 3+/- 0.5
Al(56.6%) O (43%)Si (0.346)
Signature(<10-4) of:Th, Cu, Ca, S, Mo
abs(ppm/cm)
~120(Stanford)
~64
(UWA)
after annealing
40(UWA)
Photothermalabsorption
Photothermalabsorption
XRF
spectroscopy
Photothermalabsorption scan
Annealing
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Photothermal Absorption measurement results
Samples Absorption(ppm/cm)
Hemex Ultra(101020)
50->70->40 X-rayed->reannealed
CSI white(101020)
3->100->20 X-rayed->reannealed
CSI standard (A)(30100)
45->55 Localised exposure to x-ray
CSI white (C)(30100)
43
CSI white (D)(30100)
42
Russian Czochralski grown(30100)
90
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Absorption MapCSI Standard- #A
(plan z=10mm)
- 15 - 10 - 5 0 5 10 15
Horizontal positionHstepL- 15
- 10
- 5
0
5
10
15
lacitreV
noitis
opHpetsL
<1.3
<4.1
<6.9
<9.7
<12.5
<15.2
<18.
<20.8
<23.6
<26.3
<29.1
<31.9
<34.7
<37.5
<40.2
<43.
<45.8
<48.6
<51.4
<54.1
>54.1
ppmcm
Xray-irradiated spot Max=55.6ppm/cm
min=37ppm/cmaver=45.2 ppm/cmSTDdev=3.2
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Annealing Effect on the Absorption in the UV Range (F centers range)
200 300 400 500 600 700 800 900 1000 1100 1200
1E-4
1E-3
0.01
0.1
1
AB
SOR
PTIO
N C
OEF
FIC
IEN
T (c
m-1
)
WAVELENGTH (nm)
1E-4
1E-3
0.01
0.1
1
483 nm409 nm
568 nm band
298 nm band
364 nm band
1120 nm band
F2
+
921nmband
784 nm band
[Ti3+
][Ti4+
]
F+
F2and/or [Ti
3+][Ti
4+]
(~260 nm band)
F Hemex Ultra Csi White
200 250 300 3500.01
0.1
1
200 250 300 350
0.01
0.1
1
Dashed lines->Before annealingContinuous->After annealingred/Magenta->CSI-White sampleblue/Cyan->Hemex-Ultra sample
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Annealing Effect on the Absorption in the IR Range
200 300 400 500 600 700 800 900 1000
1E-4
1E-3
0.01
0.1
1
AB
SOR
PTIO
N C
OE
FFIC
IEN
T (
cm-1)
WAVELENGTH (nm)
200 300 400 500 600 700 800 900 1000
1E-4
1E-3
0.01
0.1
1
F2
+
921nmband
[Ti3+
][Ti4+
]
F+
F2
F Hemex Ultra Csi White
800 900 1000
1E-4
1E-3
750 800 850 900 950 1000
1E-4
1E-3
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Birefringence Phase Retardation (degree/ 10cm)
Contour Plot of Sapphire Hemex
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Rayleigh Scattering measurements set-up
CCD
Ammeter
Calibrated photo-detector
La s
e r
Data treatment
Sample
D
D:pupil.: angle of observation: collection solid angleV: scattering volume
V=d.S
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Rayleigh Scattering Measurement of Different Sapphire Samples
Sample sca @1064nm(ppm/cm)measured
sca @1064nm(ppm/cm)predicted
Hemex
(50100)
18.4
CSI standard (A)
(30100)
12.6
CSI standard (B)
(30100)
13.4
0.2
Fused silica I 11.7
Fused silica II 6.7 0.4
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Microcantilever suspension study
Qcantilever~ 3105
Internal mode of cantilever control
Qsapphire ~ 5107
High pressure contact (plastic deformation) to achieve low loss
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Internal Q of sapphire
Suspension System
niobium catherine wheel
cantilever
vacuum chamber
bottom stage (steel)
intermediate stage (brass)
steel ball
sapphire sample
aluminium platform
mechanical exciter
transducer
HEMEX sapphire sample (Cristal Systems)
100 mm
50 mmlongitudinal frequency = 53.4 kHz
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The Loss of Test Mass due to the Coupling to the Internal Resonances of Supporting structure
104
105
106
107
108
109
40 42 44 46 48 50 52 54 56
as-machined
annealed
annealed & etched
exp as machined
exp annealed
exp etched (2nd-)
Q o
f H
EM
EX
sap
phire
sam
ple
internal frequency of catherine wheel (kHz)
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Test of monolithic Nb pendulum
•Annealed & etched flexure1mm10mm 60m
•Material Q ~2 105
•Pendulum Q ~ 3 107
(3.4 kg, pressure corrected)
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0.001
0.01
0 10 20 30 40 50 60 70
y = 0.0086383 * e (̂-0.0017274x) R= 0.98176
Time (hr)
f=1.26 Hz
Q=8.2x106
Ring down of a Nb monolithic pendulum
Material Q-factor Q0= 2 x 105
(gas damping corrected)
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Dovetail Suspension
•Tensile equivalent to microcantilever •Low loss flexure included•Low mass reduces cantilever loss contribution
--predicted Qint>108
•Modular easily replaceable suspension element•Exceptional cryogenic performance predicted•Need to confirm sapphire Q after cutting
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2001 program on suspension:measure internal mode Q of sapphire
with Nb flexure suspension
Configuration 1
•Suspension losses minimised--coupling factor: 0.1~0.3
•Dovetail groove near stress antinode--possible Q-degradation
•Note: dovetail groove is very smallcf, Braginsky’s sapphire bar with horns
excitation
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Configuration 2
•Suspension loss maximised--coupling factor =1
•Low stress at dovetail joint
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Cryogenic Applications of
Dovetail Flexure
•Thermal conductivity of niobium at 10K:
90Wm-1K-1
•Expected thermal resistance:
~ 10K/W
•Niobium is an exceptional material
for high thermal conductivity isolation
and suspension stages
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ACIGA High Power Test FacilityResearch Program
2001 Implement 10m mode cleanerLow power evaluation of isolator/suspension pairs
Low residual motion isolators with pre-isolationNiobium flexure suspensions
2002 Adelaide University 5-10W laser.PR mirror + South Arm input mirrorBaseline data:
Lock acquisition Thermal lensing Optical degradation
2003 80m high power test cavity100W Adelaide University laser Power recycling cavity + 80m arm cavity
Lock acquisition under high radiation pressureThermal lensingOptical degradation
2004 East arm cavity-2005 Implement interferometer
for high power noise evaluation
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High Power Testing Facility at Gingin, WA
Interferometer arm for noise measurements(2004-2005)
80m high power test cavity (2003)
10m Mode cleaner (2001)
Injection locked laser0.5W (2001), 5W (2002), 100W (2004)
Pre-stabilisationcavity (2001)
Beam expander
Input mirror(2002)
End mirror (2003)
Power recycling(2002)