Progress in UCSD Chamber Simulation Experiments Farrokh Najmabadi Sophia Chen, Andres Gaeris, Bindhu Harilal, S.S. Harilal, John Pulsifer, Mark Tillack.

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Presentation transcript:

Progress in UCSD Chamber Simulation Experiments Farrokh Najmabadi Sophia Chen, Andres Gaeris, Bindhu Harilal, S.S. Harilal, John Pulsifer, Mark Tillack HAPL Meeting April 4-5, 2002 San Diego, CA Electronic copy: UCSD IFE Web Site:

Thermo-mechanical Response of the Wall Is Mainly Dictated by Wall Temperature Evolution  In order to develop predictive capability: There is no need to exactly duplicate wall temperature temporal and spatial profiles. (We do not know them anyway!) Rather, we need to measure and understand the wall response in a relevant range of wall temperature profiles and in real time.  Most phenomena encountered depend on wall temperature evolution (temporal and spatial) and chamber environment Only sputtering and radiation (ion & neutron) damage effects depend on “how” the energy is delivered.  Most energy sources (lasers, X-rays, ion beam) can generate similar temperature temporal and spatial profiles.

One Laser Pulse Can Simulate Wall Temperature Evolution due to X-rays  Only laser intensity is adjusted to give similar peak temperatures.  Spatial temperature profile can be adjusted by changing laser pulse shape. NRL Target, X-ray Only 1 J/cm 2, 10 ns Rectangular pulse Time (  s) Wall surface 10  m depth Time (  s) Laser 0.24 J/cm 2,10 ns Gaussian pulse

Careful Measurements of the Wall response is the Focus of our Simulation Experiments Sample can be examined for material behavior after high rep-rate experiments Per shot Ejecta Mass and Constituents Real Time Thermal shock and stress Vacuum Chamber provides a controlled environment Laser pulse simulates temperature evolution A suite of diagnostics is identified Real Time Temperature

Components of Simulation Experiment  High-Temperature Sample HolderDesigned, In Fabrication.  Preparation of Vacuum ChamberReady  Optical Train Main laser:Ready SBS CellIn assembly  Master Timing Control SystemTested on protoboard Awaits Integrated Test  Data Acquisition SystemEquipment Purchased Software is under development  Diagnostics: PIMAX and SpectrographReady ThermometerDesigned, Parts purchased IR CameraPurchase is deferred to June. Quartz MicrobalancingPurchase is deferred to June. RGAPurchase is deferred to June.

 Function: Maintains an equilibrium temperature of o C to simulate laser- IFE wall conditions.  Both active cooling (over cooling) and heating (for feedback control).  Radiative heating from a tungsten element is the best option: Uniform temperature No insulator Can easily exceed 500 o C Halogen lamps are not small enough to fit behind a ~1 cm diameter sample. High Temperature Sample Holder Thermocouples Specimen Flange Power supply PID Vacuum Fan Atmosphere Air flow Laser

High Temperature Sample Holder is Designed and is in Fabrication Specimen Ceramic Insulator S.S. vacuum seal Air cooling inlet Sample holder is made of Mo Copper conductor with set screw Power feed through Thermocouple feed through

Vacuum System is Ready  Vacuum System: Capable to Torr  High-temperature Sample Holder can radiate up to 100W into the chamber: Mockup Experiment

Laser Optical Train is Ready New SBS cell is in Fabrication  Data Acquisition system is capable of 5 G sample/s. Equipment installed. Software being developed.  Timing/control system is tested at protoboard level.

Real-time Temperature Measurements Can Be Made With Fast Optical Thermometry MCFOT — Multi-Color Fiber Optic Thermometry  Compares the thermal emission intensity at several narrow spectral bands.  Time resolution ~100 ps to 1 ns.  Measurement range is from ambient to ionization—self-calibrating.  Simple design, construction, operation and analysis.  Easy selection of spectral ranges, via filter changes.  Emissivity must be known. Emissivitiy Correlation can be used!  Detailed Design completed. Parts Purchased.

Feb. Mar. Apr. May Jun.Jul. Integrated Test Sample Holder DesignFab. Thermal Control system Integrated Test Data Optical Train Design Purchase Alignment New SBS Cell Data Acquisition Purchase Install. & Software Dev. Control & timing DesignProtoboradIntegrated Test Thermometer Design Purchase Assembly Calibration PIMAX & Spectrograph Ready IR Camera RGA QCM Purchase Assembly } Experiment Should Be Ready By June 2002

Backup Slides

FOTERM-S Is a Self-Referential Fast Optical Thermometry Technique FOTERM-S: Fiber Optic Temperature & Emissivity Radiative Measurement Self standard  Compares the direct thermal emission and its self-reflection at a narrow spectral band to measure both temperature and emissivitiy.  Time resolution ~100 ps to 1 ns.  Measurement range is from ambient to ionization—self-calibrating.  More complex design and construction, but simple operation and analysis.

QCM Measures Single-Shot Mass Ablation Rates With High Accuracy QCM: Quartz Crystal Microbalance  Measures the drift in oscillation frequency of the quartz crystal.  QCM has extreme mass sensitivity: to g/cm 2.  Time resolution is < 0.1 ms (each single shot).  Quartz crystal is inexpensive. It can be detached after several shots. Composition of the ablated ejecta can be analyzed by surface examination.

Composition of Ejecta Can Be Measured with RGA  Ejecta spectrum can be measured to better than 1 ppm.  Time resolution is ~1 ms (each single shot).  Inexpensive, commercially available diagnostics. RGA: Residual Gas Analyzer is a mass spectrometer. 1) Repeller 2) Anode Grid 3) Filament 4) Focus Plate

Laser propagation and Breakdown experiment setup Spectroscopy Can Identify the Ejecta Constituents Near the Sample Acton Research SpectraPro 500i Focal Length: 500 mm Aperture Ratio: f/6.5 Scan Range: 0 to 1400-nm mechanical range Maximum resolution: 0.04 nm Grating size: 68x68 mm in a triple-grating turret Gratings: 150g/mm, 600g/mm, 2400g/mm

Laser Interferometry Can Measure the Velocity History of the Target Surface  Time resolution of 0.1 to 1 ns.  Accuracy is better than 1%-2% for velocities up to 3000 m/s.  Measuring velocity histories of the front and back surfaces of the target allows to calculate the thermal and mechanical stresses inside it. VISAR: Velocity Interferometer System for Any Reflector  Measures the motion of a surface

Three Laser Pulses Can Simulate the Complete Surface Temperature Evolution Time (  s) Laser 0.24 J/cm 2,10 ns Gaussian pulse 0.95 J/cm 2,1  s Rectangular pulse 0.75 J/cm 2,1.5  s Rectangular pulse Time (  s) 20  m depth Wall surface NRL Target, X-ray and Ions