Emittance Growth Caused by Surface Roughness
Zhe Zhang, Chuanxiang Tang Tsinghua University, Beijing
- Oct. 17th, 2016
Emittance Growth Caused by Surface Roughness Zhe Zhang, Chuanxiang - - PowerPoint PPT Presentation
Emittance Growth Caused by Surface Roughness Zhe Zhang, Chuanxiang Tang Tsinghua University, Beijing Oct. 17th, 2016 Motivation What causes the emittance growth Dowells equations of QE & emittance for bulk emission Dowell, 2009,
Zhe Zhang, Chuanxiang Tang Tsinghua University, Beijing
QE(ω) ≈ 1 − R(ω) 1 + λopt λe−e(ω) (~ω − φeff)2 8φeff(EF + φeff)
εn,x = σx r ~ω − φeff 3mc2
What causes the emittance growth
Dowell, 2009, PRST
QE(ω) ≈ 1 − R(ω) 1 + λopt λe−e(ω) (~ω − φeff)2 8φeff(EF + φeff)
εn,x = σx r ~ω − φeff 3mc2
What causes the emittance growth
Dowell, 2009, PRST
QE: Theory vs. Measurement
1x10-3 1x10-4 1x10-5 1x10-6 1x10-7 1x10-2 1x10-8 Quantum Efficiency
180 200 220 240 260 280 300
Theory at 0 MV/m
Theory at 50 MV/m
Experiment Wavelength (nm)
Dowell, 2006, PRST
QE(ω) ≈ 1 − R(ω) 1 + λopt λe−e(ω) (~ω − φeff)2 8φeff(EF + φeff)
εn,x = σx r ~ω − φeff 3mc2
What causes the emittance growth
Dowell, 2009, PRST
Emittance: Theory vs. Measurement
Qian, 2012, Ph.D.
Parameter Unit BNL SLAC PSI laser wavelength mm 266 253 261 272 282 gun gradient MV/m 95 115 / / / gun phase deg / 15 / / / launch electric field MV/m / 30 25 25 25 measured therm. emit. µm/mm 0.92 0.9 0.68 0.54 0.41 theory therm. emit. µm/mm / 0.54 0.64 0.54 0.43 copper work function µm/mm 4.59 4.65 4.3 4.3 4.3
photon electron
VACUUM METAL
x z O
BASE PLANE
x' z' O' P'
How people deal with the surface roughness effect
ε2
x ≈ ε2 D,x
✓ 1 + 1 2ξ2 ◆ ε2
x ≈ ε2 D,x
✓ 1 + 3πe 4 · a2kE ~ω − φeff ◆
Ex = Eξ · e−kz sin kx Ez = E
slope effect field effect
R = a sin(kx)
surface morphology field distribution
Diffjculties in 3D case calculation
distribution (slope effect)
surface (field effect)
Diffjculties in 3D case simulation
samples (slope effect)
near a real-life rough surface (field effect)
Diffjculties in 3D case simulation
3-step Model
barrier Could sampling by applying the Monte-Carlo method.
Dowell, 2009, PRST
samples (slope effect)
near a real-life rough surface (field effect)
samples (slope effect)
near a real-life rough surface (field effect)
Diffjculties in 3D case simulation
3-step Model
barrier Could sampling by applying the Monte-Carlo method.
Dowell, 2009, PRST
Monte-Carlo Sampling
Generate s ~ Exp(λ), E ~ U(EF−ħω, EF), θ′ ~ U(0, π/ 2), φ′ ~ U(0, 2π), where 1/λ = 1/λopt+1/λe-e, then apply the filter condition (E+ħω)cos2θ′ ≥ φeff.
However the sampling efficiency is quite low (~ 1e-4) because of the low QE of metals.
z ' y ' x' O'
photonVACUUM
P
electronz y x O
METAL
local globalDiffjculties in 3D case simulation
Meshing on the Rough Surface
The rms amplitude of the surface roughness is ~ 10 nm, the average rms wavelength is ~ 10 µm, and the size of the laser spot is ~ 1 mm. Meshing would be too memory-consuming.
Unrealistic to do this in EM field simulation code.
samples (slope effect)
near a real-life rough surface (field effect)
samples (slope effect)
near a real-life rough surface (field effect)
How to deal with the diffjculties in 3D case
Utilize the Point Spread Function
By applying the Point Spread Function (PSF) of photocathode,
the rough surface.
Thus the sampling efficiency could be significantly improved.
fp(px, py, pz) = Cp(θ)pz p p2
z + p2 m ·
q p2
x + p2 y + p2 z + p2 m
· H(pz)H(p2
M − p2 m − p2 x − p2 y − p2 z)
Cp(θ) = 1 − R(θ) 1 + λopt λe−e cos θ · 1 4πm~ω
samples (slope effect)
near a real-life rough surface (field effect)
How to deal with the diffjculties in 3D case
Approximate Formula for the Electric Potential
For gently undulating surface, there exist some approximate formula for the electric potential distribution, which is proved to be accurate enough for our case.
Therefore we could generate the fields much faster and cost much less memory.
φ(x, y, z) = z − Z dkxdkyR(kx, ky) · ej(kxx+kyy)−kz
The PSF of the fmat surface
z y x O
photon electron
METAL VACUUM
Transform (s, θ, φ, E, ω) to (x, y, px, py, pz)
f(s, θ, φ, E, ω) =(1 − R) 1 λopt exp −s ✓ 1 λopt + 1 ¯ λe-e ◆ · H(EF − E)H(E + ~ω − EF) ~ω sin θ 4π f(x, y, px, py, pz) =C exp 2 4− p p2
z + p2 m
q p2
x + p2 y
· p x2 + y2 λ 3 5 · pz q p2
x + p2 y + p2 z + p2 m
· δ(xpy − ypx) · H(pz)H(xpx)H(p2
M − p2 m − p2 x − p2 y − p2 z)
Dowell, 2009, PRST
Point Spread Function
The response (image) is the convolution of the point spread function (PSF) and the source (object).
D(x, y) = I(x, y) ∗ f(x, y)
The PSF of the fmat surface
z y x O
photon electron
METAL VACUUM
Transform (s, θ, φ, E, ω) to (x, y, px, py, pz)
f(s, θ, φ, E, ω) =(1 − R) 1 λopt exp −s ✓ 1 λopt + 1 ¯ λe-e ◆ · H(EF − E)H(E + ~ω − EF) ~ω sin θ 4π f(x, y, px, py, pz) =C exp 2 4− p p2
z + p2 m
q p2
x + p2 y
· p x2 + y2 λ 3 5 · pz q p2
x + p2 y + p2 z + p2 m
· δ(xpy − ypx) · H(pz)H(xpx)H(p2
M − p2 m − p2 x − p2 y − p2 z)
Dowell, 2009, PRST
The PSF of the rough surface
z' y ' x' O'
photon
VACUUM
P
electron
z y x O
METAL
l
a l global
D
D
The PSF of the rough surface
z' y ' x' O'
photon
VACUUM
P
electron
z y x O
METAL
l
a l global
D
D
The Momentum PSF
The momentum PSF is the integration of PSF over the real-space (x, y).
fp(px, py, pz) = Cp(θ)pz p p2
z + p2 m ·
q p2
x + p2 y + p2 z + p2 m
· H(pz)H(p2
M − p2 m − p2 x − p2 y − p2 z)
Cp(θ) = 1 − R(θ) 1 + λopt λe−e cos θ · 1 4πm~ω
The Momentum PSF
The momentum PSF is the integration of PSF over the real-space (x, y).
fp(px, py, pz) = Cp(θ)pz p p2
z + p2 m ·
q p2
x + p2 y + p2 z + p2 m
· H(pz)H(p2
M − p2 m − p2 x − p2 y − p2 z)
Cp(θ) = 1 − R(θ) 1 + λopt λe−e cos θ · 1 4πm~ω
z' y ' x' O'
photon
VACUUM
P
electron
z y x O
METAL
l
a l global
D
D
The PSF of the rough surface
The Effect of the Incident Angle
For a gently undulating surface, the effect of the incident angle could be neglected.
The slope effect on the rough surface
fp(px, py, pz) = Cp0 · pz p p2
z + p2 m ·
q p2
x + p2 y + p2 z + p2 m
Cathode Surface
The slope effect on the rough surface
fp(px, py, pz) = Cp0 · pz p p2
z + p2 m ·
q p2
x + p2 y + p2 z + p2 m
Cathode Surface
The slope effect on the rough surface
fp(px, py, pz) = Cp0 · pz p p2
z + p2 m ·
q p2
x + p2 y + p2 z + p2 m
Cathode Surface
The electric fjeld distribution near the rough surface
φ(x, y, z) = z + Z dkxdkyC(kx, ky) · ej(kxx+kyy)−kz φ(x, y, z) = z − Z dkxdkyR(kx, ky) · ej(kxx+kyy)−kz The Form of the Approximate Potential
The form is set to satisfy the Laplace’s equation and the B.C. for infinity.
z = R(x, y) φ = 0 z = d → +∞ φ = d Cathode Vacuum
The electric fjeld distribution near the rough surface
φ(x, y, z) = z + Z dkxdkyC(kx, ky) · ej(kxx+kyy)−kz φ(x, y, z) = z − Z dkxdkyR(kx, ky) · ej(kxx+kyy)−kz The B.C. at Surface
When kR(x, y) << 1, the B.C. at surface would lead to C(kx, ky) = -R(kx, ky).
φ (x, y, R(x, y)) = R(x, y) + Z dkxdkyC(kx, ky) · ej(kxx+kyy)−kR(x,y) ≈ R(x, y) + Z dkxdkyC(kx, ky) · ej(kxx+kyy) (1 − kR(x, y)) = Z dkxdky(R(kx, ky) + C(kx, ky)) · ej(kxx+kyy) + O(1) = O(1)
The electric fjeld distribution near the rough surface
φ(x, y, z) = z + Z dkxdkyC(kx, ky) · ej(kxx+kyy)−kz φ(x, y, z) = z − Z dkxdkyR(kx, ky) · ej(kxx+kyy)−kz The B.C. at Surface
When kR(x, y) << 1, the B.C. at surface would lead to C(kx, ky) = -R(kx, ky).
φ (x, y, R(x, y)) = R(x, y) + Z dkxdkyC(kx, ky) · ej(kxx+kyy)−kR(x,y) ≈ R(x, y) + Z dkxdkyC(kx, ky) · ej(kxx+kyy) (1 − kR(x, y)) = Z dkxdky(R(kx, ky) + C(kx, ky)) · ej(kxx+kyy) + O(1) = O(1)
Gently Undulating Surface
A gently undulating surface should mean that:
rms(R) · rms(k) ⌧ 1
The electric fjeld distribution near the rough surface
φ(x, y, z) = z + Z dkxdkyC(kx, ky) · ej(kxx+kyy)−kz φ(x, y, z) = z − Z dkxdkyR(kx, ky) · ej(kxx+kyy)−kz Approximate Formula for the Electric Field Ex = j Z dkxdky · kxR(kx, ky) · ej(kxx+kyy)−kz Ey = j Z dkxdky · kyR(kx, ky) · ej(kxx+kyy)−kz Ez = −1 − Z dkxdky · kR(kx, ky) · ej(kxx+kyy)−kz
3D arbitrary surface
ε2 = hx2ihp2
xi hxpxi2
Roughness Emittance on Arbitrary Gently Undulating Surface
ε2
x = ε2 D,x
2 6 6 6 6 6 4 1 − ⌦ ∂2
xR
↵ + * p0
z · ∂xR + jm
r πA 2 · Z dkxdky kx √ k R(kx, ky) · ej(kxx+kyy) !2+ ⌦ p0
x 2↵
3 7 7 7 7 7 5
Saturated Transverse Momentum p∞ − p0 = m r A 2 · Z − Ex √z dz = −jm r πA 2 · Z dkxdky kx √ k R(kx, ky) · ej(kxx+kyy)
A = eE/m
The principles
The principles
Average Number of Attempts to Produce an Accepted Sample
The samples generated by rejective method obey the geometry distribution.
E(N) = π ✓ 1 + pm pM ◆ ≈ 2π pm = p 2m(EF + φeff) pM = p 2m(EF + ~ω) N ∼ G(p)
The principles
Z-based Motion Equations
We choose the z-based motion equations because the E-field is calculated by z-layer, z-based motion could guarantee the accuracy.
dpx [keV/c] dz [nm] = 511 × 10−6 · E0 [MV/m] pz [keV/c] · ˆ Ex(x, y, z) dx [µm] dz [nm] = px [keV/c] pz [keV/c] · 1 × 10−3
Cathode Surface Z-layers Electron
The simulation confjguration
details Table 1: Parameters used in numerical simulation. Parameter Value Unit Description λl 266.0 nm laser wavelength l-dist uniform
rl 20.0 µm laser transverse radius xl 80.0 µm laser incident x center yl 60.0 µm laser incident y center mat copper
E0 50.0 MV/m effective electric field strength φw 4.31 eV work function φeff 4.04 eV effective work function EF 7.0 eV Fermi energy N 10000
zi nm simulation starting position zf 5000.0 nm simulation ending position dz 10.0 nm simulation z step
The phase-space & emittance evolution
Comparison between 2D and 3D result
¯ ε2
n,x = σ2 x ·
" ~ω − φeff 3mc2 + πe2 mc2 · R2
qE
λq #
initial phase-space distribution due to slope effect
phase-space evolution based
for a given emittance growth upper limit
emission effect
SPPs (Surface Plasmon Polaritons) generation
smoothing effect
work function variation due to the surface roughness
Pros & Cons
Questions or Comments