target threat spectra gregory moses and john santarius fusion technology institute university of...
DESCRIPTION
“Conventional” target chamber simulation Time of flight spreading as ions reach wall leads to coarse finite particle approximation E N Ion energy distribution sampled at discrete energies E i Target explosion Split particles at R* to give resolution as they impinge on first wallTRANSCRIPT
Target threat spectra
Gregory Moses and John SantariusFusion Technology Institute
University of Wisconsin-Madison
HAPL Review MeetingMarch 3-4, 2005
Naval Research LabWashington DC
Outline
• Target debris transport to wall modeling– Monte Carlo “splitting” algorithm implemented
• Bounding threat spectra calculations– NRL meeting on December 9, 2004– Pure hydro calculation– Long mean free path calculation
• BUCKY explosion simulations
“Conventional” target chamber simulation
Time of flight spreading asions reach wall leads to coarsefinite particle approximation
E
N
Ion energy distribution sampled at discrete energies Ei
Target explosion
Split particles at R* to giveresolution as they impingeon first wall
Target debris transport to wall: wall surface temperature for different splitting parameters
0 0.5 1 1.5 2 2.5
x 10-6
0.1
0.15
0.2
0.25
Time (s)
Tem
pera
tue
(eV
)
Wall Surface Temperature vs Time
No splitting10:1 splitting100:1 splitting
160 MJ NRL target50 mTorr Xe gas6.5 m radius
Bounding threat spectra calculations
• Meeting at NRL on Dec 9, 2004– Post-burn exploding target has ion mean free
path “issues” that potentially reduce the shock acceleration of the plasma debris.
– HANE experiments and theory are relevant to these issues. Instabilities could produce effective collisionality that “re-validates” hydrodynamics model. (Ref: R. Clark, et. al.)
– First step: bounding calculations with models currently in BUCKY.
Bounding threat spectra calculations High collisionality – pure hydrodynamic
Bounding threat spectra calculations High collisionality – pure hydrodynamic
Bounding threat spectra calculations High collisionality – pure hydrodynamic
4x108 cm/s
Wave-Particle Interactions May Cause theHydrodynamic Approximation to Remain Valid
• This mechanism was pointed out by NRL during the NRL/UW physics meeting on Dec. 9.
• Instabilities and wave-particle interactions caused hydrodynamics to be a good approximation for the HANE experiments.
• Bob Clark’s poster at this meeting, based on HANE program research during the 1970’s, very nicely summarizes the potential instabilities and coupling mechanisms.
• Work has begun on this mechanism for HAPL.– Caveat: Devil is in the details, and the problem is very difficult.
• Each point represents a Lagrangian zone of constant mass.
Shock Parameters at 34.586 ns (Ignition Plus ~20 ps)Show That the Shock Has Reached r = 0.02-0.03 cm
Ener
gy (k
eV)
Bounding threat spectra calculations Low collisionality – kinetic fast ions
Hydrodynamic calculation of ion
energy in shock frame
Kinetic calculation of energy gained by ion
• At ~34.586 ns, hydrodynamic and kinetic energy deposition calculations begin to diverge.
• A separate BUCKY calculation will stream the shock ions through the ambient plasma.
DT-CH shock
Expanding Au
Maxwellian DT core
Expanding DT-CH
“Conventional” chamber simulations
• For low Xe pressure the gas volumetrically heats, there is little hydrodynamic motion– 50-50% split between plasma deposition and
wall deposition for target debris at 50 mTorr.• The wall temperature response is most
sensitive to ion stopping models and Xe opacity in 10-1,000 eV range.– Ion stopping model determines prompt heat input– Opacity determines gas re-radiation time
BUCKY explosion simulations160 MJ NRL Target Ionic Debris Deposition in 50 mTorr Xe
-5
0
5
10
15
20
25
0 1000 2000 3000 4000 5000
Time (ns)
Ene
rgy
depo
site
d (M
J)
Plasma(MJ)
Wall(MJ)
Summary
• New debris transport model developed and working. Next step:– Review ion-stopping model and opacity theory– Do simulations
• Spartan initial conditions• Xe vs. Ar
• Bounding calculations– Pure hydrodynamic calculation working– Kinetic calculation in progress– Next step: Evaluate HANE literature