Cryogenics in CLIO Masatake Ohashi and the LCGT collaboration
Status of LCGT and CLIO Masatake Ohashi (ICRR, The University of TOKYO) and LCGT, CLIO collaborators...
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Transcript of Status of LCGT and CLIO Masatake Ohashi (ICRR, The University of TOKYO) and LCGT, CLIO collaborators...
Status of LCGT and CLIO
Masatake Ohashi(ICRR, The University of TOKYO)
andLCGT, CLIO collaborators
TAUP2007Sendai, Japan
2007/9/12
Status of LCGT and CLIO
Masatake Ohashi(ICRR, The University of TOKYO)
andLCGT, CLIO collaborators
TAUP2007Sendai, Japan
2007/9/12
TAUP 2007 Sendai Japan 2007/09/12TAUP 2007 Sendai Japan 2007/09/12
Contents
• LCGT Outline• Status of LCGT
– Interferometer Design– Sapphire Mirror and its Suspension– Cryostat and Cooling Technique
• Status of CLIO– Present Status as a proto-type of
LCGT
• Summary
TAUP 2007 Sendai Japan 2007/09/12illustration: KAGAYA
Large-scale Cryogenic Gravitational wave Telescope ( LCGT) 180Mpc
TAUP 2007 Sendai Japan 2007/09/12TAUP 2007 Sendai Japan 2007/09/12
LCGT Outline
• It is 3km Fabry-Perot interferometer with power recycling and broadband RSE.
• Main mirrors made of sapphire are cooled at 20K.
• It is built at underground site in Kamioka Mine.
• Two independent interferometers are installed.
• The main target is the coalescence of Binary Neutron Star s at 180Mpc.
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LCGT on LIGO Web
Next generation IFO from Japan
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Merit of Underground site
Quiet !
Seismic activity of city area
Seismic activity of Kamioka Mine
The point is that
at least 100m below land surface is necessary to prevent wind effect.
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Interferometer Design
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Interferometer Design - Over View 1 -
• Detector parametersLaserNd:YAG laser (1064nm)Injection lock + MOPA
Power : 150 W
Main InterferometerBroad band RSE configuration
Baseline length : 3kmBeam Radius : 3-5cmArm cavity Finesse : 1550Power Recycling Gain : 11Signal Band Gain : 15Stored Power : 771kWSignal band : 230Hz
Vacuum systemBeam duct diameter : 100cmPressure : 10-9 Torr
MirrorSapphire substrate + mirror coating
Diameter :25cmThickness :15cmMass : 30 kgAbsorption Loss : 20ppm/cmTemperature : 20 KQ = 108
Loss of coating : 10-4
Final SuspensionSuspension + heat link with 4 Sapphire fibersSuspension length :40cmFiber diameter :1.5mmTemperature : 16KQ of final suspension : 108
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Interferometer Design - Over View 2 -
Main IFO : 3km IFO Input optics : Two MCs, Modulators, MMTOutput optics: OMC, Photo detectors
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Interferometer Design - Layout 1 -
Center room for IFO-1
Center room for IFO-2
3km arm
3km
arm
Two IFOs share the vacuum pipes
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Interferometer Design- RSE -
• Merit of RSEHigh-finesse cavity and moderate PRGEasier to realize high power in cavitiesSmaller transmission light in opticsFlexible optimization for GW sources
Independent adjustment of power in cavities and signal bandNarrow-band observation (optional)
Main reason for LCGT
Absorption in sapphire substrates Heat absorption : 20ppm/cm x 15 cm = 300 ppm Cooling power : 1W for each mirror
Laser power on BS should be less than ~1kW (safety factor 3)
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Sapphire Mirror
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Sapphire Mirror- Absorption -
Laser light absorption is important factor for cooling.
LCGT requirement :
substrate 20ppm/cm (-> 250mW) coating 1ppm (-> 40mW)
We need high quality sapphire substrate.
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Sapphire Mirror- Mechanical Quality Factor -
Over 108 is obtained
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Sapphire Mirror- Dissipation of the Coating film -
Loss A
ng
le
Temperature [K]
Dissipation is almost independent of Temperature
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Sapphire Mirror- Thermal Expansion -
Thermal expansion is negligible at cryogenic temperature.
Th
erm
al Exp
an
sio
n
Temperature [K]
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Cryogenic Techniques
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Cryogenic Technique- Estimated Heat Generation in the Mirror -
T=20 K
q=290 mW ・ Design Safety factor
Mirror substrate : SapphireSuspension rods : Sapphire
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Cooling method by a cryocooler
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Seismic Noise Attenuation
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Seismic Attenuation System (SAS)
• Inverted pendulum – 30mHz
• 3 cascaded GAS filter – 500mHz
• Test mass suspension– triple pendulum
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Suspension Point Interferometer (SPI)- Background and Purpose -
(i) Seismic noisethrough heat link wires(HLWs)
DampingMagnets
VibrationIsolationSystem(Room temp.)
CryogenicSuspension(4K-20K)Upper Mass(SPI)
Test Mass (Main IFO)
Recoil MassCoil-magnetActuators
Upper RecoilMass
Flex Joint
GAS filter
Displacement sensorCoil-magnet actuator
Acc. sensor
InvertedPendulum
SuspensionPlatform
77K shield4.2K shield
(ii) Magnet - CoilActuator Noise
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Schedule and Budget
LCGT proposal is submitted to the Ministry of Education and Science ( MEXT) as one of recommended projects of the University of TOKYO. But LCGT will not start at 2008.
130 M$ without salary and maintenance
We will retry next year.
2008 2009 2010 2011 2012 2013 2014
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CLIO
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Cryogenic prototype for LCGT
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Overview of CLIO
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Cryostat for an end mirror
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8.8K45K
63K
12.9K
Cooling test and achieved temperature
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Cooling summary
Cooling time
Mirror tempHeat in the suspension
Heat at the 1st cooling2006/02
Inline end 176hourstart 07/06/22,10:00
13.5K 40mW N/A
Inline near 174hourstart 07/06/22,10:00
13.4K 36mW N/A
Per arm end
164hourstart 07/04/27,11:05
12.5K 62mW#1 116mW
Per arm near
193hourstart 07/08/16,12:30
13.8K 29mW 109mW
#1; No shield for radiation from the outer shield at 63K.
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Low vibration PT refrigeratorby KEK and SUMITOMO
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Cryogenic suspension
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Heat Transfer
Radiation shield (40K)Mirror (20K)
300K Radiation( straying )
300K Radiation from window of Gate Valve warms mirrors
Serious Problem for cooling
Good Heat Transfer, Baffles, …
Gate Valve (300K)
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Radiation Shields
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Cooling procedure
Cooling shortens suspension by 2mm
STEP1 cooling mirror alignment
STEP4 cooling mirror alignment
STEP2 cooling mirror alignment
STEP3 cooling mirror alignment
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Expected Noise Spectrum at 20K
Current best (300K)
Target sensitivity (300K)
Target sensitivity (20K)
Resonance of suspension system
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Noise budget for CLIO (300K)
Cooling
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YES !Thermal Noise of Aluminum Wires
Thermal noise reduced by cooling ?
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CLIO Stability
Akutsu’s POSTER
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SUMMARY
• We will submit LCGT budget request for FY2009 again next year.
• Cryogenic prototype CLIO was completed. Now in commissioning phase.
• We demonstrated to operate interferometer with cryogenic mirrors, but careful heat transfer is necessary for cooling.
TAUP 2007 Sendai Japan 2007/09/12
European Plan
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Interferometer Design - Layout 2 -
Baffle for LCGTSpecification of LCGT
Tube diameter 1000mmMirror diameter 250mmMirror distance 600mmMirror offset 340mmSeismic motion 1 x 10-11m/Hz1/2@30Hz
Estimated scattered light noise4.2 x 10-21m/Hz1/2@30Hz (Safety factor=7)
1/10
45
(for one mirror)
Integration
Each reflection
Baffle designNumber: 45x2for one armHeight: 35~50mmSurface: DLC coatings
Diamond-Like Carbon (DLC) coatingsSurface roughness: Ra=20nmOutgassing: lower than SS316 with baking
Reflectivity: 5% for p-polarization at 45deg.