S.Yu.Gus’kov. LPI RAS Fast Ignition by Detonating Hydrodynamic Flow S.Yu. Gus’kov *, M. Murakami...
-
Upload
prudence-baker -
Category
Documents
-
view
232 -
download
0
Transcript of S.Yu.Gus’kov. LPI RAS Fast Ignition by Detonating Hydrodynamic Flow S.Yu. Gus’kov *, M. Murakami...
![Page 1: S.Yu.Gus’kov. LPI RAS Fast Ignition by Detonating Hydrodynamic Flow S.Yu. Gus’kov *, M. Murakami ** * P.N. Lebedev Physical Institute of Russian Academy.](https://reader035.fdocuments.in/reader035/viewer/2022062520/5697c0111a28abf838ccbd78/html5/thumbnails/1.jpg)
S.Yu.Gus’kov. LPI RAS
Fast Ignition by Detonating Hydrodynamic Flow
S.Yu. Gus’kov*, M. Murakami**
*P.N. Lebedev Physical Institute of Russian Academy of Sciences, Moscow, Russia
**Institute of Laser Engineering. Osaka University. Japan
7-th Direct Drive and Fast Ignition Workshop. May 3-6, 2009. Prague
Contents:
1. Fast ignition by hydrodynamic flow
2. Fast ignition by detonating hydrodynamic flow - “target from target” ignition
3. Conclusion: Practicability of fast ignition at the impactor velocity of 300-500 km/s
![Page 2: S.Yu.Gus’kov. LPI RAS Fast Ignition by Detonating Hydrodynamic Flow S.Yu. Gus’kov *, M. Murakami ** * P.N. Lebedev Physical Institute of Russian Academy.](https://reader035.fdocuments.in/reader035/viewer/2022062520/5697c0111a28abf838ccbd78/html5/thumbnails/2.jpg)
S.Yu.Gus’kov. LPI RAS
Fast ignition by hydrodynamic flow
![Page 3: S.Yu.Gus’kov. LPI RAS Fast Ignition by Detonating Hydrodynamic Flow S.Yu. Gus’kov *, M. Murakami ** * P.N. Lebedev Physical Institute of Russian Academy.](https://reader035.fdocuments.in/reader035/viewer/2022062520/5697c0111a28abf838ccbd78/html5/thumbnails/3.jpg)
Fast Ignition Drivers
Igniting Drivers:
Fast particles from laser-produced plasma
• electrons (Ee ~ 0.5-1.5 MeV)
• light ions (Ei ~ 10 -100 MeV/nuclon)
Laser : IL > 1019 W/cm2, L< 10-20 ps.
Experiments: CD-target + cone
RAL (UK), ILE (Japan)
Neutron yield: 105 106
Hydrodynamic pulse
I u3 , u ~ 1000 km/s
Laser: IL 1015 W/cm2, L 1 ns
Experiments: CD-target + cone
ILE (Japan)
Neutron yield: 105 106
S.Yu.Gus’kov. LPI RAS
Compression
=(300 - 500) g/cm3
R = (3 - 4) g/cm2
Ignition
T=10 keV
Rign = 0. 4 g/cm2
Igniting Driver
Energy: Eign = (10-15)/1002 kJ Eign = (10-30) kJ
Beam radius: Rign= Rign / Rign 10-30m
Pulse duration: ign = Rign/108 ign 10 ps
Intensity: Iign (1018 - 1019) W/cm2
![Page 4: S.Yu.Gus’kov. LPI RAS Fast Ignition by Detonating Hydrodynamic Flow S.Yu. Gus’kov *, M. Murakami ** * P.N. Lebedev Physical Institute of Russian Academy.](https://reader035.fdocuments.in/reader035/viewer/2022062520/5697c0111a28abf838ccbd78/html5/thumbnails/4.jpg)
S.Yu.Gus’kov. LPI RAS
t=300-500 g/cm3 ! Tign=10keV. I imu3
General Requirements for Impact Ignition
Iign t (CDTTign)3/2, ign 0.5(im /t)1/2
=300-500 g/cm3
R=3-4 g/cm2
u 1.5(t /im)1/2 (CDTTign)1/2
t = im u = 1500 km/s,
t = 10im u > 4000 km/s,
Ignition of the Target
R=3-4 g/cm2
=300-500 g/cm3
I im (CDTTign)3/2
u (CDTTign)1/2
u ~1000 km/s
Ignition of the Impactor
Theoretical limit of low-entropy laser-driven acceleration of a foil: 1700 km/s
![Page 5: S.Yu.Gus’kov. LPI RAS Fast Ignition by Detonating Hydrodynamic Flow S.Yu. Gus’kov *, M. Murakami ** * P.N. Lebedev Physical Institute of Russian Academy.](https://reader035.fdocuments.in/reader035/viewer/2022062520/5697c0111a28abf838ccbd78/html5/thumbnails/5.jpg)
S.Yu.Gus’kov. LPI RASHydrodynamic fast ignition
Compression in a conical target.
Detonating flow.
~ (100-200) g/cm3 V ~ (500 - 300) km/s,
S. Gus’kov, M.Murakami XXX ECLIM, 2008
Impact along a cone
~ 1 g/cm3 V ~ 1000 km/s,
M.Murakami, H. Nagatomo
Nucl. Inst. & Meth. Phys. Res. A544, 67, 2005
Profiling laser pulse
Simple laser pulse
ILE (Osaka University, Japan) experiments on impact ignition, EL~ (1-3) kJ, 3:
• Acceleration of the foil up to record velocity: 600–700 km/s.
• Impact neutron generation: (1 -2) 106 DD-neutrons/shot.
1000 km/s 300 km/
![Page 6: S.Yu.Gus’kov. LPI RAS Fast Ignition by Detonating Hydrodynamic Flow S.Yu. Gus’kov *, M. Murakami ** * P.N. Lebedev Physical Institute of Russian Academy.](https://reader035.fdocuments.in/reader035/viewer/2022062520/5697c0111a28abf838ccbd78/html5/thumbnails/6.jpg)
S.Yu.Gus’kov. LPI RASILE planar impact ignition experiments
impactorMain fuel
laser
600 m
Be plane(weight)
Be frame
CD foils 20 mt
Laser energy :1.9 kJSpot size : 300 m
laser
Be frameCD foil 20 mt
Laser energy :1.9 kJSpot size : 300 m
laser
600 m
CH plane300 mt
Be frame
CD foils 20 mt
Laser energy :1.3 kJSpot size : 300 m
1. CD-foil - CD-target impact
2. CD-foil - CD-target impact
3. CD-foil - CH-target impact
Watari T, Sakaiya T, Azachi H et al Neutron generation from impact fast ignition Proc. 5-th IFSA conference (Kobe, Japan, September 2007)
N: 106 N: 1.3105N: 8.3105
1) impact nature of neutron generation and
2) neutron generation in impact-produced plasma of impactor
>>
![Page 7: S.Yu.Gus’kov. LPI RAS Fast Ignition by Detonating Hydrodynamic Flow S.Yu. Gus’kov *, M. Murakami ** * P.N. Lebedev Physical Institute of Russian Academy.](https://reader035.fdocuments.in/reader035/viewer/2022062520/5697c0111a28abf838ccbd78/html5/thumbnails/7.jpg)
S.Yu.Gus’kov. LPI RASILE spherical impact ignition experiments
50m
275mAucone:90degree
CD shell7m
t
500m
500m
CD shell 10m
t
Impactor
Main
P M T
Plastic scintillator18 cm × 2.5 cm
47 cm 311 cm
190 cm178 cm
Pb 10 cm
25°
80°
52°
168°
Plastic scintillator10 cm × 5 cm
target
421 detectors
MANDALA
1344 cm
Target chamber
Watari T, Sakaiya T, Azachi H et al. Neutron generation from impact fast ignition. Proc. 5-th IFSA conference (Kobe, Japan, September 2007
1. Nmax= 2106
2. Ti=1.59 keV
3. Nmax corresponds to coincidence of the moments
of maximal compression and impact
![Page 8: S.Yu.Gus’kov. LPI RAS Fast Ignition by Detonating Hydrodynamic Flow S.Yu. Gus’kov *, M. Murakami ** * P.N. Lebedev Physical Institute of Russian Academy.](https://reader035.fdocuments.in/reader035/viewer/2022062520/5697c0111a28abf838ccbd78/html5/thumbnails/8.jpg)
S.Yu.Gus’kov. LPI RASImpactor’s state before collision.
Impactor’s density and velocity distributions along the central axis.
L = 600 m, t = 1.8 ns L = 1000 m, t = 2 ns
u u
u 600 km/s u 800 km/s
0.2 g / cc 0.08 g /cc
<>
![Page 9: S.Yu.Gus’kov. LPI RAS Fast Ignition by Detonating Hydrodynamic Flow S.Yu. Gus’kov *, M. Murakami ** * P.N. Lebedev Physical Institute of Russian Academy.](https://reader035.fdocuments.in/reader035/viewer/2022062520/5697c0111a28abf838ccbd78/html5/thumbnails/9.jpg)
S.Yu.Gus’kov. LPI RASImpact-produced plasma of impactor and target
Density, ion and electron temperature distributions along the central axis
L = 600 m, t = 1.8 ns L = 1000 m, t = 2 ns
Target Impactor ImpactorTarget
Ti Te
Ti Te
Ti=Te
Ti=Te
Target Ti 80 eV, 3.8
g/cc
Impactor Ti 2.2 keV, Te 1.2 keV
0.18 g/cc
Target Ti 60 eV, 3.8 g/cc
Impactor Ti 6.2 keV, Te 1.8 keV
0.12 g/cc
N 106 N 6.3106<<
>>
![Page 10: S.Yu.Gus’kov. LPI RAS Fast Ignition by Detonating Hydrodynamic Flow S.Yu. Gus’kov *, M. Murakami ** * P.N. Lebedev Physical Institute of Russian Academy.](https://reader035.fdocuments.in/reader035/viewer/2022062520/5697c0111a28abf838ccbd78/html5/thumbnails/10.jpg)
S.Yu.Gus’kov. LPI RAS
Gekko/HIPER
1. Impactor’s density significantly less than target’s density:
imp 0.6 g/cm3 << t 4 g/cm3
1. Predominant heating of impactor’s ions,Ti>>Te . Equilibrium target’s plasma Ti=Te .
Impactor’s temperature significantly larger than target’s temperature:
Timp (1.5 -3) keV >> Tt (0.1 -0.2) keV
1. Neutron yield from impactor significantly larger than neutron yield from the target:
Nm 107 >> Nm 106
Confirmation of the approach:
initial ignition of impactor and subsequent propagation of detonation wave
from impactor to compressed thermonuclear fuel of ICF-target
![Page 11: S.Yu.Gus’kov. LPI RAS Fast Ignition by Detonating Hydrodynamic Flow S.Yu. Gus’kov *, M. Murakami ** * P.N. Lebedev Physical Institute of Russian Academy.](https://reader035.fdocuments.in/reader035/viewer/2022062520/5697c0111a28abf838ccbd78/html5/thumbnails/11.jpg)
S.Yu.Gus’kov. LPI RAS
Fast ignition by detonating
hydrodynamic flow
![Page 12: S.Yu.Gus’kov. LPI RAS Fast Ignition by Detonating Hydrodynamic Flow S.Yu. Gus’kov *, M. Murakami ** * P.N. Lebedev Physical Institute of Russian Academy.](https://reader035.fdocuments.in/reader035/viewer/2022062520/5697c0111a28abf838ccbd78/html5/thumbnails/12.jpg)
Detonating impactorS.Yu.Gus’kov.
LPI RAS
ICF-target
PusherAblator
Igniter
Development of “Cone-Guided Impactor” to “Target inside Target”
Ignition by Detonating Impactor - “Target From Target” Ignition
Conetarget
1. Cone target withhomogeneous DT-fuel
and profiled laser pulse
2. Cone target with spatial distributed
density
Multi-layer cone target
Conetarget
Conetarget
ICF-target ICF-target
Two well-known ICF-methods:1. Profiled Laser Pulse and 2. Initial Density Distribution
![Page 13: S.Yu.Gus’kov. LPI RAS Fast Ignition by Detonating Hydrodynamic Flow S.Yu. Gus’kov *, M. Murakami ** * P.N. Lebedev Physical Institute of Russian Academy.](https://reader035.fdocuments.in/reader035/viewer/2022062520/5697c0111a28abf838ccbd78/html5/thumbnails/13.jpg)
General requirement for ignition by detonating DT-impactor
(R )t ~ 3 -4 g /cm 2
t ~ 100-200 g /cm 3
tw = 4tDT-fuel
ShockedDT-fuel
Impactor
Cone
Ignition
1. Ignition of the impactor:
2. Detonation wave to DT-fuel:
ign2T = 10 keV, ρ Δ 0.4g/cm
m m
1/ 220.15 /t g cm
m mm
United requirement :
S.Yu.Gus’kov. LPI RAS
1/ 220.15 / if 0.14
20.4 / if 0.14
t mg cmm m
m t
mg cmm m
t
Minimal ignition energy, m= t :15
,23/100 /
E kJ
g cmt
Factor of exceeding:
7 / 20.053 if 0.14min
2 if 0.14min
mtE Em t
mtE Em t
m t
1/ 2
3 ,( )
mP D C T Dm th DT t ig th
t
![Page 14: S.Yu.Gus’kov. LPI RAS Fast Ignition by Detonating Hydrodynamic Flow S.Yu. Gus’kov *, M. Murakami ** * P.N. Lebedev Physical Institute of Russian Academy.](https://reader035.fdocuments.in/reader035/viewer/2022062520/5697c0111a28abf838ccbd78/html5/thumbnails/14.jpg)
S.Yu.Gus’kov. LPI RAS
“Target from Target” Ignition by
Three-Layer Cone Target
![Page 15: S.Yu.Gus’kov. LPI RAS Fast Ignition by Detonating Hydrodynamic Flow S.Yu. Gus’kov *, M. Murakami ** * P.N. Lebedev Physical Institute of Russian Academy.](https://reader035.fdocuments.in/reader035/viewer/2022062520/5697c0111a28abf838ccbd78/html5/thumbnails/15.jpg)
3. DT-ice Igniter.• Function: Self-burning and ignition of ICF-target DT fuel by the detonation wave
Three-layer cone target
M m
M p>>M m
m
p> >m
AblatorDT-ice Pusher
M a~M p
M p
p a
a< <p
M a
2. Pusher. • Heavy-element material: Cu, Pb, Au and others.
• Function: Impact-driven adiabatic compression of the igniter.
1. Ablator.
• Light-element material: (CH)n-plastics, Be, Al and others.
•Function: Acceleration of impactor laser light absorption, ablation pressure creation.
• Totally evaporated at the acceleration stage.
S.Yu.Gus’kov. LPI RAS
![Page 16: S.Yu.Gus’kov. LPI RAS Fast Ignition by Detonating Hydrodynamic Flow S.Yu. Gus’kov *, M. Murakami ** * P.N. Lebedev Physical Institute of Russian Academy.](https://reader035.fdocuments.in/reader035/viewer/2022062520/5697c0111a28abf838ccbd78/html5/thumbnails/16.jpg)
Statement of the Problem. Planar Approximation.
Initial pressure of DT-fuel
5 / 33 32.17 ( / ) , ; 100 300 / (5 30)P g cm Mbar g cm Gbartt
Pressure in the igniter at a decelleration stage:
2 3, 0.25 / , 1000 / 30 0 0 0
P u g cm u km s P Gbarb m m m m b
1. Deceleration of the igniter by first shock wave, Pb0 << Pt
2. Deceleration of the pusher and adiabatic compression of the ignitor, Pb>>Pb0
3. Shock wave in ICF-Target DT-fuel; Effect of DT-fuel compressibility, Pb>Pt
(R )t ~ 3 -4 g /cm 2
t ~ 100-200 g /cm 3
tw = 4tDT-fuel
ShockedDT-fuel
Ignition
Cone
Cone
Igniter
Pusher
Impactor = Igniter+Pusher
P s0=0Pm
U 0m
s0Tm2
Ts0=0
DT-fuel DT-ign.
D sPs
s
Ts
P t>>Pm
t
Ablator
S.Yu.Gus’kov. LPI RAS
Pressure in the igniter at a burning stage:
R=0.4 г/см2, T=10 keV, =100 г/см2 P~100-200 Gbar
![Page 17: S.Yu.Gus’kov. LPI RAS Fast Ignition by Detonating Hydrodynamic Flow S.Yu. Gus’kov *, M. Murakami ** * P.N. Lebedev Physical Institute of Russian Academy.](https://reader035.fdocuments.in/reader035/viewer/2022062520/5697c0111a28abf838ccbd78/html5/thumbnails/17.jpg)
S.Yu.Gus’kov. LPI RASCompression and heating of the igniter
P t0 PP P
D t
U w1U U
t twm s
T twTm
Ts
DT-fuel DT-igniter Pusher
1 221 1
M Mm sP M M u E Em sb m w bm m s s
The moment of maximal compression: deceleration of the impactor down to the velocity of shock wave in ICF-target DT-fuel
Energy of shock wave in ICF-target DT-fuel
Residual kinetic energy of the impactor
1. Residual kinetic energy of the impactor: 1/ 2
1 22 ,2 1 0
PtE M M u um pb w wt t
2. Energy of shock wave in ICF-target DT-fuel: 1/ 22 1
, ,( 1) 2 20
M M uP P m s mt t tE D t D tw t b t b Pt b
Adiabatic compression at the initial entropy from first shock wave: 11/ 1/ 2/ , / ,
02mm sP P P ub m b sm s w m m
1/ 23. = 200 g/cm : E ~0.12 E , E ~ 0.03 E
0 t0 w 0 b 00
EbE E E Ew w bE
![Page 18: S.Yu.Gus’kov. LPI RAS Fast Ignition by Detonating Hydrodynamic Flow S.Yu. Gus’kov *, M. Murakami ** * P.N. Lebedev Physical Institute of Russian Academy.](https://reader035.fdocuments.in/reader035/viewer/2022062520/5697c0111a28abf838ccbd78/html5/thumbnails/18.jpg)
Final state of the igniter
P t0 PP P
D t
U w1U U
t twm s
T twTm
Ts
DT-fuel DT-igniter Pusher
2 /( 1)1/ 21 1 01
1/ 2 1 /2 1 00 0
mP Pbc b
tm s
Au-pusher, Ms/Mm=20
Compressible ICF-target fuel:Pb/Pw 700; m 52 g/cm3; T=10 keV, at um 410 km/s; energy factor, 0.18
S.Yu.Gus’kov. LPI RAS
Exact solution for m= s= t= :
/( 1)11 2 ,
021 /0 0
Mm sP P where P ub w w m m Mmm s
Compressibility factor“Uncompressible” solution
Uncompressible ICF-target fuel: Pb/Pw 1100,m 75 g/cm3; T=10 keV, at um 365 km/s; energy factor,
0.25
101
0 0
E Mm s mE Mm sb
Internal energy of igniter
![Page 19: S.Yu.Gus’kov. LPI RAS Fast Ignition by Detonating Hydrodynamic Flow S.Yu. Gus’kov *, M. Murakami ** * P.N. Lebedev Physical Institute of Russian Academy.](https://reader035.fdocuments.in/reader035/viewer/2022062520/5697c0111a28abf838ccbd78/html5/thumbnails/19.jpg)
S.Yu.Gus’kov. LPI RAS
t=200g/cc
t=500g/cc
t=300g/cc
- - - - uncompressible ICF-target fuel
Pusher and igniter mass ratio vsfinal igniter density
1, 2, 3, 4 - energy factor, Em / E0 = 0.35, 6, 7, 8 - energy factor, Em / E0 = 0.5
Tig=10 keV:initial impactor velocity vs final igniter density
( 1) / 21 0(100 / ) 1.521
mu km sm
Final igniter density and velocity of ignition
u 330 km/sAu-pusher: Mpusher/Migniter 38DT-igniter, ()ig=0.4 g/cm2:
ig 40 m Migniter 4 10-5 gMpusher 1.5 10-4 g
t=300 g/cm3
Eigniter/Eimpactor = 0,56
ig=100 g/cm3
Initial: Eimpactor 70 kJ
Final: Eigniter 40 kJ
![Page 20: S.Yu.Gus’kov. LPI RAS Fast Ignition by Detonating Hydrodynamic Flow S.Yu. Gus’kov *, M. Murakami ** * P.N. Lebedev Physical Institute of Russian Academy.](https://reader035.fdocuments.in/reader035/viewer/2022062520/5697c0111a28abf838ccbd78/html5/thumbnails/20.jpg)
Conical three - layer igniting target design
S.Yu.Gus’kov. LPI RAS
![Page 21: S.Yu.Gus’kov. LPI RAS Fast Ignition by Detonating Hydrodynamic Flow S.Yu. Gus’kov *, M. Murakami ** * P.N. Lebedev Physical Institute of Russian Academy.](https://reader035.fdocuments.in/reader035/viewer/2022062520/5697c0111a28abf838ccbd78/html5/thumbnails/21.jpg)
2
R ig ttgR igt
S.Yu.Gus’kov. LPI RAS
Ignition of the igniter: (R)ig=0.4 g/cm2
High gain of ICF-target (R)t=3-4 g/cm2
Cone opening angle
0.5 0.2ig
t
400-600
Igniting target. Requirements to the design
1/ 32 08,3 lnM
u IM f
Evaporation - 50%, M0 / Mf = 2 Mass of ablator = a half of total mass,
0.3, u 0.57(I2)1/3
Shell velocity:
2R0
L(R)ig , ig
(R)t , t
1/ 31/ 3 2 / 3
3.1 ,0 1/ 3 2 / 3
E tgimpactR cm
u
Eimp=70 kJ, u = 3.3 107 cm/s, =0.3, =50o, = 0.35 m R0 0.153 cm, L0. 32 cm, 19.5ns
![Page 22: S.Yu.Gus’kov. LPI RAS Fast Ignition by Detonating Hydrodynamic Flow S.Yu. Gus’kov *, M. Murakami ** * P.N. Lebedev Physical Institute of Russian Academy.](https://reader035.fdocuments.in/reader035/viewer/2022062520/5697c0111a28abf838ccbd78/html5/thumbnails/22.jpg)
Igniting conical target designS.Yu.Gus’kov.
LPI RAS
igniter 21,3 m
pusher 10.7 m
ablator 115.6 m
R0 0.153 cm
DT-igniter: Migniter 4 10-5 g
Au-pusher: Mpusher 1.5 10-4 g
Be-ablator: Mablator=Mpusher
115.6 m
21,3 m
10.7 m
L 0. 32 cm
2R0 0.3 cm
=50o
Elaser= Eimpactor / Kabs
Eimpactor 70 kJ
= 0.3, Kabs= 0.7
Elaser 320 kJ
![Page 23: S.Yu.Gus’kov. LPI RAS Fast Ignition by Detonating Hydrodynamic Flow S.Yu. Gus’kov *, M. Murakami ** * P.N. Lebedev Physical Institute of Russian Academy.](https://reader035.fdocuments.in/reader035/viewer/2022062520/5697c0111a28abf838ccbd78/html5/thumbnails/23.jpg)
Conclusion:
Practicability of hydrodynamic ignition at the velocity of 300-500 km/s 1. Fast Ignition by Detonating Hydrodynamical Flow
• Approach of “Target from Target” ignition
• Conical three-layer igniting target:
Ignition at the initial velocity of hydrodynamical flow 330 km/s
and final density of detonating flow 100 g/cm3
Laser parameters: EL= 320 kJ, L= 19.5 ns
2. Key points:
• Hydrodynamic instability
• Impactor’s state before impact
• EOS of heavy pusher
3. Experiments: collision of multi-layer impactor accelerated along conical or
cyllindrical channels with a massive plane target.