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Overview of Advanced LIGO Coating Status
Sheila Rowan University of Glasgow for the Core Optics Working Group Plenary technical session LSC meeting, Livingston, LA 17th March 2004
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Coating Development Specifications for Test Masses
Parameter Sapphire goal Sapphire requirement Fused Silica goal Fused Silica requirement Mechanical loss 2 x 10-5 6 x 10-5 1 x 10-5 3 x 10-5 Optical Absorption 0.5 ppm 1 ppm 0.2 ppm Thermal expansion 5 x 10-6/K < 2 x 10-5/K >1 x 10-6/K 5 x 10-7/K < 2 x 10-6/K >1 x 10-7/K Birefringence 1 x 10-4 rad 2 x 10-4 rad - Scatter5 2 ppm Thickness uniformity 10-3 (over 21.5 cm diameter) 10-2 (over 33.0 cm diameter) 10-2 (over 30.0 cm diameter) ITM HR transmission 5 x 10-3 ±2.5 x 10-4 ETM HR transmission 5 ppm 10 ppm Test Mass HR matching 1 x 10-2 AR reflectivity 200 ±20 ppm
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Adv LIGO Coating Requirements
Mechanical loss Fused silica : f < 3 x 10-5 (goal 1 x 10-5) Sapphire: f < 6 x 10-5 ( goal 2 x 10-5 ) These numbers are guides, thermal noise will depend on other parameters also. Source of requirements on all parameters influencing thermal noise: Brownian thermal noise (Nakagawa/Gretarsson) Thermoelastic noise (Braginsky/Fejer) AdvLIGO sensitivity modeling with BENCH Optical absorption Fused silica: 0.5 ppm (goal 0.2 ppm) Sapphire: 1 ppm (goal 0.5 ppm)
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Results for Initial LIGO Silica/Tantala Coating
Silica substrates were coated with layers of alternating silica and tantala, similar to the initial LIGO coating Q factors were measured by exciting resonances in the samples and recording the subsequent decay Fused silica substrates of 2 different aspect ratios used: ‘Thick’ samples (3” dia. x 1” thick): c=(2.8 ± 0.7) x 10-4 ‘Thin’ samples (3” dia. x 0.100” thick): butterfly = 2.7 x 10-4 drumhead = 3.1 x 10-4
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Reminder of Previous Results
Measurements on several SiO2/Ta2O5 coatings with different amounts of layers (2 to 60) and with various layer thickness in different combinations (λ/4 - λ/4; λ/8 - 3λ/8; 3λ/8 - λ/8) Concluded that: Substrate / coating interface is not a significant source of loss. Coating layer interfaces are not a dominant source of loss Ta2O5 has a higher mechanical loss than SiO2 fsilica = (4±3)x f (2.7±0.9)x10-9 ftantala = (4.2±0.4)x f (4±9)x10-10
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Status of experiments Measured mechanical loss (and optical absorption) of a number of alternate coatings: eg: Al203/Ta2O5 SiO2/Al203 Nb2O5/ SiO2 Mechanical loss results are broadly similar to SiO2/Ta2O5 – no significant benefits from using coatings listed above. Most promising results to date: Ti-Doped (3%) Ta2O5 / SiO2 Reduction in coating loss: c= (1.8 +/- 0.1) x 10-4 c= (1.5 +/- 0.7) x 10-4
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Program Overview Driver is development of low mechanical loss coating
Optical and thermo-mechanical properties will be studied during development, (vendors, Caltech, Stanford), but will not drive program until mechanical loss is better understood and/or a low mechanical loss coating is developed Coating vendors selected: LMA/Virgo in Lyon, France CSIRO in Sydney, Australia Next phase of coating development has begun
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Current results and immediate coating development plans
CSIRO: First ‘calibration’ coating studies of SiO2/Ta2O5 coating from CSIRO: fc = (4.4 +/- 0.6) x 10-4 fbutterfly = (4.1 +/- 0.1) x 10-4 fdrumhead = (5.0 +/- 0.1) x 10-4 ‘secondary ion-bombardment’ used in deposition process (Nb: coating appeared to show variations in thickness across surface) LMA/VIRGO: Currently working on: a) depositing single layers of coating materials for study of mechanical loss and thermo-mechanical properties b) depositing doped SiO2/Ta2O5 coating on sapphire substrate
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Coating development plans
Dopants Continue with studies of effects of doping on mechanical loss SiO2/Ta2O5 doped with 3% Ti showed a reduction in mechanical loss without sacrificing n, Y, or optical absorption. Alternate high index materials HfO2/SiO2 sample produced – mechanical loss to be measured shortly Annealing Systematic studies of effects of annealing on coating mechanical loss Ion bombardment of substrate during coating Controls density and stress of coatings – investigate effect on mechanical loss
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R & D Milestones Start Coating Development January 2004
Substrate Material Downselect June 2004 Coating Material Downselect June 2005 LASTI’s ETM Delivered January 2006
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