threat spectra calculations for hapl chamber first wall
DESCRIPTION
Threat Spectra Calculations for HAPL Chamber First Wall Greg Moses, John Santarius, and Milad Fatenejad HAPL Team Meeting Princeton Plasma Physics Laboratory October 27-28, 2004. Progress on Three Modeling Issues. Threat spectra target source computed by BUCKY. - PowerPoint PPT PresentationTRANSCRIPT
Threat Spectra Calculations for HAPL Chamber First Wall
Greg Moses, John Santarius, and Milad Fatenejad
HAPL Team Meeting
Princeton Plasma Physics Laboratory
October 27-28, 2004
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Progress on Three Modeling Issues
• Threat spectra target source computed by BUCKY. Fluid approximation not valid (TOFE ’04).
Hybrid fluid-kinetic approximation.
• Ion threat time of flight transport to first wall and deposition in wall computed by BUCKY. Temporal prediction of ion threat at the first surface in BUCKY
improved (piece-wise continuous model replaces discrete model.) Model verified.
• Chamber—first wall integrated calculation computed by BUCKY. Replace two region model with integrated e.o.s. and conductivity
models. Modifications completed.
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30 32 34 36 38 40Timens0
5
10
15
20
enoZsuidarmm DT
vapor
DTice
CHDTmix
CH
Au
For the Examination of Long Mean Free Path Effects,
the Time Near Ignition Will Be the Focus
Lagrangian constant-mass zones from BUCKY run of HAPL case
• Ignition occurs at ~34.6 ns.
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104 103 102 101 100
Radiuscm102
103
104
105
106
erutare
pme
TVe
Time 34.592 ns
Ti
Ti
Te Te
DTvapor
DTice
CHDTmix
CH
Au
104 103 102 101 100
Radiuscm107
105
103
101
101
103
ssaM
ytisne
dgmc3 Time 34.592 ns
DTvapor
DTice
CHDTmix
CH
Au
104 103 102 101 100
Radiuscm0
2 108
4 108
6 108
8 108
1 109
diul
Fytic
olevmcs
Time 34.592 ns
DTvapor
DTice
CHDTmix
CH
Au
• Each point represents a Lagrangian zone of constant mass.
DT Core, DT-CH Shock, and CH-Au ShockWill Exemplify the Issues
34.55 34.56 34.57 34.58 34.59 34.6Timens1015
1016
1017
1018
evitalu
mu
Cn
ortue
ndleiy
• Neutrons get produced within ~30 ps.
DT-CH
CH-Au
DT-Core
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DTCore
rshock (cm) < 0.001
rshock (cm) < 0.001
vshock (cm/s) 6.6 x 106
ni (cm-3) 1.5 x 1026
Ti (keV) 276
Te (keV) 72
Ave. charge state 1
rshock / mfp > 1000
DTCore
DT-CHShock
rshock (cm) < 0.001 0.026
rshock (cm) < 0.001 0.02
vshock (cm/s) 6.6 x 106 5.5 x 108
ni (cm-3) 1.5 x 1026 5.1 x 1024
Ti (keV) 276 86
Te (keV) 72 47
Ave. charge state 1DT 1CH 1
rshock / mfp > 1000 1.1
DTCore
DT-CHShock
CH-AuShock
rshock (cm) < 0.001 0.026 1.1
rshock (cm) < 0.001 0.02 0.004
vshock (cm/s) 6.6 x 106 5.5 x 108 8.6 x 107
ni (cm-3) 1.5 x 1026 5.1 x 1024 5.0 x 1018
Ti (keV) 276 86 2.8
Te (keV) 72 47 0.69
Ave. charge state 1DT 1CH 1
CH 1Au 36
rshock / mfp > 1000 1.1 0.001
At 34.592 ns, the DT-CH Shock Thickness andIncoming Ion Mean Free Paths Become Comparable
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34.58 34.585 34.59 34.595 34.6Timens0
100
200
300
400
500
ygre
nEVek
Ei
Hydrodynamic prediction of ion energy in shock frame
34.58 34.585 34.59 34.595 34.6Timens0
100
200
300
400
500
ygre
nEVek
Ei
Ei
Hydrodynamic prediction of ion energy in shock frame
Actual energy gained by ion
By 30 ps after Ignition, DT-CH Shock WaveIs Ineffective at Transferring Energy
34.58 34.585 34.59 34.595 34.6Timens0.1
0.2
0.5
1
2
5
10
kco
hS
ssenkci
htnaeM
eerfhta
p
• Ignition begins at ~34.56 ns.
• Mean-free path calculations includeion-ion collisions and ion-electron drag.
• shock / mfp ratio quickly falls.
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Implications for HAPL Ions
• Hydrodynamic assumption of perfect momentum transfer between Lagrangian zones fails after ~25 ps.
• By ~40 ps after ignition, ions in the shock wave are free streaming.
• Energy spectrum of ions hitting the first wall will be of lower energy than estimated by purely hydrodynamic codes.
Effect is being evaluated using the Icarus (SNL) Discrete Simulation Monte Carlo (DSMC) computer code.
UW 1-D radiation hydrodynamics code, BUCKY, will be modified to predict the HAPL ion energy spectrum.
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Icarus mesh for the HAPL problem.
ne Step 1
0200
400600
8001000
Zm0
200400
600800
1000
Rm51026
1 1027
1.51027
0200
400600
8001000
Zm
Initial electron density
UW is Simulating Target Explosions Using the Icarus Direct Simulation Monte Carlo (DSMC) Code
0 0.2 0.4 0.6 0.8 1Zmm0
0.2
0.4
0.6
0.8
1
Rmm
ne Step 1
020
4060
80100
Zm0
2040
6080
100
Rm51026
1 1027
1.51027
020
4060
80100
Zm• Code written by Dr. Tim Bartel, SNL.
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Ion threat time of flight transport to first wall and deposition in wall computed by BUCKY.
• Temporal prediction of ion threat at the first surface improved (piece-wise continuous model replaces discrete model.) BUCKY results reproduced in “stand-alone” simulation
and compared to new model.
Further testing and comparisons.
Implementation in BUCKY with verification and validation.
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Select a portion of the HAPL ion spectrum to simulate using new model
•Ion energies between 150 keV and 5 MeV
104 103 102 101 100
Radiuscm0
2 108
4 108
6 108
8 108
1 109di
ulF
yticolevmcs
Time 34.592 ns
DTvapor
DTice
CHDTmix
CH
Au
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Discrete ion spectrum
Initial ion distribution < 0.5 cm
Outermost ions have highest velocities. Time-of-flight spreading widens pulse length at first wall.
0 s 0.3 microsecFirst wall
6.5 m
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Discrete ion spectrum(2)
0.6 microsec 0.9 microsec
1.2 microsec 1.5 microsec
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Discrete ion spectrum(3)
1.8 microsec 2.1 microsec
2.4 microsec 2.7 microsec
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Continuous ion spectrum
0. s 0.3 microsec
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Continuous ion spectrum(2)
0.6 microsec 0.9 microsec
1.2 microsec 1.5 microsec
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Continuous ion spectrum(3)
1.8 microsec 2.1 microsec
2.4 microsec 2.7 microsec
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Surface temperature vs. time for discrete and piece-wise continuous ion spectrums
Time (arbitrary units)
Tem
pera
ture
(ar
bitr
ary
units
)Time integrated source is the same for both curves.
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Chamber and first wall integrated calculation computed by BUCKY.
Replace two region model with single region model with integrated equation of state and conductivity for plasma and solid state materials.
Radiation hydrodynamics, plasma properties
Heat conduction, solid state properties.
Two different models communicate across boundary.
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Future work in threat spectra task
• Perform DSMC analysis of long mean-free path ions and modify hydrodynamic model.
• Verify and validate BUCKY for new models.
• Continue with improved simulations for HAPL reactor design.
• Continue to interface with wall response simulations and cavity clearing simulations.