Changeset 741 in ETALON for papers/2016_HDR_ND/Advanced_diags/smithpurcell.tex
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papers/2016_HDR_ND/Advanced_diags/smithpurcell.tex
r736 r741 316 316 This relation is purely a consequence of the fact that waves emitted by a grating will interfere and in each direction constructive interferences correspond to specific wavelengths. 317 317 318 The intensity of radiation emitted by a single electron (single electron yield), per unit solid angle ($\Omega$) and per frequency ($\omega$)is given by318 The intensity of radiation emitted by a single electron (single electron yield), per unit solid angle ($\Omega$) is given by 319 319 \begin{eqnarray} 320 \frac{d ^2I_1}{d\omega d\Omega} & = & \frac{e^2 \omega^2 l^2}{4 \pi^2 c^3}R^2 \exp{\frac{-2 x_0 }{\lambda_e}}320 \frac{dI_1}{d\Omega} & = & \frac{L}{l^2}\frac{2 \pi e^2 n^2 \beta^2}{\left(1 - \beta \cos \theta\right)^3}R^2 \exp{\frac{-2 x_0 }{\lambda_e}} 321 321 \end{eqnarray} 322 where $e$ is the electron charge, $x_0$ is the beam grating separation, $\lambda_e$ is the evanescent wavelength of the virtual radiation emitted by the beam and $R^2$ is a factor reflecting the coupling of the beam with the grating. 322 where $e$ is the electron charge, $L$ the grating length, $x_0$ is the beam grating separation, $\lambda_e$ is the evanescent wavelength of the virtual radiation emitted by the beam and $R^2$ is a factor reflecting the coupling of the beam with the grating. 323 324 323 325 324 326 The evanescent wavelength is given by … … 329 331 where $\gamma$ is the Lorentz factor, $\phi$ is the azimuthal angle (the ascension above or below the plane perpendicular to the grating surface and passing by the beam). 330 332 333 An example of values of single electron yield taken from~\cite{delerue:in2p3-01322166} is shown on figure~\ref{fig:sey2d}. 334 335 \begin{figure}[htbp] 336 \centering 337 \includegraphics[width=80mm]{Advanced_diags/MOPMB003f2.pdf} 338 \caption{Single electron yield of Smith-Purcell radiation for a $40\times180$ \si{mm^2} grating with a 8~mm pitch and a$30^o$ blaze angle. Image taken from~\cite{delerue:in2p3-01322166}. } 339 \label{fig:sey2d} 340 \end{figure} 341 342 331 343 332 344 As discussed above, equation~\ref{eq:coherent} applies to Smith-Purcell Radiation and the total radiation intensity emitted from a charged particle bunch of multiplicity $N$ is given by: 333 345 \begin{eqnarray} 334 \frac{d ^2I}{d\omega d\Omega} & = & \frac{d^2I_1}{d\omegad\Omega} \left[ N + N(N-1) \mathcal{F}(\omega) \right]346 \frac{dI}{ d\Omega} & = & \frac{dI_1}{ d\Omega} \left[ N + N(N-1) \mathcal{F}(\omega) \right] 335 347 \label{eq:SP_coherent} 336 348 \end{eqnarray} 337 349 where $\mathcal{F}(\omega)$ is the form factor introduced in equation~\ref{eq:form_factor}. 338 350 351 On figure~\ref{fig:compare_profiles} one can see a comparison of different profiles with the same FWHM (\SI{5}{ps}) but with different shapes and how this changes the expected CSPR signal. 352 353 \begin{figure}[htbp] 354 \centering 355 \includegraphics*[width=70mm]{Advanced_diags/shape_profile.eps} 356 \includegraphics*[width=70mm]{Advanced_diags/shape_comparison.eps} 357 \caption{Comparison of several bunch profiles with the same FWHM (\SI{5}{ps}) but with different shapes (left) and predicted CSPR signal for each of these profiles (right). The capability to distinguish internal features of the beam and in particular substructures appears clearly. The parameters used for these simulations are based on the experiment done at CLIO (see section~\ref{sec:CLIO}).} 358 \label{fig:compare_profiles} 359 \end{figure} 360 361 362 363 339 364 One important difference between CSPR and other radiative methods is that the choice of the grating will change the radiation intensity observed at different frequencies. On figure~\ref{fig:grating_effect} one can see the radiation intensities observed for the same bunch profile but with different gratings pitches. 340 365 … … 342 367 \center 343 368 \includegraphics[width=7.5cm]{Advanced_diags/SP_signal_different_gratings.eps} 344 \caption{Radiation profiles observed for the same pulse but for different grating pitches. }369 \caption{Radiation profiles observed for the same pulse but for different grating pitches. The parameters used for these simulations are based on the experiment done at CLIO (see section~\ref{sec:CLIO}).} 345 370 \label{fig:grating_effect} 346 371 \end{figure} … … 360 385 \end{eqnarray} 361 386 362 This has led me to study with a student~\cite{rapport_duval} whether it would be possible to benefit from the advanced work done in the field of grating theory~\cite{diffraction_gratings_Loewen} to estimate $R^2$. We produced some predictions but these are rather close to what has been obtained with simulation codes based on~\cite{Brownell:2005my} and therefore we have not yet been able to distinguish the two approaches. This may become possible at the experiment described in~\ref{sec:CLIO}.387 This has led me to study with two students~\cite{rapport_solene,rapport_duval} whether it would be possible to benefit from the advanced work done in the field of grating theory~\cite{diffraction_gratings_Loewen} to estimate $R^2$. We produced some predictions but these are rather close to what has been obtained with simulation codes based on~\cite{Brownell:2005my} and therefore we have not yet been able to distinguish the two approaches. This may become possible at the experiment described in~\ref{sec:CLIO}. 363 388 364 389 … … 456 481 457 482 483 \subsubsection{Near field, far field and pre-wave effects} 484 485 As the Smith-Purcell radiation is formed by a grating, there is a formation length and the number of teeth of the grating, the distance between the grating and the detector have to be taken into account. 486 The line width of the radiation is given by the formula: 487 \begin{equation} 488 \frac{\delta \lambda}{ \lambda} = \frac{l}{nL} 489 \end{equation} 490 491 The effect of the grating-detector distance has been discussed in details in~\cite{E203prstab}. 492 493 With a student I also studied the predictions for the pre-wave effect~\cite{malovystia-2015} and this work shows that corrections might have to be applied, especially at very high energy. However owing to the non observation of this effect in~\cite{1748-0221-6-07-P07004} as discussed in section \ref{sec:OTR_interference}, experimental verification of the effect of pre-wave interferences and accurate calculation are needed. Experimental attempts will be discussed in section~\ref{sec:SPESO}. 494 458 495 459 496 \section{Experimental study of Coherent Smith-Purcell radiation} 460 497 461 One of the remaining difficulties preventing the adoption of Smith-Purcell radiation as a longitudinal profile is that 462 463 464 \subsection{Smith-Purcell radiation measurement at FACET} 465 \subsection{Smith-Purcell radiation measurement at SOLEIL} 466 \subsection{Smith-Purcell radiation measurement at CLIO} 467 \label{sec:CLIO}. 468 469 470 471 472 Image CLIO 3 diff profiles 498 When I joined the effort at the University of Oxford on CSPR our main goal was to demonstrate that CSPR could be used as a longitudinal profile diagnostic in the sub-picosecond regime. The work would lead to the E-203 collaboration that took data at SLAC. Later, after I moved to Orsay, I decided to extend this effort to better understand the properties of CSPR using a test setup installed at SOLEIL and called SPESO and to also study how to make CSPR a tool available in accelerators control room, by making experiments on the CLIO accelerator. 499 500 \subsection{Smith-Purcell radiation measurement at FACET: E-203} 501 502 FACET (Facility for Advanced Accelerator Experimental Tests) was a \SI{20}{GeV} electron accelerator installed on the SLAC campus in Stanford, California~\cite{Seryi:2009zzc}. It had the advantage of being the only test facility offering easy access to sub-picosecond bunches. 503 504 In 2010 we proposed to re-use the hardware from a previous experiment~\cite{Doucas_ESB} to use it at FACET to measure sub-picosecond bunches. This led to the formation of the E-203 collaboration. 505 506 The experiment has been described in details in~\cite{SP_E203_first_paper}. It consists of a carousel on which 3 different gratings and a blank (a flat grating without teeth are mounted). This carousel can be moved inside the accelerator vacuum to bring the grating close from the beam. Opposite to the carousel there are 11 silicon windows located every \ang{10} in $\theta$ from \ang{40} to \ang{140}. Outside the movable windows waveguide array plates (WAP) filters are used to filter only the radiation at the wavelength expected from the selected grating. After the filters Winston cones concentrate the radiation within their acceptance onto pyroelectric detectors. Several pictures of the E-203 experiment are shown on figure~\ref{fig:E_203_setup} and the optical elements are shown on figure~\ref{fig:E_203_setup_optics}. 507 508 509 %\vspace*{1cm} 510 \begin{figure}[htbp] 511 \centering 512 \begin{tabular}{cc} 513 \vspace*{-0.5cm} & \multirow{3}{*}{\includegraphics*[width=68mm,angle=90]{Advanced_diags/E203_motor_side.JPG}} \\ 514 \includegraphics*[width=50mm,angle=0]{Advanced_diags/E203_filters_side.JPG} \\ 515 \includegraphics*[width=50mm]{Advanced_diags/E203_carousel.JPG} 516 \end{tabular} 517 \caption{The E-203 experiment (during pre-installation tests) seen from the detectors side (top left), from the motors side (right) and the grating's carousel (bottom left). Images taken from~\cite{andrews:in2p3-00830708}.} 518 \label{fig:E_203_setup} 519 \end{figure} 520 521 \begin{figure}[htbp] 522 \centering 523 \hspace*{-.0cm} \begin{tabular}{ccc} 524 \includegraphics*[height=60mm]{Advanced_diags/E203_filters.png} \hspace*{-2cm}& 525 \includegraphics*[height=60mm]{Advanced_diags/E203_Winston_cone.png} & 526 \includegraphics*[height=60mm]{Advanced_diags/E203_optics.png} 527 \end{tabular} 528 \caption{The optical parts of the E-203 experiment: (from left to right) the filters, the optical concentrators (winston cones) and the optical assembly (image taken from~\cite{E203prstab}).} 529 \label{fig:E_203_setup_optics} 530 \end{figure} 531 532 The experiment was successful in measuring sub-picosecond bunches~\cite{SP_E203_first_paper,E203prstab,andrews:in2p3-00830708}. and examples of the profiles measured are shown on figure~\ref{fig:E_203_profiles}. 533 534 535 536 %\vspace*{1cm} 537 \begin{figure}[htbp] 538 \centering 539 \begin{tabular}{cc} 540 \includegraphics*[width=75mm]{Advanced_diags/E203_high_comp_rho.png} & 541 \includegraphics*[width=75mm]{Advanced_diags/E203_high_comp_profile.png} \\ 542 \includegraphics*[width=75mm]{Advanced_diags/E203_med_comp_profile.png} & 543 \includegraphics*[width=75mm]{Advanced_diags/E203_low_comp_profile.png} \\ 544 \end{tabular} 545 \caption{ Top left: The magnitude of the Fourrier Transform of the time profile of the bunch for a ?high compression? run on the 9 April 2013 (see text in~\cite{E203prstab}). Other plots: bunch profile reconstructed from measurements at different times and with different bunch compression settings (top right: 9 April 2013, high compression; bottom left: 9 April 2013, medium compression; bottom right: 25 june 2013). Plots taken from~\cite{E203prstab} where more explanations can be found.} 546 \label{fig:E_203_profiles} 547 \end{figure} 548 549 Background rejection is an important problem for radiative measurements. Because CSPR uses the dispersion induced by the grating it is less sensitive than other methods but still not immune. One method to measure the background is to expose a "blank" grating, that is a grating without teeth, to the beam and measure the signal produced. This signal is then considered to be the background. 550 551 Another solution could be to measure the two polarisation components of the signal: CSPR is known to be polarized whereas most backgrounds aren't. We verified this with the E-203 apparatus~\cite{E203prstab} (see figure~\ref{fig:E203_polar}). and I worked further on that topic with a student who had taken part in the experiment~\cite{rapport_solene}. 552 553 554 \begin{figure}[htbp] 555 \centering 556 \includegraphics*[height=60mm]{Advanced_diags/E203_polar.png} 557 \caption{The measured degree of polarisation of the grating signal as a function of observation angle. The solid line is the theoretically predicted polarisation of CSPR, as a function of wavelength (see text in~\cite{E203prstab} for details; plot taken from~\cite{E203prstab}).} 558 \label{fig:E203_polar} 559 \end{figure} 560 561 562 563 Additional measurements of the polarization and the azimuthal distribution of CSPR have been done by the E-203 experiment and are being analyzed. 564 565 566 \subsection{Smith-Purcell radiation measurement at SOLEIL: SPESO} 567 \label{sec:SPESO} 568 569 Many questions about Smith-Purcell arose when we formed the E-203 collaboration and FACET being far from Europe, it was not the best suited place to make detailed comparison between theory and experimental results. 570 571 With colleagues from Synchrotron SOLEIL I therefore started another experiment called SPESO (Smith-Purcell Experiment at SOLEIL). SPESO is installed at the end the Helios, the SOLEIL linac. For simplicity reasons SPESO uses a fixed grating on a movable arm. Opposite to this window is a z-cut quartz window (transparent at the wavelengths at which the radiation is expected). In front of that window a set of 3 translation stages and 4 rotation stages allow to move detectors in 3D and mesure the intensity of Smith-Purcell radiation at different locations. 572 The layout of the experiment is shown on figure~\ref{fig:SPESOlayout} and a photo is shown on figure~\ref{fig:SPESOphoto}. The experiment has been described in details at~\cite{delerue:in2p3-00862652}. 573 574 %\vspace*{2cm} 575 \begin{figure*}[tbp] 576 \centering 577 \includegraphics*[width=85mm]{Advanced_diags/test_stand_step1_v5_cleaned.pdf} 578 \caption{The experimental setup of SPESO at the end of the SOLEIL Linac (image taken from~\cite{delerue:in2p3-00862652}).} 579 \label{fig:SPESOlayout} 580 \end{figure*} 581 582 %\vspace*{2cm} 583 \begin{figure}[htbp] 584 \centering 585 \hspace*{-0.5cm}\begin{tabular}{cc} 586 \includegraphics*[width=90mm,angle=90]{Advanced_diags/SPESO_layout.jpg} & 587 \includegraphics*[width=0.45\textwidth]{Advanced_diags/MOPAB025f1.jpg} 588 \end{tabular} 589 \caption{The experimental setup of SPESO at the end of the SOLEIL Linac: left, as it was in 2015 (image taken from~\cite{delerue:in2p3-00862652}) and right with the polarizer installed in 2016 (image taken from~\cite{Delerue:IPAC17-SOLEIL}). On both images the electrons travels from left to right. 590 } 591 \label{fig:SPESOphoto} 592 \end{figure} 593 594 The first SPESO signal was difficult to obtain because the pulse length had been underestimated. After some searching we finally found some signal at wavelength much longer than expected (see figure~\ref{fig:SPESO_first_data}). These data allowed us to reconstruct the spectrum emitted by the bunch and its profile (see figure~\ref{fig:SPESO_signal_spectrum}). These results were reported in~\cite{Delerue:2016zgr} where detailed explanations of these figures are available. Discussion with persons who contributed to the commissioning of the linac showed that our measurement is in agreement with the measurements done during the linac commissioning. 595 596 597 598 599 \begin{figure}[htbp] 600 % \vspace*{-.5\baselineskip} 601 \centering 602 \hspace*{-0.5cm}\begin{tabular}{cc} 603 \includegraphics*[width=75mm]{Advanced_diags/MOPMB002f2_negated.png} & \includegraphics*[width=75mm]{MOPMB002f5a.png} 604 \end{tabular} 605 \caption{Left: Example adapted from~\cite{Delerue:2016zgr} of the initial data recorded with the two SPESO detectors (Pink is the Q-band detector and blue is the Ka-band detector, see explanation in~\cite{Delerue:2016zgr}). Right: Example taken from~\cite{Delerue:2016zgr} of raw signal collected with the the Ka-band detector while the detectors were moving vertically. The red line corresponds to the grating in the inserted position and the blue line to the grating in the retracted position (background). } 606 \label{fig:SPESO_first_data} 607 % \vspace*{-\baselineskip} 608 \end{figure} 609 610 611 612 613 \begin{figure}[htbp] 614 % \vspace*{-.5\baselineskip} 615 \centering 616 \hspace*{-1.5cm}\begin{tabular}{cc} 617 \includegraphics[height=45mm]{Advanced_diags/MOPMB002f6.eps} & 618 \includegraphics[height=45mm]{Advanced_diags/MOPMB002f7.eps} 619 \end{tabular} 620 \caption{Images taken from~\cite{Delerue:2016zgr}. Left: Distribution of the signal measured as function of the observation angle. The red dots correspond to the Ka band detector and the blue dots to the Q-band detector. The solid lines correspond to data points at frequencies within the sensitivity range of the detector and the dashed lines to data points at frequencies outside that range. These data are compared to simulations for 4 different bunch FWHM. Right: Bunch profile recovered from the data presented on the left using the method described in~\cite{reco_paper}.} 621 \label{fig:SPESO_signal_spectrum} 622 % \vspace*{-\baselineskip} 623 \end{figure} 624 625 The SPESO experiment has been upgraded in 2016 to study the polarisation of the Smith-Purcell radiation. The result has been presented in~\cite{Delerue:IPAC17-SOLEIL} and is shown in figure~\ref{fig:SPRESO_polarization_2017}. This result is a surprise to us as we expected almost 100\% polarization but it could be compatible with what was observed at FACET (see figure~\ref{fig:E203_polar}). The measurement campaign on SPESO is continuing to increase the range of the measurement. 626 627 628 \begin{figure*}[!htb] 629 % \vspace*{-.5\baselineskip} 630 \centering 631 \includegraphics*[width=70mm]{Advanced_diags/MOPAB025f6.pdf} 632 \caption{Degree of polarisation as function of the longitudinal displacement (along the beam propagation axis). Image taken from~\cite{Delerue:IPAC17-SOLEIL}. } 633 \label{fig:SPRESO_polarization_2017} 634 % \vspace*{-\baselineskip} 635 \end{figure*} 636 637 638 \subsection{Coherent Smith-Purcell radiation measurement at CLIO.} 639 \label{sec:CLIO} 640 641 SPESO is meant to be a test bench to study the properties of Coherent Smith-Purcell Radiation. However to have this diagnostic accepted in control rooms, it is necessary to demonstrate that it can work as a control room tool and produce results quickly. This is the aim of the Smith-Purcell experiment at CLIO. CLIO (Acronym in french for Infrared Laser Center at Orsay - {\em Centre Laser Infrarouge à Orsay}) is a Free Electron Laser installed in Orsay. It has been described in~\cite{Ageron:1989eq,bourdon:in2p3-00020744,Glotin:1992aj}. 642 643 Before installing the experiment we studied the dynamics of the beam and the predicted signal~\cite{delerue:in2p3-01322166}. Example of expected signal are shown on figure~\ref{fig:CLIO_sp-normalised}. To avoid searching the signal for too long in case the pulse length was very different from the expectations we decided to first measure CTR and made a comparison of expected signal level for CTR and CSPR~\cite{delerue:in2p3-01322182}. On figure~\ref{fig:CLIO_CTR_CSPRr} the single electron yield and the predicted spectrum at CLIO are compared. 644 Our conclusion was that using the CLIO parameters and with a beam-grating separation of \SI{3}{mm} we expect a signal (in the range 0.03-3 THz [ 0.1 - 10 mm]) of \SI{8.37e-7}{J} for CSPR and \SI{7.35e-08}{J} for CTR. This result was questioned by a few colleagues but finally accepted and confirmed by independent experimental verifications made at another facility by another group~\cite{PhysRevAccelBeams.20.024701}. 645 646 647 \begin{figure}[!htb] 648 \centering 649 \hspace*{-0.05cm}\begin{tabular}{cc} 650 \includegraphics[width=0.45\linewidth]{Advanced_diags/MOPMB005f6.pdf} & 651 \includegraphics[width=0.45\linewidth]{Advanced_diags/MOPMB005f7.pdf} 652 \end{tabular} 653 654 \caption{ Coherent Smith-Purcell spectrum as a function of the observation angle for different bunch profiles in CLIO. The grating used for these simulations has a pitch of 8~mm and a blaze angle of $30^o$. The left figure gives the energy distribution, the right figure is normalized so that the maximum amplitude of each line is 1. Image taken from~\cite{delerue:in2p3-01322166}. 655 } 656 \label{fig:CLIO_sp-normalised} 657 \end{figure} 658 659 \begin{figure}[htb] 660 \centering 661 \label{sey} 662 \end{figure} 663 664 \begin{figure}[!tbp] 665 \centering 666 \hspace*{-0.05cm}\begin{tabular}{cc} 667 \includegraphics[height=55mm]{Advanced_diags/MOPMB003f1.pdf} & 668 \includegraphics[height=55mm]{Advanced_diags/MOPMB003f9.pdf} 669 \end{tabular} 670 671 \caption{Left: Single electron yield for transition radiation (TR) and Smith-Purcell radiation (SP). The screen diameter for transition radiation is \SI{40}{mm}. The SP single electron yield is presented for different beam-grating separation (\SIlist{3;6;9}{mm}). The grating used here is $40\times180$ \si{mm^2} with 8 mm pitch and $30^o$ blaze angle. The signal is measured as integrated with a \SI{50}{mm} diameter parabolic mirror located \SI{300}{mm} from the beam axis. Right: CSPR and CTR energy density as function of wavelength with the same parameters than on the left figure. Both images are taken from~\cite{delerue:in2p3-01322166}.} 672 \label{fig:CLIO_CTR_CSPRr} 673 \end{figure} 674 675 After a first phase during which we measured CTR to validate the detection chain the experiment has quickly been upgraded with a grating instead of the CTR screen. Unlike the E-203 experiment we use single quartz window to let the radiation out. We also decided to use Off Axis Parabolic mirrors (OAP) instead of Winston cones to focus the radiation of the detectors. Photos of the experiment are shown on figure~\ref{fig:CLIO_expstp} and the experiment has been described in details in~\cite{Delerue:IPAC17-CLIO}. 676 677 \begin{figure} 678 \centering 679 \hspace*{-0.05cm}\begin{tabular}{cc} 680 \includegraphics[height=55mm]{Advanced_diags/20170203_193939_resized.jpg} & 681 \includegraphics[height=55mm]{Advanced_diags/MOPAB026f1.jpg} 682 \end{tabular} 683 684 \caption{The experimental setup for CSPR measurements at CLIO: a set of pyrodectors with off axis parabolic mirrors is placed equidistantly with \ang{7} separation around the window and the experimental chamber with the grating inside (right image taken from~\cite{Delerue:IPAC17-CLIO}). The two images have been taken at different dates and have a different number of detectors.} 685 \label{fig:CLIO_expstp} 686 \end{figure} 687 688 \begin{figure}[!htb] 689 \centering 690 \hspace*{-0.05cm}\begin{tabular}{cc} 691 \includegraphics[height=55mm]{Advanced_diags/MOPAB026f3.pdf} & 692 \includegraphics[height=55mm]{Advanced_diags/MOPAB026f6.pdf} 693 \end{tabular} 694 \caption{Signal amplitude as function of the grating position with respect to the center of the beam for three different detectors angles for a long range (left) and a short range near the beam (right). On the right the data (circles) is compared to a fit (solid line). Images taken form~\cite{Delerue:IPAC17-CLIO}. On the left image the peak between \SI{20}{mm} and \SI{30}{mm} is still under investigations.} 695 \label{fig:CLIO_gscan} 696 \end{figure} 697 698 699 After the publication of~\cite{Delerue:IPAC17-CLIO} further work was done and has been reported in~\cite{rapport_vitalii_CLIO_2017}. The figure~\ref{fig:CLIO_form_factor} shows form factors that were measured on CLIO and figure~\ref{fig:CLIO_profile} shows the reconstructed profile. 700 701 \begin{figure}[!htb] 702 \centering 703 \hspace*{-0.05cm}\begin{tabular}{cc} 704 \includegraphics[height=55mm]{Advanced_diags/FF.eps} & 705 \includegraphics[height=55mm]{Advanced_diags/FF6.eps} 706 \end{tabular} 707 \caption{Form factor measured at CLIO as reported in~\cite{rapport_vitalii_CLIO_2017}. Left: Variation of the form factor when the beam grating separation varies. Right: Variation of the form factor when the buncher phase varies. 708 } 709 \label{fig:CLIO_form_factor} 710 \end{figure} 711 712 \begin{figure}[!htb] 713 \centering 714 \includegraphics[width=\linewidth]{Profile1.eps} 715 \caption{Bunche profile reconstructed on CLIO for different buncher phase as reported in~\cite{rapport_vitalii_CLIO_2017}. 716 } 717 \label{fig:CLIO_profile} 718 \end{figure} 719 720 We 721 722 723 724 Future plans 725 473 726 474 727 475 728 \subsection{Outlook: Application to laser-driven plasma accelerators and ERLs} 476 729 beam grating sep. 477 stability 730 beam stability 731 shot to shot stability 732 ESS 478 733 479 734
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