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1/22
Influence of a Space Charge Effect in aFemtosecond Electron Beam on Coherent
Transition Radiation Spectrum
M. Shevelev1, A. Aryshev1, Y. Honda1,2, N. Terunuma1,2 andJ. Urakawa1
1High Energy Accelerator Research Organization (KEK)
2The Graduate University for Advanced Studies (SOKENDAI)
Tsukuba, Ibaraki, 305− 0801, Japan
30 September 2016
2/22
Motivations and goals
Top Goal:
I Development of radiation source based on compactaccelerator.
Subgoals:
1 estimation of bunch length in experimental area using ASTRAsoftware for usual settings of LUCX facility;
2 optimization of LUCX parameters for suppression of spacecharge effect;
3 demonstration how the beam dynamics could influence oncoherent radiation of electron bunches.
3/22
Report outline:
1 ASTRA simulation;
2 Experimental test;
3 Discussions and conclusion.
4/22
ASTRA
ASTRA - A Space Charge Tracking Algorithm written by KlausFlottmann from DESY (Germany)1.
The software allows tracking charge particles bunches throughdifferent beam line components. Plus it permits to take intoaccount space charge effect.
1K. Flottmann ASTRA (DESY, Zeuthen, 2013)
5/22
LUCX facility and controlled settings
RF Gun
Solenoid
GVGV
ScreenT z ChamberH
laser pulse
ICT FCT
1.31m
1.72 m
x
y z
We could change the next parametersin real experiment:
I solenoid current;
I bunch charge (from a darkcurrent to 400 pC);
I maximum value of an electricfield strength on the cathode(from 60 to 120 MV/m);
I laser spot size on the cathode(from 340× 420 µm2 to severalmm);
I laser pulse duration (from 50 to200 fs);
I laser pulse energy.
6/22
Electron distributions in bunch
Transverse distributionLongitudinal distribution
Simulation parameters: laser pulse is 100 fs, laser spot size is 450× 450 µm2,
Q = 25 pC, MaxB= 0.225 T, MaxE= 77 MV/m, z = 1.31 m.
7/22
Solenoid scan
0.210 0.215 0.220 0.225 0.230 0.235 0.240
Maximum value of magnetic field in the solenoid (T)
0.0
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
Tran
sver
sesi
ze(m
m)
200
400
600
800
1000
1200
1400
long
itudi
nals
ize
(fs)
σx
σy
σz
Simulation parameters: Q=25 pC, t=100 fs, σlx = σl
y = 0.45 mm,
MaxE=80 MV/m, RF gun phase= 30deg., z = 1.72 m.
8/22
Charge scan
0 50 100 150 200
Bunch charge (pC)
0.0
0.2
0.4
0.6
0.8
1.0
1.2
Tran
sver
sesi
ze(m
m)
0.0
0.5
1.0
1.5
2.0
2.5
3.0
long
itudi
nals
ize
(ps)
σx
σy
σz
Simulation parameters: MaxB=0.233, t=100 fs, σlx = σl
y = 0.45 mm,
MaxE=80 MV/m, RF gun phase= 30 deg., z = 1.31 m.
9/22
Charge scan for different value of maximum amplitude ofelectric field strength on the cathode
0 50 100 150 200
Bunch Charge (pC)
0.0
0.5
1.0
1.5
2.0
2.5
3.0
3.5
4.0
4.5Lo
ngitu
dina
lsiz
e(p
s)
60 MV/m80 MV/m100 MV/m120 MV/m
Simulation parameters: MaxB=0.2254, t=100 fs, σlx = σl
y = 0.45 mm,
MaxE=80 MV/m, RF gun phase= 30 deg., z = 1.31 m.
10/22
Laser settings
0.0 0.5 1.0 1.5 2.0 2.5 3.0 3.5
Laser spot size on the cathode (mm)
0.0
0.5
1.0
1.5
2.0
Long
itudi
nals
ize
(ps)
60 MV/m80 MV/m100 MV/m120 MV/m
50 100 150 200
Laser pulse duration (fs)
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
1.0
Long
itudi
nals
ize
(ps)
Simulation parameters: Q=25 pC, MaxB=0.2254, t=100 fs,
σlx = σl
y = 0.45 mm, MaxE=80 MV/m, RF gun phase= 30 deg., z = 1.31 m.
11/22
Simulation summary
A Magnetic field in solenoid allows compensate transverse sizeof electron bunches without any effects on longitudinal size;
B Increase of bunch charge using laser technique would increasethe space charge forces in bunch;
C The laser pulse length does not influence on bunch length (inreasonable range);
D Transform laser spot size on the photocathode we couldsuppress space charge effect in electron bunches.
Let’s check!
12/22
Experimental scheme and electron beam settings
RF Gun
Accel. M
Soleniod
Laser pulse
Screen
M2
M1
BS
PM
Detector
Beam direction
Sapphirewindow
Traget
PMPM
Electron beam parameters:
I One bunch operation mode;
I Beam energy (RF gun out) is7.9 MeV ⇒ maximum value ofelectric field strength on thecathode (MaxE) is 80 MV/m ;
I Transverse electron beam size onthe luminophore screen is 230 µm(gauss distribution);
I Bunch charge iss 60 pC which ismeasured by FCT.
13/22
Form-Factor for coherent transition radiation
Coherent Transition Radiation:
d2WCTR
dωdΩ=
[N +N (N − 1)F 2 (k)
] d2WTR
dωdΩ, (1)
where F (k) is the form-factor. Formfactor for transition radiationwas calculated analytically2:
F (k) = F (λ, θ, η, ψ)
= exp
[− 2π2
λ2
(σ2x
(tan θ
β− cosψ (cos η tan θ + sin η)
)2
+ σ2y sin2 ψ cos2 (η − θ) +σ2zβ2
)],
where is λ the wavelength, θ is angle of incidence, η is the angle ofobservation, ψ is the azimuth angle of observation.
2G. Naumenko Adv. Material Res. 1084 (2015) or A. Potylitsyn JETP Lett.103 (2016)
14/22
Orientation dependence of TR
40 45 50 55
θ (deg)
0.5
1.0
1.5
2.0
2.5
3.0
Inte
nsity
(arb
.uni
ts)
−10 −8 −6 −4 −2 0 2 4
φ (deg)
4.5 5.0 5.5 6.0 6.5 7.0 7.5
Distance (mm)
0.0
0.5
1.0
1.5
2.0
2.5
3.0
Inte
nsity
(arb
.uni
ts)
15/22
Laser spot size on the virtual cathode
11.0 11.5 12.0 12.5 13.0 13.5 14.0
Revative distance (mm)
300
400
500
600
700
800
900
UV
lase
rspo
tsiz
e(µ
m)
σly
σlx
Relative distance is 12 mm
Relative distance is 13.5 mm
16/22
Laser spot size scan
11.0 11.5 12.0 12.5 13.0 13.5 14.0 14.5
Revative distance (mm)
3
4
5
6
7
Inte
nsity
(arb
.uni
ts)
4.5 5.0 5.5 6.0 6.5 7.0 7.5
Distance (mm)
2
3
4
5
6
7
8
Inte
nsity
(arb
.uni
ts)
0.5
1.0
1.5
2.0
2.5
3.0
Inte
nsity
(arb
.uni
ts)
17/22
Charge scan: comparison between experimental data andsimulation results
Relative distance is 12 mm
0.00 0.01 0.02 0.03 0.04 0.05 0.06
Bunch charge (nC)
0.0
0.5
1.0
1.5
2.0
2.5
3.0
3.5In
tens
ity(a
rb.u
nits
)
−0.84 + 29.70 · x0.64
−0.84 + 23.95 · x0.57
Experimantal dataSimulations
Simulation parameters: Q=60 pC, MaxB=0.2335, t=100 fs, σlx = 344.91 µm,
σly = 420.50 µm, MaxE=80 MV/m, RF gun phase= 30 deg., z = 1.31 m.
18/22
Fit function: y = a+ bc.Simulations:
Parameter Estimation Standard Error
a −0.84 0.34b 29.7 7.83c 0.64 0.10
Experimental data:
Parameter Estimation Standard Error
a −0.84 0.34b 23.95 6.22c 0.57 0.10
19/22
Charge scan
Relative distance is 13.5 mm
0.00 0.01 0.02 0.03 0.04 0.05 0.06
Bunch charge (nC)
0
1
2
3
4
5
6
7
8
Inte
nsity
(arb
.uni
ts)
−0.55 + 66.92 · x0.77
−0.46 + 71.40 · x0.79
Experimantal dataSimulation
Simulation parameters: Q=60 pC, MaxB=0.228, t=100 fs, σlx = 727.42 µm,
σly = 0.757.21 µm, MaxE=80 MV/m, RF gun phase= 30 deg., z = 1.31 m.
20/22
Fit function: y = a+ bc.Simulations:
Parameter Estimation Standard Error
a −0.55 0.47b 66.92 10.55c 0.77 0.08
Experimental data:
Parameter Estimation Standard Error
a −0.46 0.19b 71.40 5.66c 0.79 0.04
21/22
Conclusion future plans
Conclusions:
I ASTRA software allows to estimate the bunch parameters forour experimental conditions;
I In the case of LUCX facility, the space charge effect is themain barrier to produce intense radiation source in THz range;
I Laser technique is not suitable to confirm quadraticdependence of coherent radiation intensity;
I However, laser techniques allows to suppress space chargeeffect in femtosecond electron bunches.
Future plans:
I We are going to decrease space charge effect in the RF gunusing spatial reshaping technique for laser pulse;
I We make optimization of the LUCX settings for themulti-bunches operation mode (two and four bunches).
22/22
Thank you for attention!