1. September 24-25, 2003 HAPL meeting, UW, Madison 1 Armor Configuration & Thermal Analysis 1.Parametric analysis in support of system studies 2.Preliminary scoping analysis of the use of a porous armor layer A. René Raffray UCSD HAPL Program Meeting University of Wisconsin, Madison September 24-25, 2003

2. HAPL meeting, UW, Madison 2 Integrated Chamber Armor/FW/Blanket Analysis Required for Chamber System Studies Chamber engineering constraints are set by limits on maximum temp. and cyclic temperature behavior of armor (W) and of structural material (ferritic steel), which depend on: IFE system parameters –e.g. yield, rep rate, chamber size, protective gas density Chamber first wall and blanket design parameters for example configuration -e.g. coolant inlet and outlet temperatures, first wall structural material thickness, armor thickness and properties (including engineered materials) and heat transfer coefficient at coolant Use RACLETTE-IFE code in conjunction with photon and ion energy deposition models to provide series of runs to be used as input data for system studies -Update code to include a second layer in the geometry for modeling W + FS wall with a convective boundary condition at the coolant interface -Add capability to model over many cycles -Compare with other modeling results for consistency Coolant FS W q

3. September 24-25, 2003 HAPL meeting, UW, Madison 3 Example Results Comparing W Temperature Histories for Armor Thicknesses of 0.05 mm and 0.5 mm, respectively 154 MJ yield No gas Rep Rate =10 R chamber = 6.5 m  FS = 2.5mm T coolant = 500°C  W =0.05mm  W =0.5mm Not much difference in maximum W temperature and in number of cycles to ramp up to the maximum temperature level Coolant (h) FS W q

4. September 24-25, 2003 HAPL meeting, UW, Madison 4 Example Results Comparing FS Temperature Histories for W Armor Thicknesses of 0.05 mm and 0.5 mm, respectively 154 MJ yield No gas Rep Rate =10 R chamber = 6.5 m  FS = 2.5mm T coolant = 500°C Substantial differences in max. T FS and cyclic  T FS at FS/W interface depending on  W Can adjust T max by varying T coolant and h coolant Design for separate function and operating regime: -armor function under cyclic temperature conditions -structural material, coolant and blanket operation designed for quasi steady-state  W =0.05mm  W =0.5mm

5. September 24-25, 2003 HAPL meeting, UW, Madison 5 Maximum T W, T FS,  T FS as a Function of Armor Thickness for Example Parameters Must be integrated with chamber system modeling for consistent overall blanket and armor design parameters For given IFE conditions and chamber parameters, set maximum possible  W (to minimize cyclic  T FS and FS T max and provide lifetime margin) that would accommodate: -maximum allowable T W -fabrication Maximum W temperature is virtually constant over range of armor thicknesses, ~ 3050°C

6. September 24-25, 2003 HAPL meeting, UW, Madison 6 Procedure for Parametric Armor Analysis Utilize consistent parameters from steady state parametric study of example blanket/FW/power cycle configuration (FS/Li/Brayton Cycle) -parameters evolved on the basis of maximizing cycle efficiency while accommodating max. allowable T FS (~800°C for ODS FS) and T FS/Li (~600°C) -T coolant, convective heat transfer coefficient, and FS thickness set 1-mm W thickness assumed for analysis -maintain  T FS <~20° C for example cases -also applicable for higher energy density cases as increasing the W thickness in the range of ~1 mm has only a ~10°C effect on the max. T W -could be regarded as a mid-life or end of life scenario also For given fusion power from blanket analysis, calculate combination of yield, chamber radius and protective gas density which would maintain max. T W < assumed limit (2400 °C) -Utilize D. Haynes/J. Blanchard’s approximation to account for gas attenuation -Reduction in photon/burn ion/debris ion of 9%/1%/29% for 10mtorr Xe and R=6.5 m -Reduction of 16%/2%/48% for 20mtorr Xe and R=6.5 m -Conservative assumption: shift ion energy spectrum correspondingly -Heat in gas reradiated to surface over time 300-700  s

7. September 24-25, 2003 HAPL meeting, UW, Madison 7 Summary of Armor Parametric Results for a Fusion Power of 1800 MW These results are used as input in the system code in combination with results from the blanket/FW/cycle parametric analysis for the given fusion power Example target survival constraints based on allowable q’’ for case with 100  m 10% dense foam and 4000 K Xe (& 16 K target)

8. September 24-25, 2003 HAPL meeting, UW, Madison 8 Summary of Armor Parametric Results for a Fusion Power of 3000 MW

9. September 24-25, 2003 HAPL meeting, UW, Madison 9 Scoping Study of Thermal Performance of Armor with a Porous Layer -PPI plans to develop nano-scaled engineered W for armor applications as part of current SBIR Phase I grant Work with PPI to help optimize material microstructure characteristics (e.g. microstructure characteristic dimension, porosity, pore sizes, heterogeneity) –Minimize resistance to migration and release of implanted He –Provide adequate heat transfer performance –Use RACLETTE-IFE with adjusted material property data and energy deposition input to help understand impact on integrated chamber armor/FW/blanket system

10. September 24-25, 2003 HAPL meeting, UW, Madison 10 Ion Energy Deposition as a Function of Penetration Depth for a W Armor with a 10  m Porous Layer Maximum energy deposition decreases and energy penetration depth increases with increasing porosity of the porous layer

11. September 24-25, 2003 HAPL meeting, UW, Madison 11 Ion Energy Deposition as a Function of Penetration Depth for a W Armor with a 10  m Porous Layer For these scoping calculations, fully dense k and  of W scaled to density of porous region Maximum armor temp. increases appreciably with increasing porosity but not with porous region thickness past ion penetration depth (<10  m) Important to minimize porosity of porous region but there is flexibility in setting its thickness Porous region might reduce peak thermal stresses on armor and allow for higher max. temp. limits

12. September 24-25, 2003 HAPL meeting, UW, Madison 12 Assessing Relative Effects of Decrease in Thermal Conductivity and Density and Change in Ion and Photon Energy Deposition Profile in Porous Region Effect on max. T W of decrease in k in porous region dominates opposite effect due to broadening of energy deposition Similar results for different thicknesses of porous region (10 and 100  m)

13. September 24-25, 2003 HAPL meeting, UW, Madison 13 Conclusions Scoping study of thermal performance of porous armor region has been performed -Max. T W dependent on porosity of porous region but virtually not on its thickness (past energy deposition depth) -Effect of lower thermal conductivity of porous region outweighs counterbalancing effect of energy deposition spread in porous region -Optimization of porous material based on providing least resistance to migration of implanted He ions while accommodating maximum W temperature constraint (i.e. providing acceptable heat transfer performance) Parametric study of armor performed to provide input for initial system studies -W thickness affects  T FS at FS/W interface but virtually not max. T W - Design armor based on transient conditions and FW and blanket based on quasi steady-state conditions -Study has yielded combination of yield, chamber radius and protective gas density which would maintain max. T W < assumed limit (2400 °C) for different fusion powers and consistent blanket/FW/cycle parameters