17 Pages

G050113-00

Course: G 050113, Fall 2009
School: Caltech
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Thermal Suspension Noise in Initial LIGO Gregory Harry LIGO / MIT March 23, 2005 Detector Characterization LSC Meeting LLO LIGO-G050113-00-R Outline Impact of thermal noise on sensitivity and commissioning Measurements of suspension thermal noise Frequency domain Time domain Discrepancies Questions and ideas Feedback contamination Modeling Impact of Thermal Noise Suspension thermal noise Suspension T...

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Thermal Suspension Noise in Initial LIGO Gregory Harry LIGO / MIT March 23, 2005 Detector Characterization LSC Meeting LLO LIGO-G050113-00-R Outline Impact of thermal noise on sensitivity and commissioning Measurements of suspension thermal noise Frequency domain Time domain Discrepancies Questions and ideas Feedback contamination Modeling Impact of Thermal Noise Suspension thermal noise Suspension T hermal Noise Structural damping Lower loss Thermoelastic can be relevant = 6 10 -3 LHO 4K Noise -3 -4 = 2 10 Mirror thermal noise Coating (SiO2/Ta2O5) thermal noise dominant Silica substrate thermal noise not really a factor About factor of 5 below SRD Optic al (Shot) = 3 10 SRD Noise Three presented scenarios for suspension thermal noise Pessimistic (worst measured) Nominal (average measured) Optimistic (material limit) Coating T hermal Sensitivity to Sources Single Interferometer Sensitivity Neutron Star Inspirals SRD = 6 10-3 = 2 10-3 = 3 10-4 Thermoelastic Limit 16 Mpc 16 Mpc 20 Mpc 26 Mpc 29 Mpc 10 MO Black Hole Inspirals 63 Mpc 60 Mpc 84 Mpc 120 Mpc 140 Mpc Stochastic Background Crab Pulsar ( limit) 1.6 10-5 2.3 10-5 1.4 10-5 7.5 10-6 5.7 10-6 Sco X-1 Pulsar ( limit) 3.1 10-7 3.0 10-7 3.0 10-7 3.0 10-7 3.0 10-7 2.3 10-6 4.7 10-6 1.9 10-6 5.9 10-7 2.7 10-7 Suspension Thermal Noise Sx(f) = 4 kB T g/(m L (2 f)5) Dissipation Dilution Restoring force in pendulum is due to both elastic bending and gravity Effective loss angle for thermal noise `diluted' by the ratio = ke/kg (ke/kg)violin = 2/L (E I/T) (1+1/(2 L) (E I/T) n2 2) 2/L (E I/T) = 3.5 10-3 Correction for first three violin mode harmonics is negligible 5 Q Measurements Frequency Domain Collect data for ~ 2 h Associate peaks with mirrors Fit Lorentzians to peaks Limitations Optical gain drift ? Get similar results with S2 data as current data with improved wavefront sensors Temperature drift can cause central frequency to migrate Minimal over a few hours Graphic from R. Adhikari's Thesis 6 Q Measurements Time Domain Excited modes with onresonance drive to coil Let freely ring down Put notch filters in LSC loop Fit data to decaying exponential times sine wave Limitations Must ring up to much higher amplitude than thermal excitation No consistent difference between Michelson and Full IFO locks LLO ITMy Violin Mode 1 0.5 Amplitude 0 -0.5 -1 -1.5 0 20 40 60 Time (s) 80 100 120 10 2 Amplitude 10 0 10 -2 10 -4 0 20 40 60 Time (s) 80 100 120 Feedback can effect measured Q 7 Violin Mode Results Overview Ringdown Q's and frequency domain fits do not agree Ringdown Q's repeatable within a lock stretch but frequency domain fits are not Results different in different lock stretches High harmonics show a little more pattern Still unexplained discrepancies Highest Q's consistent with material loss in wires Gillespie laboratory results Similar (lack of) patterns in all three IFOs Data from all 3, but more data on H2 than others Violin Mode Results Livingston Comparison of Time Domain and Frequency Domain x 10 5 Time Domain 2 Frequency Domain 1.5 Q 1 0.5 0 ITMy l ITMy h l ETMy ETMy h ETMx l ETMx h ITMx l ITMx h Violin Mode Results Hanford 2K Comparison of Frequency Domain Q's in Same Lock UTC 10:30 Jan 31, 2005 2 x 10 6 Comparison of Time Domain Q's in Same Lock 2 x 10 6 1.5 ITMx low ITMx high ITMy low ITMy high 1.5 ITMx low ITMx high ITMy low ITMy high 0.5 Q 20 40 60 80 1 1 Q 0.5 0 0 Time (minutes) 0 1 Ringdown Number 2 3 Violin Mode Results Hanford 2K/Livingston Comparison of Time Domain Q's in Different Locks LHO2K IMTx low 8.6 104 1.6 105 1.6 105 1.2 105 LLO ITMx high 1.7 105 1.4 105 Higher Harmonic Results Hanford 2K 10^7 Time Domain Frequency Domain 10^6 Q 10^5 10^4 x 2l x 2h x 3l x 3h ITM y 2l y 2h y 3l y 3h Violin Mode Results Hanford Highest Q's Measured Frequency Domain H2K ITMx Third Harmonic H2K ITMy Third Harmonic H4K ITMy Third Harmonic Time Domain H2K ITMy Third Harmonic Gillespie Lab Results Q 3.2 106 1.6 106 9.8 105 8.6 10-5 1.7 10-4 2.8 10-4 2.3 105 1.2 10-3 3 10-4 Questions from Violin Q Measurements Why the disagreement between t and f domain? Is f domain unreliable? Why? Changes in instrument over hour time scales? Optical drift? Thermal drift? Interaction between degenerate polarizations of modes? Why changes in ringdowns between lock stretches? Changes in suspension during lock acquisition? Feedback influence on Q's? ASC? LSC and optical spring? Why are the highest Q's in f domain third harmonic? Higher frequency gets away from unity gain frequency of loop? Why not seen in t domain? How reliable are these numbers? Changing thermal noise from lock to lock? Feedback contamination so Q's do not predict thermal noise? What about internal mode Q's? Modeling Some Hope for Answers Is feedback mechanism feasible? Violin modes coming soon to e2e What about loss from optical spring? Thomas Corbitt at MIT has done preliminary modeling Need to have cavity offset from...

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