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Status of HAPL Tasks 1 & 3 for University of Wisconsin
Gregory Moses
Milad FatenejadFusion Technology Institute
High Average Power Laser Meeting
September 24-25, 2003
Madison, WI
Numbers
010010101101011100010101010101010100101011010010110001010100101001010101010101010010100100000100101100110001001001000001111101000100100101010010101010001001010101010001000010111010100101001000101111011001010001010101001010001010100100111010010101100100101001000101010010101110100100101010010101100101010101010001010101011010100101010101001010011001001010101010101010110010100101001011100101000001100110011010101100110010101010101010100101010100100100101010110100010100111101010101001010010100010010101101011011001010010100101010101010010101001000010001010101010001010111101010101010010101
Outline
• BUCKY-ANSYS coupling (Task 3)– Task 3—couple BUCKY output to ANSYS input so
that a large number of cases can be examined in a short time using CONDOR
• Modeling target ion threat spectrum for chamber response studies (Task 1)– Task 1—simulate target output spectra with BUCKY
and improve underlying models to more reliably compute threat spectra
• Energy spectrum• Time of arrival
Task 3 -- Stress Analysis
BUCKY target
simulation- implosion,
burn, explosion
BUCKYchamber simulationincluding
wall response
BUCKYchamber simulation
withoutwall response
Vaporization, wall temperature history
Heating rate density q(r,t)
ANSYS thermalstress simulation
Stress/fatigue design criteria
New capability
Old capability
Stress analysis
RRP
Task 1 -- Modeling target ion threat spectrum
• Historical reminder of Carbon wall analysis– HAPL Meeting December 2002– HAPL Meeting April 2003
BUCKY simulations of chamber response allow the prediction of first wall surface temperature evolution.
• Roughly speaking, there are three peaks in the first wall temperature:
1) A response to the prompt, unattenuated x-rays hitting the wall (heating it practically volumetrically, in the case of a graphite first wall).
2) Response to soft xrays re-radiated after the Xe slows and captures the least penetrating ions.
3) Bursts of temperature rise as the unstopped ions strike the wall. This effect is somewhat exaggerated in these simulations due to the coarse binning of the ion spectum.
Surface Temperature Evolution, 80mTorr Xe,
650cm radius graphite wall, PD_EOSOPA target
1000
1500
2000
2500
3000
3500
1.E-08 1.E-07 1.E-06 1.E-05
Time (s)
Su
rfac
e T
em
pe
ratu
re (
C)
1
2
3
D. Haynes, HAPL Dec 2002
Ion binning: For compatibility with earlier studies, ion spectra were divided into 15 energy bins. This led to an overestimatein the temperature rise due to ions.
•Increasing the detail in the reproduction until the wall response converges indicates that this led to an conservative definition of the operating window.
Deuterium ion binning effect on simulated wall response
0.10
0.12
0.14
0.16
0.18
0.20
0.22
0.24
0.26
1.E-07 2.E-06 4.E-06 6.E-06 8.E-06
Time (s)
Tem
pera
ture
(eV
)
Coarse binning
Resolvedbinning
Though brief, the spurious temperature excursions can lead to
unphysical mass loss or melting.
However:
500C
D. Haynes, HAPL Apr 2003
Conclusions
•Two approximations in previously reported BUCKY/CONDOR studies were examined:
•Looking only at shot 1 underestimated the starting temperature of the armor surface; and,
•Coarse binning of ion spectrum overestimated mass loss.
•These two approximations compensated for each other, at least for the carbon wall case considered.
•Thus, operating windows previously reported for C walls are still in force through serendipity.
•Yield was added as a dimension in the space of chamber design parameters.
•A single figure of merit for ion deposition effects needs to be carefully applied, as differences in spectrum change temperatures and gradients within the wall.
•Two approximations in previously reported BUCKY/CONDOR studies were examined:
•Looking only at shot 1 underestimated the starting temperature of the armor surface; and,
•Coarse binning of ion spectrum overestimated mass loss.
•These two approximations compensated for each other, at least for the carbon wall case considered.
•Thus, operating windows previously reported for C walls are still in force through serendipity.
•Yield was added as a dimension in the space of chamber design parameters.
•A single figure of merit for ion deposition effects needs to be carefully applied, as differences in spectrum change temperatures and gradients within the wall.
D. Haynes, HAPL Apr 2003
Ion Debris Spectra
Ion Energy (eV)
#o
fIo
ns
103 104 105 106 107
1016
1017
1018
1019 DTHCPdHeHe - burn
Pd Layered TargetEOSOPA
Each ion spectrum approximated by 15“representative” energies
Ion heating source is not temporally resolved
Volumetric Heating Rate vs Cycle (zone 2)
1.00E+10
1.00E+11
1.00E+12
1.00E+13
1.00E+14
1.00E+15
1
2040
4079
6118
8157
1019
6
1223
5
1427
4
1631
3
1835
2
2039
1
2243
0
2446
9
2650
8
2854
7
3058
6
Cycle
Vo
lum
etri
c H
eati
ng
Rat
e (W
/cc)
~1-10 sTime of flightto first wall
Increase “resolution” of spectrum
Volumetric Heating Rate vs Cycle (Zone 1 - n energies)
1.00E+03
1.00E+05
1.00E+07
1.00E+09
1.00E+11
1.00E+13
1.00E+15
1
1494
2987
4480
5973
7466
8959
1045
2
1194
5
1343
8
1493
1
1642
4
1791
7
1941
0
2090
3
2239
6
2388
9
2538
2
2687
5
2836
8
2986
1
Cycle
Vo
lum
etri
c H
eati
ng
Rat
e (W
/cc)
Volumetric Heating Rate vs Cycle (Zone 1 - 2*n energies)
1.00E+03
1.00E+04
1.00E+05
1.00E+06
1.00E+07
1.00E+08
1.00E+09
1.00E+10
1.00E+11
1.00E+12
1.00E+13
1.00E+14
1
1381
2761
4141
5521
6901
8281
9661
1104
1
1242
1
1380
1
1518
1
1656
1
1794
1
1932
1
2070
1
2208
1
2346
1
2484
1
2622
1
2760
1
2898
1
Cycle
Vo
lum
etri
c H
eati
ng
Rat
e (W
/cc)
15 representative ions 30 representative ions
Future plans
• We are now capable of doing large parameter sweeps involving complex lengthy calculations. Hands-off analysis.
• We must focus on correctly doing the right calculations.
• Need better characterization of x-ray and ion spectra for all ions and relevant target designs. (Target threat group?).