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Phase-space Description of Charged Particle Beams

Fall, 2017

Kyoung-Jae Chung

Department of Nuclear Engineering

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Basic properties of electron and proton

 Electron (e)

β€’ Mass (me) = 9.11x10-31 kg

β€’ Charge (qe) = -1.6x10-19 C (-e)

β€’ Rest energy = 0.511 MeV

β€’ Electrons are relativistic when they have kinetic energy above about 100 keV.

 Proton (p, H+)

β€’ Mass (mp) = 1.67x10-27 kg οƒ  mi = Amp (A: atomic mass number)

β€’ Charge (qp) = +1.6x10-19 C (+e) οƒ  qi = Z*qp (Z*: charge state of the ion)

β€’ Rest energy = 938.27 MeV

β€’ Because of the high rest energy, we can use Newtonian dynamics to predict the motion of ions in many applications.

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Beam

 Although single charged particles may be useful for some physics experiments, we need large numbers of energetic particles for most applications. A flux of particles is a beam when the following two conditions hold:

β€’ The particles travel in almost the same direction.

β€’ The particles have a small spread in kinetic energy.

 A beam is an ordered flow of charged particles. A disordered set of particles, such as a thermal plasma, is not a beam.

 The degree of order in a flow of particles is called coherence.

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Charged particle beam parameters

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Description of particle dynamics

 The central issue in beam physics is the solution of collective problems involving large numbers of particles.

 Collective physics is a science of approximation.

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Particle dynamics

 The special theory of relativity states that the inertia of a particle observed in a frame of reference depends on the magnitude of its speed in that frame.

 The inertia of a particle is proportional to 𝛾𝛾. The apparent mass is π‘šπ‘š = π›Ύπ›Ύπ‘šπ‘š0.

 The particle momentum, a vector quantity, equals 𝒑𝒑 = π›Ύπ›Ύπ‘šπ‘š0𝒗𝒗.

 The equation of motion:

 The kinetic energy equals the total energy minus the rest energy:

 Newtonian dynamics describes the motion of low-energy particles when 𝑇𝑇 β‰ͺ π‘šπ‘š0𝑐𝑐2.

𝛾𝛾 = 1

1 βˆ’ 𝑣𝑣/𝑐𝑐 2 = 1

1 βˆ’ 𝛽𝛽2

𝑑𝑑𝒑𝒑

𝑑𝑑𝑑𝑑 = 𝑑𝑑(π›Ύπ›Ύπ‘šπ‘š0𝒗𝒗)

𝑑𝑑𝑑𝑑 = 𝑭𝑭

𝑇𝑇 = 𝛾𝛾 βˆ’ 1 π‘šπ‘š0𝑐𝑐2

Lorentz factor

(7)

Transfer matrix

 Most beam transport devices, such as charged particle lenses and bending

magnets, apply transverse forces that are linearly proportional to the distance of a particle from a preferred axis.

 To specify the orbit of the particle in the x-direction, we must give its position, x, and velocity, vx. The convention in charged-particle optics is to represent particle orbits in terms of their angle relative to the main axis, rather than the transverse velocity. In the limit that 𝑣𝑣π‘₯π‘₯ β‰ͺ 𝑣𝑣𝑧𝑧, the angle is

 If the x-directed forces in the device are linear, then we can express the exit vector as a linear combination of the entrance vector components:

 The quantities amn depend on the distribution of forces. Without acceleration, the determinant of the transfer matrix equals unity.

π‘₯π‘₯

β€²

= 𝑑𝑑π‘₯π‘₯ 𝑑𝑑𝑑𝑑 β‰ˆ

𝑣𝑣

π‘₯π‘₯

𝑣𝑣

𝑧𝑧

π‘₯π‘₯

1

π‘₯π‘₯

1β€²

= π‘Žπ‘Ž

11

π‘Žπ‘Ž

12

π‘Žπ‘Ž

21

π‘Žπ‘Ž

22

π‘₯π‘₯

0

π‘₯π‘₯

0β€²

Transfer matrix

Exit vector Entrance vector

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Transfer matrix

 If a particle travels through linear device A and then through device B, the final orbit vector is

 The orbit vector transformation from any combination of one-dimensional focusing elements is a single transfer matrix, the product of the individual matrices of all the elements.

 The particle orbit vector for a two-dimensional focusing system is 𝒙𝒙 = [π‘₯π‘₯,π‘₯π‘₯π‘₯,𝑦𝑦,𝑦𝑦π‘₯]. A 4Γ—4 matrix represents the effect of a general linear focusing element or

system.

 In many practical devices, such as quadrupole lens arrays, the forces in the π‘₯π‘₯ and 𝑦𝑦 directions are independent. Then, we can calculate motion in π‘₯π‘₯ and 𝑦𝑦 separately using individual 2Γ—2 matrices.

π‘₯π‘₯

2

π‘₯π‘₯

2β€²

= 𝑏𝑏

11

𝑏𝑏

12

𝑏𝑏

21

𝑏𝑏

22

π‘Žπ‘Ž

11

π‘Žπ‘Ž

12

π‘Žπ‘Ž

21

π‘Žπ‘Ž

22

π‘₯π‘₯

0

π‘₯π‘₯

0β€²

𝒙𝒙

𝟐𝟐

= 𝑩𝑩 𝑨𝑨𝒙𝒙

𝟎𝟎

= 𝑩𝑩𝑨𝑨 𝒙𝒙

𝟎𝟎

= π‘ͺπ‘ͺ𝒙𝒙

𝟎𝟎
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Phase dynamics

 Despite differences in geometry, all radio-frequency accelerators use a traveling electromagnetic wave to accelerate charged particles. For ion acceleration, the axial component of the electric field on the axis has the form:

 Axial variation of the electric field:

 The wave can accelerate particles to high energy only if they stay within the region of accelerating electric field. In other words, the particles must remain at about the same phase of the accelerating wave. This means that the wave

phase-velocity must increase to match the velocity of the accelerating particles.

𝐸𝐸

𝑧𝑧

𝑑𝑑, 𝑑𝑑 = 𝐸𝐸

0

sin[π‘˜π‘˜ 𝑑𝑑 𝑑𝑑 βˆ’ πœ”πœ”π‘‘π‘‘]

(10)

Synchronous particle

 The wave accelerates particles with phase in the range 0 < πœ™πœ™ < πœ‹πœ‹ and decelerates particles in the phase range βˆ’πœ‹πœ‹ < πœ™πœ™ < 0 .

𝑑𝑑𝑣𝑣

𝑠𝑠

𝑑𝑑

𝑑𝑑𝑑𝑑 = π‘žπ‘žπΈπΈ

0

sin πœ™πœ™

𝑠𝑠

π‘šπ‘š

0

 We can define conditions where a particle stays at a constant phase. A particle with this property is a synchronous particle – its phase is the synchronous phase, πœ™πœ™π‘ π‘ .

 Figure shows that the synchronous particle experiences a constant axial electric field, 𝐸𝐸𝑧𝑧𝑠𝑠 = 𝐸𝐸0 sinπœ™πœ™π‘ π‘ .

 The velocity of the synchronous particle changes as:

 The accelerating structure must vary along its

length so that the wave number is

π‘˜π‘˜ 𝑑𝑑 = πœ”πœ” 𝑣𝑣

𝑠𝑠

𝑑𝑑

Conditions for having synchronous particles in an accelerator

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Non-synchronous particle

 Under some conditions non-synchronous particles have stable oscillations about the synchronous particle position, 𝑑𝑑𝑠𝑠.

 Let 𝑑𝑑 and 𝑣𝑣 be the axial position and velocity of a non-synchronous particle. We define the small quantities:

 Then, we obtain

 The instantaneous acceleration of the non-synchronous particle is:

 The general phase equations for non-relativistic particles:

𝑑𝑑

2

𝑑𝑑

𝑑𝑑𝑑𝑑

2

= 𝑑𝑑𝑣𝑣

𝑑𝑑𝑑𝑑 = π‘žπ‘žπΈπΈ

0

sin πœ™πœ™ π‘šπ‘š

0

𝑑𝑑

2

βˆ†π‘‘π‘‘

𝑑𝑑𝑑𝑑

2

= π‘žπ‘žπΈπΈ

0

sin πœ™πœ™

π‘šπ‘š

0

βˆ’ 𝑑𝑑

2

𝑑𝑑

𝑠𝑠

𝑑𝑑𝑑𝑑

2

= π‘žπ‘žπΈπΈ

0

π‘šπ‘š

0

sin πœ™πœ™ βˆ’ sin πœ™πœ™

𝑠𝑠

πœ™πœ™ = πœ™πœ™

𝑠𝑠

βˆ’ πœ”πœ”βˆ†π‘‘π‘‘/𝑣𝑣

𝑠𝑠
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Non-synchronous particle

 If 𝐸𝐸0 and 𝑣𝑣𝑠𝑠 are almost constant during an axial oscillation of a non-synchronous particle, then we obtain a non-linear differential equation as following:

 For small oscillations about the phase of the synchronous particle, βˆ†πœ™πœ™ β‰ͺ πœ™πœ™π‘ π‘ , the above equation reduces to:

οƒ  If cosπœ™πœ™π‘ π‘  > 0, the axial oscillations of non-synchronous particles are stable.

 The conditions for synchronized particle acceleration are cosπœ™πœ™π‘ π‘  > 0 and sinπœ™πœ™π‘ π‘  >

0, or

 The conditions for synchronized particle deceleration are cosπœ™πœ™π‘ π‘  > 0 and sinπœ™πœ™π‘ π‘  <

0, or

𝑑𝑑

2

πœ™πœ™

𝑑𝑑𝑑𝑑

2

β‰… βˆ’ πœ”πœ”π‘žπ‘žπΈπΈ

0

π‘šπ‘š

0

𝑣𝑣

𝑠𝑠

sin πœ™πœ™ βˆ’ sin πœ™πœ™

𝑠𝑠

𝑑𝑑

2

βˆ†πœ™πœ™

𝑑𝑑𝑑𝑑

2

β‰… βˆ’ πœ”πœ”π‘žπ‘žπΈπΈ

0

π‘šπ‘š

0

𝑣𝑣

𝑠𝑠

cos πœ™πœ™

𝑠𝑠

βˆ†πœ™πœ™

0 < πœ™πœ™

𝑠𝑠

< πœ‹πœ‹/2 (acceleration)

βˆ’πœ‹πœ‹/2 < πœ™πœ™

𝑠𝑠

< 0 (deceleration)

(13)

Configuration space vs phase space

 Lamina phase flow is the foundation for theories of collective behavior.

(π‘₯π‘₯(𝑑𝑑), 𝑦𝑦(𝑑𝑑), 𝑑𝑑(𝑑𝑑))

(π‘₯π‘₯, 𝑦𝑦, 𝑑𝑑, 𝑣𝑣

π‘₯π‘₯

, 𝑣𝑣

𝑦𝑦

, 𝑣𝑣

𝑑𝑑

)

(14)

Examples of phase space description

 The trajectories of particles accelerated by a constant axial electric field 𝐸𝐸𝑑𝑑:

 Trajectories of particles in a linear focusing force 𝐹𝐹π‘₯π‘₯ = βˆ’π‘Žπ‘Žπ‘₯π‘₯:

𝑑𝑑 𝑑𝑑 = 𝑑𝑑0 + 𝑣𝑣𝑧𝑧0𝑑𝑑 + π‘žπ‘žπΈπΈπ‘§π‘§β„π‘šπ‘š0 𝑑𝑑2/2 𝑣𝑣𝑧𝑧 𝑑𝑑 = 𝑣𝑣𝑧𝑧0 + π‘žπ‘žπΈπΈπ‘§π‘§β„π‘šπ‘š0 𝑑𝑑

π‘₯π‘₯ 𝑑𝑑 = π‘₯π‘₯0 cos(πœ”πœ”π‘‘π‘‘ + πœ™πœ™)

πœ”πœ” = π‘Žπ‘Ž/π‘šπ‘š0

𝑣𝑣π‘₯π‘₯ 𝑑𝑑 = βˆ’π‘₯π‘₯0πœ”πœ”sin(πœ”πœ”π‘‘π‘‘ + πœ™πœ™)

300 keV protons with a betatron wavelength of 0.3 m

Protons in an electric field of 105 V/m

(15)

Phase space description for relativistic particles

 The relativistic equations of motion

 Normalization:

𝑑𝑑π‘₯π‘₯

𝑑𝑑𝑑𝑑 = 𝑝𝑝π‘₯π‘₯

π›Ύπ›Ύπ‘šπ‘š0 = 𝑝𝑝π‘₯π‘₯

π‘šπ‘š0 1 + 𝑝𝑝π‘₯π‘₯2/π‘šπ‘š02𝑐𝑐2 𝑑𝑑𝑝𝑝π‘₯π‘₯

𝑑𝑑𝑑𝑑 = βˆ’π‘Žπ‘Žπ‘₯π‘₯

π›Ύπ›Ύπ‘šπ‘š0𝑐𝑐2 2 = 𝑐𝑐𝑝𝑝π‘₯π‘₯ 2 + π‘šπ‘š0𝑐𝑐2 2

𝑑𝑑𝑑𝑑

𝑑𝑑𝑇𝑇 = 𝑃𝑃π‘₯π‘₯ 1 + 𝑃𝑃π‘₯π‘₯2 𝑑𝑑𝑃𝑃π‘₯π‘₯

𝑑𝑑𝑇𝑇 = βˆ’π›Όπ›Όπ‘‘π‘‘

where, 𝛼𝛼 = π‘Žπ‘Žπ‘₯π‘₯02/π‘šπ‘š0𝑐𝑐2

𝑇𝑇 = 𝑑𝑑/(π‘₯π‘₯0⁄𝑐𝑐) 𝑑𝑑 = π‘₯π‘₯/π‘₯π‘₯0 𝑃𝑃π‘₯π‘₯ = 𝑝𝑝π‘₯π‘₯/π‘šπ‘š0𝑐𝑐

𝛼𝛼 = 0.5

𝛼𝛼 = 5

𝛼𝛼 = 5

(16)

Conservation of phase space volume

 Conservation of the phase-space volume occupied by a particle distribution is a fundamental theorem of collective physics. (Liouville’s theorem: the principle of incompressiblity of a phase fluid)

Same area

(17)

Maxwell distribution

 Particles in an isotropic Maxwell distribution are in thermal equilibrium. They have a spread in kinetic energy.

 For a single species in thermal equilibrium with itself (e.g. electrons), in the absence of time variation, spatial gradients, and accelerations, the Boltzmann equation reduces to

 Then, we obtain the Maxwell-Boltzmann velocity distribution

𝑓𝑓 𝑣𝑣 = 2

πœ‹πœ‹ π‘šπ‘š π‘˜π‘˜π‘‡π‘‡

3 𝑣𝑣2𝑒𝑒π‘₯π‘₯𝑝𝑝 βˆ’π‘šπ‘šπ‘£π‘£2 2π‘˜π‘˜π‘‡π‘‡ 𝑓𝑓 πœ€πœ€ = 2

πœ‹πœ‹ πœ€πœ€ π‘˜π‘˜π‘‡π‘‡

1/2 𝑒𝑒π‘₯π‘₯𝑝𝑝 βˆ’ πœ€πœ€ π‘˜π‘˜π‘‡π‘‡

 The mean speed

̅𝑣𝑣 = 8π‘˜π‘˜π‘‡π‘‡ πœ‹πœ‹π‘šπ‘š

1/2

πœ•πœ•π‘“π‘“οΏ½

πœ•πœ•π‘‘π‘‘ 𝑐𝑐 = 0

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Displaced Maxwell distribution

 Charged particle beams are non-isotropic and usually almost monoenergetic. In a sense, the primary goal of beam technology is to create non-Maxwellian

distributions and to preserve them over time scales set by the application.

 A common assumption used in beam theory is that the particles have a Maxwell distribution when observed in the beam rest frame. The transformed distribution observed in the stationary frame of the accelerator is called a displaced Maxwell distribution.

 For example, consider a nonrelativistic ion beam extracted from a plasma source with ion temperature 𝑇𝑇𝑖𝑖. The beam is axially bunched passing through a radio- frequency quadrupole accelerator. The beam emerges from the accelerator with kinetic energy 𝐸𝐸0. We can represent the exit beam distribution in the stationary frame as

𝑓𝑓 𝑣𝑣π‘₯π‘₯,𝑣𝑣𝑦𝑦,𝑣𝑣𝑧𝑧 ~ 𝑒𝑒π‘₯π‘₯𝑝𝑝 βˆ’π‘šπ‘šπ‘–π‘–(𝑣𝑣π‘₯π‘₯2 + 𝑣𝑣𝑦𝑦2)

2π‘˜π‘˜π‘‡π‘‡π‘–π‘– 𝑒𝑒π‘₯π‘₯𝑝𝑝 βˆ’π‘šπ‘šπ‘–π‘–(𝑣𝑣𝑧𝑧 βˆ’ 𝑣𝑣0)2 2π‘˜π‘˜π‘‡π‘‡π‘–π‘–β€² 𝑣𝑣0 = 2𝐸𝐸0

π‘šπ‘šπ‘–π‘–

1/2

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