G0300294-00-M LIGO Laboratory1 Responses to Review Questions David Shoemaker, Peter Fritschel NSF Review of Advanced LIGO 12 June 2003.

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Presentation transcript:

G M LIGO Laboratory1 Responses to Review Questions David Shoemaker, Peter Fritschel NSF Review of Advanced LIGO 12 June 2003

G M LIGO Laboratory2 Plan for choosing substrate Basic notion: »Sapphire development for the downselect close to completed; some measurements remain »Silica development still being pursued »Continue analysis of impact of current material properties on performance »Continue coating development in parallel »Downselect at latest time compatible with other schedule constraints

G M LIGO Laboratory3 Sapphire Further characterization: »Absorption, scattering (level, spatial scale) on additional samples: 6 months –Caltech scanning setup to be built, and/or SMA Lyon contracted for measurements –Billingsley, Armandula »Homogeneity – confirmation of positive results »Birefringence – characterization of large pieces »Mechanical Q on additional samples: 6 months –Additional existing samples of sapphire – disks, rods –Harry, Willems, Rowan »Trace element analysis – neutron activation, precision spectroscopy Experiments »Annealing to reduce absorption: ongoing –Route et al Analysis: 6 months »Optics simulation with absorption profiles –Kells, d’Ambrosio Times in parallel, data in ~6 months

G M LIGO Laboratory4 Silica Measurements to be made »Mechanical Q in input test mass material (‘Suprasil 311 SV’) –Measure additional existing samples, Acquire additional samples –Harry, Penn, Ageev Experiments »Annealing –Oven time to be rented (near term), oven acquired (Penn) –Regimes of time and temperature to be explored, Effect of polishing to be explored –Characterization of sample before and after for optical, mechanical properties Polishing test, 3 months, small samples »Ion beam and superpolishing of surfaces, anneal, characterize Surface character test, 3 months »Repolish after anneal, characterize  Initial results for comparison with Sapphire Scaling of annealing process, 6 months »Scale up to midsize piece »Scale to initial LIGO piece Results in ~1 year

G M LIGO Laboratory5 Downselect Plan Downselect team : Jordan Camp, Marty Fejer, Peter Saulson, Phil Willems, Jim Hough, Peter Fritschel, Sam Finn, David Shoemaker (chair) Team meets monthly to discuss progress, choose directions, brainstorm Document, web site tracks status – » Downselect Date is April 04 »Allows both Sapphire and Silica evaluation to make good progress

G M LIGO Laboratory6 Plan for Coating development Coordinated trials and characterization »Advanced LIGO Coating Development Plan, LIGO-C R RFP out, »multiple vendors interested, anticipate selecting 2 »Informal responses encourage our approach Motivated by experiments to date, perceived expertise in coating vendors 8 coating runs anticipated, ~8 months for complete cycle Continue with one vendor, refining concept Encouraged to pursue program with university materials science expertise – will integrate into program Example flow chart from plan

G M LIGO Laboratory7 Coating Characterization Measurements »Internal friction (LIGO, Stanford, Glasgow, HWS) »Optical absorption (LIGO, Stanford, vendors) »Birefringence (LIGO) »Young’s modulus (Stanford, vendors) »Thermal expansion (Stanford) Team »MIT - Gregg Harry, David Shoemaker »Caltech - Helena Armandula, GariLynn Billingsley, Dennis Coyne, Eric Black, Riccardo DeSalvo »Livingston - Andri Gretarsson »LSC Collaborators »Stanford University - Sheila Rowan, Martin Fejer, Roger Route, Vlad Kondilenko, Alex Alexandrovski »Glasgow University - Jim Hough, Peter Sneddon, David Crooks »Hobart and William Smith College - Steve Penn »University of Florida - Dave Reitze »TAMA collaborators »University of Tokyo - Kenji Numata(GSFC), Masaki Ando

G M LIGO Laboratory8 Recovery scenario Suppose no improvement in coatings found before coatings must be applied (in ~2006), BUT then a better coating is developed at a later time (e.g., 2010) Spares for test masses would be coated with improved coating; sufficient spares exist to replace all masses in one interferometer Old coated masses swapped out for new coated masses »Opening vacuum, but minor activity – down time of ~1 month Old coated masses repolished, coated, installed in second ifo »~6 month turnaround Process repeated for third interferometer …gradual upgrade of all interferometers over ~1.5 years, minimal down time (~3 months out of ~18 months), cost ~$2M

G M LIGO Laboratory9 What are the big steps leading to the Advanced LIGO sensitivity? Seismic noise rendered negligible through a combination of Active Isolation systems, and multiple-pendulum suspensions »Moves wall from 40 Hz to 10 Hz, below Newtonian background Thermal noise reduced by materials, assembly techniques »Suspensions of fused silica, monolithic construction lowers suspension noise below Newtonian Background »Choice of low-loss sapphire substrates to minimize internal thermal noise »Development of low-mechanical-loss coatings Quantum noise reduced by significant increase in power »Factor of 20 over initial LIGO Quantum noise, power “managed” with signal recycling »Optimization of response for given laser power, thermal noise, and astrophysical signal signatures

G M LIGO Laboratory10 Risk Items Laser power »Plan calls for 180 watts »If do not improve over present 87 W, 322 Mpc instead of 350 Mpc Laser intensity noise »Plan calls for 2e-9 ΔP/P (to make contribution 1/10 of other noises) »If do not improve over present 1e-8, noise level increases by 1.11 in amplitude Modulators/Isolators »Plan calls for handling 180 W »If can only handle half power, 322 Mpc instead of 350 Mpc Sapphire absorption »Plan calls for 40 ppm/cm, irregularities ‘moderate’ »If do not improve over present average of 60 ppm, reduce input power to (40/60), 332 Mpc »If do not improve over present irregularity of pk-pk ~130 ppm and spatial scales of ~0.5 cm, guess 10% power loss, or ~340 Mpc

G M LIGO Laboratory11 Impact of reduced laser power or sapphire absorption losses

G M LIGO Laboratory12 10 Hz100 Hz1 kHz Anatomy of the projected Adv LIGO detector performance Newtonian background, estimate for LIGO sites Seismic ‘cutoff’ at 10 Hz Suspension thermal noise Test mass thermal noise Unified quantum noise dominates at most frequencies for full power, broadband tuning Advanced LIGO's Fabry-Perot Michelson Interferometer is a platform for all currently envisaged enhancements to this detector architecture Initial LIGO Advanced LIGO

G M LIGO Laboratory13 Risk Items Test Masses »Plan calls for sapphire »If choose fused silica, good coatings, ~ worst case 300 Mpc

G M LIGO Laboratory14 Risk Items Coatings »Plan calls for losses of ~2e-5 phi on sapphire »If do not improve over present best 1e-4 phi, 314 Mpc

G M LIGO Laboratory15 Risk Items Suspension thermal noise »Losses in fiber could be greater than anticipated »Factor 10 increase would give small change in NS seeing »Impact on stochastic background, BH – TBD Seismic Isolation »Noise in system could be greater than anticipated, or gains lower »Raises low-frequency limit of interferometer; very hard to raise to 20 Hz, small change in NS seeing »Impact on stochastic background, BH – TBD

G M LIGO Laboratory16 10 Hz100 Hz1 kHz Anatomy of the projected Adv LIGO detector performance Newtonian background, estimate for LIGO sites Seismic ‘cutoff’ at 10 Hz Suspension thermal noise Test mass thermal noise Unified quantum noise dominates at most frequencies for full power, broadband tuning Advanced LIGO's Fabry-Perot Michelson Interferometer is a platform for all currently envisaged enhancements to this detector architecture Initial LIGO Advanced LIGO

G M LIGO Laboratory17 Risk Items: summary Seeing distance for NS binaries, linear noise robust against most shortcomings 10-20% losses in sensitivity if we are “stuck” at the present levels of R&D progress Most potential risks considered small Coating may be a difficult problem to solve – (but only) 10-20% loss in sensitivity if we find no improvement over current best levels of coating loss