A. R. Raffray, J. Pulsifer, M. S. Tillack, X. Wang

Slides:



Advertisements
Similar presentations
Stefan Roesler SC-RP/CERN on behalf of the CERN-SLAC RP Collaboration
Advertisements

Introduction to Plasma-Surface Interactions Lecture 6 Divertors.
Sandia National Laboratories is a multi-program laboratory managed and operated by Sandia Corporation, a wholly owned subsidiary of Lockheed Martin Corporation,
September 24-25, 2003 HAPL meeting, UW, Madison 1 Armor Configuration & Thermal Analysis 1.Parametric analysis in support of system studies 2.Preliminary.
Japan-US Workshop held at San Diego on April 6-7, 2002 How can we keep structural integrity of the first wall having micro cracks? R. Kurihara JAERI-Naka.
Assessment of Chamber Concepts for IFE Power Plants: The ARIES-IFE study Farrokh Najmabadi for the ARIES Team IFSA2001 September 9-14, 2001 Kyoto, Japan.
April 6-7, 2002 A. R. Raffray, et al., Modeling of Inertial Fusion Chamber 1 Modeling of Inertial Fusion Chamber A. R. Raffray, F. Najmabadi, Z. Dragojlovic,
Thermal Control Techniques for Improved DT Layering of Indirect Drive IFE Targets John E. Pulsifer and Mark S. Tillack University of California, San Diego.
In-Hohlraum Layering of Indirect Drive Targets Mark S. Tillack and John E. Pulsifer University of California, San Diego Dan T. Goodin and Ron W. Petzoldt.
IFSA, Kyoto, Japan, September Dry Chamber Wall Thermo-Mechanical Behavior and Lifetime under IFE Cyclic Energy Deposition A. R. Raffray 1, D. Haynes.
May 31-June 1, 2001 A. R. Raffray, et al., Assessment of Dry Chamber Walls as Preliminary Step in Defining Key Processes for Chamber Clearing Code 1 Assessment.
March 8, 2001 A. R. Raffray, et al., Assessment of Carbon and Tungsten Dry Chamber Walls under IFE Energy Depositions Assessment of Carbon and Tungsten.
April 4-5, 2002 A. R. Raffray, et al., Modeling Analysis of Carbon Fiber Velvet Tested in RHEPP Ion Beam Facility 1 Modeling Analysis of Carbon Fiber Velvet.
April 4-5, 2002 A. R. Raffray, et al., Chamber Clearing Code Development 1 Chamber Dynamics and Clearing Code Development Effort A. R. Raffray, F. Najmabadi,
Design Windows for IFE Chambers and Target Injection Farrokh Najmabadi for the ARIES Team US/Japan Workshop on Target Fabrication December 3-4, 2001 General.
April 10, 2002 A. R. Raffray, et al., Dynamic Chamber Armor Behavior in IFE and MFE 1 Dynamic Chamber Armor Behavior in IFE and MFE A. R. Raffray 1, G.
June7-8, 2001 A. R. Raffray, et al., Completion of Assessment of Dry Chamber Wall Option Without Protective Gas, and Initial Planning Activity for Assessment.
October 24, Remaining Action Items on Dry Chamber Wall 2. “Overlap” Design Regions 3. Scoping Analysis of Sacrificial Wall A. R. Raffray, J.
1 THERMAL LOADING OF A DIRECT DRIVE TARGET IN RAREFIED GAS B. R. Christensen, A. R. Raffray, and M. S. Tillack Mechanical and Aerospace Engineering Department.
ARIES-IFE: An Integrated Assessment of Chamber Concepts for IFE Power Plants Mark Tillack for the ARIES Team 19th IEEE/NPSS SOFE January 22-25, 2002 Atlantic.
Thermal Control Techniques for Improved DT Layering of Indirect Drive IFE Targets M.S. Tillack and J.E. Pulsifer University of California, San Diego D.T.
1 of 16 M. S. Tillack, Y. Tao, J. Pulsifer, F. Najmabadi, L. C. Carlson, K. L. Sequoia, R. A. Burdt, M. Aralis Laser-matter interactions and IFE research.
December 12-13, 2007/ARR 1 Power Core Engineering: Design Updates and Trade-Off Studies A. René Raffray University of California, San Diego ARIES Meeting.
January 8-10, 2003/ARR 1 1. Pre-Shot Aerosol Parameteric Design Window for Thin Liquid Wall 2. Scoping Liquid Wall Mechanical Response to Thermal Shocks.
Aug. 8-9, 2006 HAPL meeting, GA 1 Advanced Chamber Concept with Magnetic Intervention: - Ion Dump Issues - Status of Blanket Study A. René Raffray UCSD.
Nov 13-14, 2001 A. R. Raffray, et al., Progress Report on Chamber Clearing Code Effort 1 Progress Report on Chamber Clearing Code Development Effort A.
Highlights of ARIES-IFE Study Farrokh Najmabadi VLT Conference Call April 18, 2001 Electronic copy: ARIES Web Site:
Aug. 8-9, 2006 HAPL meeting, GA 1 Open Discussion on Advanced Armor Concepts Moderated by A. René Raffray UCSD HAPL Meeting GA, La Jolla, CA August 8-9,
M. Yoda, S. I. Abdel-Khalik, D. L. Sadowski and M. D. Hageman Woodruff School of Mechanical Engineering Extrapolating Experimental Results for Model Divertor.
April 9-10, 2003 HAPL Program Meeting, SNL, Albuquerque, N.M. 1 Lowering Target Initial Temperature to Enhance Target Survival Presented by A.R. Raffray.
Ion Beam Analysis of Gold Flecks in a Foam Lattice F E Gauntlett, A S Clough Physics Department, University of Surrey, Guildford, GU2 7XH, UK.
HAPL WORKSHOP Chamber Gas Density Requirements for Ion Stopping Presented by D. A. Haynes, Jr. for the staff of the Fusion Technology Institute.
ARR/April 8, Magnetic Intervention Dump Concepts A. René Raffray UCSD With contributions from: A. E. Robson, D. Rose and J. Sethian HAPL Meeting.
ISIS Target studies Could a used ISIS target provide fusion relevant irradiated tungsten material properties? Tristan Davenne 20 th May nd Radiate.
Calorimeter Analysis Tasks, July 2014 Revision B January 22, 2015.
Ion Beam Analysis of Gold Flecks in a Foam Lattice F E Gauntlett, A S Clough Physics Department, University of Surrey, Guildford, GU2 7XH, UK.
Z Machine Materials Studies November 14, 2001 Tina J. Tanaka, Greg Rochau, Tim Renk, Craig Olson (SNL), Tim Knowles (ESLI), Per Peterson (UCB), and Robert.
Recent Results from Dragonfire Armor Simulation Experiments Farrokh Najmabadi, Lane Carlson, John Pulsifer UC San Diego HAPL Meeting, Naval Research Laboratory.
/15RRP HAPL Dec 6, Robert R. Peterson Los Alamos National Laboratory and University of Wisconsin Calculations of the Response of Inertial Fusion.
J. Hasegawa, S. Hirai, H. Kita, Y. Oguri, M. Ogawa RLNR, TIT
July 11, 2003 HAPL e-meeting. 1 Armor Design & Modeling Progress A. René Raffray UCSD HAPL e-meeting July 11, 2003 (1)Provide Parameters for Chamber “System”
Materials Studies on Z (x-rays) and RHEPP (ions) C.L. Olson, T.J.Tanaka, T.J. Renk, G.A.Rochau, M.A. Ulrickson Sandia National Laboratories, Albuquerque,
Update on Roughening Work Jake Blanchard HAPL MWG Fusion Technology Institute University of Wisconsin e-meeting – July 2003.
1 US PFC Meeting, UCLA, August 3-6, 2010 DIONISOS: Upgrading to the high temperature regime G.M. Wright, K. Woller, R. Sullivan, H. Barnard, P. Stahle,
ERMSAR 2012, Cologne March 21 – 23, The Experimental Results of LIVE-L8B: Debris Melting Process in a Simulated PWR Lower Head X. Gaus-Liu, A. Miassoedov,
Status of HAPL Tasks 1 & 3 for University of Wisconsin Gregory Moses Milad Fatenejad Fusion Technology Institute High Average Power Laser Meeting September.
Modeling of Surface Roughening M. Andersen, S. Sharafat, N. Ghoniem HAPL Surface-Thermomechanics in W and Sic Armor UCLA Workshop May 16 th 2006.
Temperature Response and Ion Deposition in the 1 mm Tungsten Armor Layer for the 10.5 m HAPL Target Chamber T.A. Heltemes, D.R. Boris and M. Fatenejad,
Effect of Re Alloying in W on Surface Morphology Changes After He + Bombardment at High Temperatures R.F. Radel, G.L. Kulcinski, J. F. Santarius, G. A.
M. Yoda, S. I. Abdel-Khalik, D. L. Sadowski, B. H. Mills and M. D. Hageman G. W. Woodruff School of Mechanical Engineering Correlations for Divertor Thermal-Hydraulic.
If information seems to be missing, make any reasonable assumptions. 1.A target has an areal density of 2.3 g/cm 2 and a thickness of 0.8 inch. What is.
Engineered-material exposure in Dragonfire – Progress Report Farrokh Najmabadi, Lane Carlson, UC San Diego HAPL Meeting, UW Madison October 22-23, 2008.
Ion Mitigation for Laser IFE Optics Ryan Abbott, Jeff Latkowski, Rob Schmitt HAPL Program Workshop Atlanta, Georgia, February 5, 2004 This work was performed.
TUTORIAL 1 7/3/2016.
Neda HASHEMI Gaëtan GILLES Rúben António TOMÉ JARDIN Hoang Hoang Son TRAN Raoul CARRUS Anne Marie HABRAKEN 2D Thermal model of powder injection laser cladding.
Modeling of Z-Ablation I. E. Golovkin, R. R. Peterson, D. A. Haynes University of Wisconsin-Madison G. Rochau Sandia National Laboratories Presented at.
350 MJ Target Thermal Response and Ion Implantation in 1 mm thick silicon carbide armor for 10.5 m HAPL Chamber T.A. Heltemes and G.A. Moses Fusion Technology.
Date of download: 7/7/2016 Copyright © ASME. All rights reserved. From: Thermal Conductivity of Turbostratic Carbon Nanofiber Networks J. Heat Transfer.
Chopper Beam Dump Thermal Problem 10/27/20101PX Linac FE Technical Discussions.
Exposures of Candidate First Wall Materials
BUCKY Simulations of Z and RHEPP Experiments
Modelling of Frost Formation and Growth on Microstuctured Surface
First thermal calculations on the target made of aluminium
Trade-Off Studies and Engineering Input to System Code
Modified Design of Aries T-Tube Divertor Concept
University of California, San Diego
IFE Wetted-Wall Chamber Engineering “Preliminary Considerations”
University of California, San Diego
Aerosol Production in Lead-protected and Flibe-protected Chambers
First Wall Response to the 400MJ NRL Target
Presentation transcript:

Modeling Analysis of Carbon Fiber Velvet Tested in RHEPP Ion Beam Facility A. R. Raffray, J. Pulsifer, M. S. Tillack, X. Wang University of California, San Diego With input from T. Knowles (ESLI) and T. Renk (SNL) HAPL Review GA, San Diego April 4-5, 2002 April 4-5, 2002 A. R. Raffray, et al., Modeling Analysis of Carbon Fiber Velvet Tested in RHEPP Ion Beam Facility

Energy Deposition as a Function of Penetration Depth in Carbon Flat Wall Under RHEPP Ion Spectra • Ion Beam data obtained from T. Renk in terms of time, voltage and current density for each ion - 5.11x104 J/m2 - Energy Split: - 16% H+ - 26% C++ - 57% C+ • Energy deposition computed as a function of penetration depth for given ion spectra based on SRIM stopping power data April 4-5, 2002 A. R. Raffray, et al., Modeling Analysis of Carbon Fiber Velvet Tested in RHEPP Ion Beam Facility

How Does the RHEPP Energy Deposition Compares with the 154 MJ DD Target Spectra Case for R=6.5 m? • Energy Deposition fromRHEPP dominated by C ions • Energy deposition from DD target spectra dominated by deuterium and tritium ions • C and H ions have different penetration depths and energy deposition profiles • RHEPP reproduces the debris ion energy deposition level and penetration depth within a factor of 2 April 4-5, 2002 A. R. Raffray, et al., Modeling Analysis of Carbon Fiber Velvet Tested in RHEPP Ion Beam Facility

Volumetric Heat Generation as a Function of Space and Time in Carbon Flat Wall Under RHEPP Ion Spectra April 4-5, 2002 A. R. Raffray, et al., Modeling Analysis of Carbon Fiber Velvet Tested in RHEPP Ion Beam Facility

Temperature History for Carbon Flat Wall Under RHEPP Ion Spectra • Updated sublimation model for C from Philipps’ recommendation • IFE reactor-like CFC thermal conductivity as a f(T) (~235 W/m-K for T >1800 °C) - Max. Temp. 4370°C - Corresponding sublimated thickness calculated as ~ 0.032 mm per shot for 5.1x104 J/m2) • Measurement from T. Renk on POCO Graphite ~20 mm after 75 shots, ~0.27 mm per shot for 5.5x104 J/m2 • Not clear what grade of POCO graphite was used but k would be much lower April 4-5, 2002 A. R. Raffray, et al., Modeling Analysis of Carbon Fiber Velvet Tested in RHEPP Ion Beam Facility

Maximum C Temperature and Sublimation Loss per Shot as a Function of Energy Density and kcarbon for Same RHEPP Ion Energy Level • Sublimation model from Philipps’ data derived for T<4000K • As expected, thermal conductivity plays a key role and it is possible to sublimate ~1 mm per shot at energy density of 4 x104 J/m2 if k < 100 W/m-K • POCO graphite seems to have low k and would be a poor material to validate CFC grade armor • It is very important to conduct experiments on well characterized material and with good diagnostics (surface T and mass loss) April 4-5, 2002 A. R. Raffray, et al., Modeling Analysis of Carbon Fiber Velvet Tested in RHEPP Ion Beam Facility

Carbon Fiber: Geometry Model ESLI fiber characteristics Fiber length 2500mm Fiber diameter 6.5mm Fiber k ~100-200 W/m-K 1.5% fiber volume fraction 98.5% void fraction Fiber separation, y 47mm yeff 215mm April 4-5, 2002 A. R. Raffray, et al., Modeling Analysis of Carbon Fiber Velvet Tested in RHEPP Ion Beam Facility

Carbon Fiber: Energy Deposition Model • Penetration depth set as a function of location in fiber based on angle of incidence and including shadowing effect from upstream fibers • Energy deposition calculated as a function of penetration depth and including angle effect which effectively increase the area seeing the ion flux April 4-5, 2002 A. R. Raffray, et al., Modeling Analysis of Carbon Fiber Velvet Tested in RHEPP Ion Beam Facility

Results for Carbon Fiber Under RHEPP Ion Spectrum Angle Max. Temp.(°C) Avg. Fract. Subl. Loss Left Right Fiber Tip Overall. 0° 4390 4390 1* 0.015 5.2° 4092 4352 0.43 0.0065 10° 4170 4292 0.31 0.0046 20° 4213 4041 0.15 0.0023 * Fractional sublimation loss of 1 is equivalent to ~0.032mm per shot • Sublimation loss for fiber based on temperature distribution at tip • Major difference with flat plate is very low density of fiber (0.015) • In agreement with post-experimental examination of fiber showing no visible ablation or loss of material Temperature Contour at Time Corresponding to Tmax for 10° Case April 4-5, 2002 A. R. Raffray, et al., Modeling Analysis of Carbon Fiber Velvet Tested in RHEPP Ion Beam Facility

Concluding Remarks from Fiber Analysis • Difficult to model flat POCO graphite case in the absence of fully characterized property data and temperature surface temperature measurement - Need to use actual material or material closely-ressembling (in properties) reactor grade armor - Need to fully characterized material properties - Need to conduct experiments with adequate diagnostics • Based on the fiber model (and consistent with experimental observation), much less material is ablated from the fiber - Incidence angle effect on local sublimation - More importantly, fiber density effect on total sublimation April 4-5, 2002 A. R. Raffray, et al., Modeling Analysis of Carbon Fiber Velvet Tested in RHEPP Ion Beam Facility