Informatics Educational Institutions & Programs

Radiation damping in accelerator physics is a phenomenum where betatron oscillations and longitudinal oscilations of the particle are damped due to energy loss by synchrotron radiation. It can be used to reduce the beam emittance of a high-velocity charged particle beam.

The two main ways of using radiation damping to reduce the emittance of a particle beam are the use of undulators and damping rings (often containing undulators), both relying on the same principle of inducing synchrotron radiation to reduce the particles' momentum, then replacing the momentum only in the desired direction of motion.

Damping rings

As particles are moving in a closed orbit, the lateral acceleration causes them to emit synchrotron radiation, thereby reducing the size of their momentum vectors (relative to the design orbit) without changing their orientation (ignoring quantum effects for the moment). In longitudinal direction, the loss of particle impulse due to radiation is replaced by accelerating sections (RF cavities) that are installed in the beam path so that an equilibrium is reached at the design energy of the accelerator. Since this is not happening in transverse direction, where the emittance of the beam is only increased by the quantization of radiation losses (quantum effects), the transverse equilibrium emittance of the particle beam will be smaller with large radiation losses, compared to small radiation losses.

Because high orbit curvatures (low curvature radii) increase the emission of synchrotron radiation, damping rings are often small. If long beams with many particle bunches are needed to fill a larger storage ring, the damping ring may be extended with long straight sections.

Undulators and wigglers

When faster damping is required than can be provided by the turns inherent in a damping ring, it is common to add undulator or wiggler magnets to induce more synchrotron radiation. These are devices with periodic magnetic fields that cause the particles to oscillate transversely, equivalent to many small tight turns. These operate using the same principle as damping rings and this oscillation causes the charged particles to emit synchrotron radiation.

The many small turns in an undulator have the advantage that the cone of synchrotron radiation is all in one direction, forward. This is easier to shield than the broad fan produced by a large turn.

Energy loss

The power radiated by a charged particle is given by a generalization of the Larmor formula derived by Liénard in 1898 ^[1] ^[2]

P={\frac {e^{2}}{6\pi \epsilon _{0}c^{3}}}\gamma ^{6}\left[({\dot {v}})^{2}-{\frac {({v}\times {\dot {v}})^{2}}{c^{2}}}\right]

, where

v=\beta c

is the velocity of the particle,

{\dot {v}}={\frac {dv}{dt}}

the acceleration, e the elementary charge,

\epsilon _{0}

the vacuum permittivity,

\gamma

the Lorentz factor and

c

the speed of light.

Note:

p=\gamma m_{0}v

is the momentum and

m_{0}

is the mass of the particle.

{\frac {d\gamma }{dt}}=\gamma ^{3}{\frac {v.{\dot {v}}}{c^{2}}}

{\frac {dp}{dt}}=\gamma ^{3}{\frac {v.{\dot {v}}}{c^{2}}}m_{0}v+\gamma m_{0}{\dot {v}}

Linac and RF Cavities

In case of an acceleration parallel to the longitudinal axis ( ${v}\times {\dot {v}}=0$ ), the radiated power can be calculated as below

{\frac {dp_{\parallel }}{dt}}=\gamma ^{3}m_{0}{\dot {v}}

Inserting in Larmor's formula gives

P_{\parallel }={\frac {e^{2}}{6\pi \epsilon _{0}{m_{0}}^{2}c^{3}}}\left({\frac {dp_{\parallel }}{dt}}\right)^{2}

Bending

In case of an acceleration perpendicular to the longitudinal axis ( ${v}.{\dot {v}}=0$ )

{\frac {dp_{\perp }}{dt}}=\gamma m_{0}{\dot {v}}

Inserting in Larmor's formula gives (Hint: Factor $1/(\gamma m_{0})^{2}$ and use $1-v^{2}/c^{2}=1/\gamma ^{2}$ )

P_{\perp }={\frac {e^{2}\gamma ^{2}}{6\pi \epsilon _{0}{m_{0}}^{2}c^{3}}}\left({\frac {dp_{\perp }}{dt}}\right)^{2}

Using magnetic field perpendicular to velocity

F_{\perp }={\frac {dp_{\perp }}{dt}}=ev\times B

P_{\gamma }={\frac {e^{2}\gamma ^{2}}{6\pi \epsilon _{0}{m_{0}}^{2}c^{3}}}\left(e\beta cB\right)^{2}={\frac {e^{4}\beta ^{2}\gamma ^{2}B^{2}}{6\pi \epsilon _{0}{m_{0}}^{2}c}}={\frac {e^{4}}{6\pi \epsilon _{0}{m_{0}}^{4}c^{5}}}\beta ^{2}E^{2}B^{2}

Using radius of curvature ${\dot {v}}={\frac {\beta ^{2}c^{2}}{\rho }}$ and inserting $\gamma m_{0}{\dot {v}}$ in $P_{\perp }$ gives

P_{\gamma }={\frac {e^{2}c}{6\pi \epsilon _{0}}}{\frac {\beta ^{4}\gamma ^{4}}{\rho ^{2}}}

Electron

Here are some usefull formulas to calculate the power radiated by an electron accelerated by a magnetic field perpendicular to the velocity and $\beta \approx 1$ .^[3]

P_{\gamma }={\frac {e^{4}}{6\pi \epsilon _{0}{m_{e}}^{4}c^{5}}}E^{2}B^{2}

where $E=\gamma m_{e}c^{2}$ , $B$ is the perpendicular magnetic field, $m_{e}$ the electron mass.

P_{\gamma }={\frac {e^{2}}{6\pi \epsilon _{0}c^{3}}}{\frac {\gamma ^{4}}{\rho ^{2}}}

Using the classical electron radius $r_{e}$

P_{\gamma }={\frac {2}{3}}{\frac {r_{e}c}{(m_{e}c^{2})^{3}}}{\frac {E^{4}}{\rho ^{2}}}={\frac {2}{3}}{\frac {r_{e}c}{m_{e}c^{2}}}{\frac {\gamma ^{2}E^{2}}{\rho ^{2}}}={\frac {2}{3}}r_{e}c{\frac {\gamma ^{3}E}{\rho ^{2}}}={\frac {2}{3}}r_{e}m_{e}c^{3}{\frac {\gamma ^{4}}{\rho ^{2}}}

where $\rho$ is the radius of curvature, $\rho ={\frac {E}{ecB}}$

$\rho$ can also be derived from particle coordinates (using common 6D phase space coordinates system x,x',y,y',s, $\Delta p/p$ ):

\rho =\left|{\frac {ds}{d\varphi }}\right|\approx {\frac {\Delta _{s}}{\sqrt {{\Delta _{x'}}^{2}+{\Delta _{y'}}^{2}}}}

Note: The transverse magnetic field is often normalized using the magnet rigidity: $B\rho ={\frac {10^{9}}{c}}E_{[GeV]}\approx 3.3356E_{[GeV]}[Tm]$ ^[4]