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M. S. Tillack Final Optic Research – Progress and Plans HAPL Project Meeting, PPPL 27-28 October 2004 Z. Dragojlovic, F. Hegeler, E. Hsieh, J. Mar, F. Najmabadi, J. Pulsifer, K. Sequoia, M. Wolford with contributions from :
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Overview 1.Final optic program summary 2.New mirror fabrication and testing 3.Larger scale testing 4.Contaminant transport modeling 5.Gas puff modeling
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The steps to develop a final optic for a Laser IFE power plant (1 of 2) 1.“Front runner” final optic – Al coated SiC GIMM: UV reflectivity, industrial base, radiation resistance 2. Characterize threats to mirror: LIDT, radiation transport, contaminants Key Issues: Shallow angle stability Laser damage resistance goal = 5 J/cm 2, 10 8 shots Contamination Optical quality Fabrication Radiation resistance 3. Perform research to explore damage mechanisms, lifetime and mitigation MicrostructureBonding/coatingFatigueIon mitigation
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6. Perform mid-scale testing5.Develop fabrication techniques and advanced concepts The steps to develop a final optic for a Laser IFE power plant (2 of 2) 4. Verify durability through exposure experiments 10 Hz KrF laser UCSD (LIDT) XAPPER LLNL (x-rays) ion acceleratorneutron modeling and exposures
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Diamond-turned, electroplated mirrors survived 10 5 shots at 18 J/cm 2 on a small scale (mm 2 )... and we would like to improve the high-cycle fatigue behavior Still, these mirrors ultimately fail due to grain motions,... 1.Relatively small grains (10-20 m) 2.Relatively dense, thick coating
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35 m “thick thin-film” mirror, turned at Schafer Corp. and exposed to 10 4 shots at 5 J/cm 2 no damage to elecroplated mirror (turned at GA) under the same exposure conditions Post-processing after thick (35-50 m) thin-film deposition should provide good optical quality with a damage-resistant microstructure rough substratepolish/turncoatfinal polish/turn
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Ringdown reflectometry (now @266 nm) indicates somewhat high absorption at 85˚ reflectivity of 35 m Schafer mirror
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Diamond turning lines are too deep – 50 nm rms – (A new Pacific Nanotechnolgy AFM has been added to our surface analysis capabilities)
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Peaks grow during exposure (unlike earlier results which exhibited etching) etching observed previously in diamond- turned polycrystalline foils
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It’s time to start making smoother mirrors MRF systems are popping up all over the place (this one is at Edmund Optics)
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Larger mirrors are being fabricated with increasing emphasis on surface quality 2.Other improvements under consideration MRF surface finishing Hardening techniques nanoprecipitate, solid solution hardening friction stir burnishing (smaller grains) 1.Mid-scale 4” optics Thick e-beam coatings Electroplated Al
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Scaled testing was initiated at Electra during late August we spent 1 week assembling the optical path, developing test procedures, and exploring issues for large scale testing
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Experimental Layout 43” 12” Lens Beam Dump Wave Plate Cube Mirror Beam Sampler Beam Profiler UV Window Window Camera
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Laser energy measurements showed dramatic energy loss along the beam path vacuum chamber telescope Nike mirror periscope 1” aperture 1/2 waveplate polarizer cubes 3” lead aperture 2” graphite aperture Electra oscillator 0.57 J 5.2 J 3.9 J 0.14 J p-polarized 1.04 J 10 cm 12.8 J (measured with a 30cm x 30 cm calorimeter) 14.2 – 15.3 J (measured with a 30 cm x 30 cm calorimeter) 13.2 J with a 2” dia. aperture 80 cm 0.14 J to 5.2 J (measured with a 2” calorimeter)
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We don’t see this with our Compex laser 1234 1 = 86 mJ 2 = 84 mJ 1 2 34 5 6 7 8 1 = 228 mJ 2 = 119 mJ 3 = 95 mJ 4 = 92 mJ 5 = 13 mJ 6 = 75 mJ 7 = 58 mJ 8 = 56 mJ 3 = 86 mJ 4 = 85 mJ
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An alternative idea for scaled testing: large-aperture uncoated FS window @56˚ 10” diameter, 6-m fl Nike lens 700 J blunderbuss 8” port 12” FS window ($5250) 30 cm square aperture 34˚ 10” round aperture 30 cm 6.7” 10” assume 700 J in 900 cm 2 ~ 0.75 J/cm 2 ~25% of s-light reflected = 0.09 J/cm 2 10” round on 6x12 rectangle ~ 362 cm 2 35 Joules (polarized) available beam dump chamber
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Another alternative idea for scaled testing: Contrast is >100:1 over a 7˚ range 10” diameter, 6-m fl Nike lens 700 J blunderbuss 8” port 12” FS window 30 cm square beam with 9” round aperture 32˚ 12” 6” assume 700 J in 900 cm 2 ~ 0.75 J/cm 2 ~25% of s-light reflected = 0.09 J/cm 2 9” round ~ 410 cm 2 37 Joules (polarized) available beam dump chamber
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Displacement field after 1st shot Net flow toward chamber center is predicted – we need to include rad-hydro displacements Net flow toward optic? Contamination transport from the chamber to the final optic was explored using Spartan 160 MJ NRL target 50 mTorr Xe @RT Bucky hand-off at 500 s
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Particles transport rapidly toward the final optic We need to run multiple shots to establish the long-term behavior Test particle trajectoriesPressure at 100 ms Pa 1 2 3 4
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Gas puffing was examined as a posssible optic protection technique ~1 Torr-m may help reduce ion and x-ray damage Fast gas puff could be used immediately preceding implosions Might also help cool chamber gas
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A gas puff sufficient to protect optics would increase the base pressure beyond 100 mTorr Pump speed per duct1.5x10 5 l/s Duct diameter75 cm Duct length3 m Number of ducts64 Orifice conductance44 l/s/cm 2 Target mass4 mg Rep rate5 Hz Chamber radius7 m It doesn’t look promising!
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electroplate success 5-yr plan and progress to date 20012002200320052006 startKrF larger optics initial promising results at 532 nm attempts at thin film optics Phase I evaluation lower limits at 248 nm, chemistry control new lab, cryopump extended database, mid-scale testing, radiation damage, mirror quality, design integration 2004
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