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Mu2e: A Proposal for a Muon to Electron Conversion Experiment at FERMILAB

Mu2e: A Proposal for a Muon to Electron Conversion Experiment at FERMILAB. James Miller, Boston University. CERN, October 2006. Outline. Brief descriptions of the  -  e - process and the current and proposed experimental limits

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Mu2e: A Proposal for a Muon to Electron Conversion Experiment at FERMILAB

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  1. Mu2e: A Proposal for a Muon to Electron Conversion Experiment at FERMILAB James Miller, Boston University CERN, October 2006

  2. Outline • Brief descriptions of the - e- process and the current and proposed experimental limits • Preliminary look: Could it be done at FNAL? Results of recent meeting at FNAL…. • General design issues of the Mu2e experiment- following the previously proposed but un-funded BNL-MECO approach?

  3. The BNL-based Experiment (MECO) • MECO: one of two experiments on the NSF- RSVP project (along with KOPIO, ) • Cost of MECO by itself was projected at $56 M for the muon beam line magnets + $23 M for the detector system • Project was not funded mainly because the cost to configure and run the AGS, plus to build the experiments was deemed to be too large due cost escalations- however by far most of the cost escalation was not in the MECO costs.

  4. Muon to electron conversion • Measure rate of the lepton flavor violating (LFV) reaction: neutrinoless muonto electron conversion in the field of a nucleus, relative to the ordinary muon capture rate on a nucleus. • Goal: Mu2e (and MECO) Re< 10-16 on Al which is ~ 4000x better than the current limit from SINDRUM II: Re<6.1x10-13 on Ti Reis the ratio of rates measured in a muonic atom, Re={Rate(-+A(N,Z) e-+A(N,Z)} / {Rate(-+A(N,Z) +A’(N+1,Z-1)} L=+1,Le=0  L=0,Le=+1 The conversion electron is monochromatic and has an energy which is typically well above most of the background flux.

  5. e  W What Will Observation of -N  e-N Teach Us? Discovery of -N  e-Nor a similar charged lepton flavor violating (LFV) process will be unambiguous evidence for physics beyond the Standard Model. • For non-degenerate neutrino masses, n oscillations can occur. Discovery of neutrino oscillations required changing the Standard Model to include massive . • Charged LFV processes occur through intermediate states with n mixing. Small n mass differences and mixing angles  expected rate is well below what is experimentally accessible. • Charged LFV processes occurin nearly all scenarios for physics beyond the SM, in many scenarios at a level that Mu2e will detect. • Effective mass reach of sensitivesearches is enormous: well beyondthat accessible with direct searches. One example of new physics, with leptoquarks lmd led 

  6. Sensitivity to Different Muon Conversion Mechanisms Supersymmetry Compositeness Predictions at 10-15 Second Higgs doublet Heavy Neutrinos Heavy Z’, Anomalous Z coupling Leptoquarks After W. Marciano

  7. History of Lepton Flavor Violation Searches 1 - N  e-N +  e++ e+ e+ e- 10-2 10-4 10-6 10-8 10-10 10-12 K0+e-K+++e- MEG Goal(m->eg) SINDRUMII 10-14 FNALm->e Goal  10-16 19401950 1960 1970 1980 1990 2000 2010

  8. Why m-A  e-A ? Some Options to m-A  e-A: • t LFV may be significantly stronger, but experimental challenges are large and solutions are not on the horizon • Kaon LFV no stronger in most models, experimental improvements are difficult. • m->eg decay is more sensitive in photon mediated processes by x200-x400, but is not more sensitive for other types of LFV reactions. (MEG: 10-13) May be experimentally limited by backgrounds to 10-13-10-14. • What could change before next m-A  e-A? • MEG (PSI) may see m->eg at 10-13 to 10-14 • LHC may discover new particles (e.g. supersymmetry). m-A  e-A will be needed to help sort things out, e.g. the flavor structure..

  9. Why m-A->e-A at FNAL? • Tens of man-years are invested in a MECO design which is applicable to FNAL. • Physics case was reviewed repeatedly w/excellent outcome • Well developed conceptual design exists, magnets have preliminary engineering design, some detector prototype work has been completed • Technical case reviewed repeatedly w/excellent outcome • An advanced costing estimate was produced • The continuing neutrino program provides facilities and an accelerator operation well-matched to m->e experimental needs. • A working group has been established to understand how the appropriate proton beam can be supplied at FNAL.

  10. Muonic Atom Formation and Nuclear Capture • A rapid process: low energy - (KE< 30 MeV) stop in target A(N,Z), undergo atomic cascade arriving primarily in atomic 1s state • Bohr radii n/mZ)EmZ2/n2 : 200x smaller radius and 200x more binding energy than atomic electron  1s muon is well inside electron orbits muon formshydrogen-like atom • Hydrogenic Radial wavefunction: Rnl(r)  rl Z3/2 for small r. Prob. of overlap between nucleus and muon wavefunction is proportional to r2lZ3which for small r is large only whenl=0. • Ordinary Muon Capture Rate -A(N,Z) A’(N’,Z’)  a bn cp: <a>~2, <b>~2, <c>~0.1 Fundamental process:  p ->  n Proportional to: (# protons)x(nuclear overlap) ~ Z4 .Capture ~ decay rate for Z=12 • Muon Conversion Rate- + A(N,Z)  A(N,Z) + e Coherent process proportional to (# nucleons)2x(nuclear overlap) ~Z5 Re  high Z preferred. But… - Nucleus

  11. ->e Conversion Rates vs. Z Nucleus Re(Z) / Re(Al) Bound lifetime Atomic Bind. Energy(1s) Conversion Electron Energy Prob decay >700 ns Al(13,27) 1.0 .88 s 0.47 MeV 104.97 MeV 0.45 Ti(22,~48) 1.7 .328 s 1.36 MeV 104.18 MeV 0.16 Au(79,~197) ~0.8-1.5 .0726 s 10.08 MeV 95.56 MeV negligible Plot of Re(Z)/Re(Z=13) For various photon couplings (Rates Normalized to Z=13, Aluminum) Kitano, et al.PRD 66, 096002 (2002) Aluminum is nominal choice for MECO

  12. SINDRUM II A eA Limit Experience of SINDRUM II carried over to the design of beam and experimental apparatus SINDRUM II has thebest limit on this process Prompt Background Cosmic RayBackground Re<6.1x10-13 (in Ti) Magnet: B=1.2 T,1.3 m dia., 1.5 m long Expected Signal Muon Decay in Orbit Experimental signature is 104 MeV eoriginating in a thin Ti stopping target

  13. Classes of background • Prompt: due to beam particles which interact almost immediately when they enter the detector region, producing electrons in the signal region, 100 MeVE106 MeV, or low energy background. • Examples: • Pions: Radiative pion capture, -+A(N,Z)+X. Very high suppression of pions is required, since it is a potentially major background. • Beam electrons: incident on the target and scattering into the detector region. Need to suppress ewith E>100 MeV • In-flight muon decays. Keep p<75 MeV/c to keep Ee<100 MeV • Antiproton annihilations along beam line or near target- (none in SINDRUM II, potential problem at 8 GeV at for MECO at AGS and at FNAL) • Delayed: due to beam particles which take > few hundred nanoseconds before they produce signals in the detectors. • Examples: • Electrons from muon decay in orbit (DIO) • Protons, neutrons, gammas from muon capture • Photons from radiative muon capture • Cosmic Rays- Back/Signal proportional to (run time)/(beam intensity)

  14. Decay of a Muon Bound in Atomic Orbit (- + N(A,Z))bound -> N(A,Z) + e + e +  (DIO) • Decay of a muon bound in an atom is slightly different from ordinary free muon decay… • Nucleus absorbs momentum -> neutrinos can carry zero momentum, with electron recoiling off of the nucleus  electron can take almost all of the muon rest energy, and the endpoint energy is the sameasa potential conversion electron, but fortunately the probability is very low. Ee(max)= (mc2NuclearRecoilEnergy AtomicBindingEnergy) For Z=13 (Al), Atomic BE=0.529 MeV, Recoil energy=0.208 MeV  Ee(max)=104.96 MeV Free muon decay, endpoint =52.8 MeV Muon decay in Al 1s bound state, endpoint=104.96 MeV 104.96 MeV

  15. Major Potential Background: Decay of a Muon Bound in Atomic Orbit (DIO, Continued) ( + N(A,Z))bound -> N(A,Z) + e + e +  • Rate near the maximum energy falls very rapidly. Near endpoint: proportional to (Ee(max)-E)5 • Major potential source of background-Discriminate against it with good electron energy resolution, ~1 MeV FWHM for Rme~10-16 Endpoint E (Al)=104.96 MeV

  16. Simulation of detected spectrum • Assumptions • Re=1x10-16 • Energy resolution 1 MeV (FWHM) • Signal region 103.6<E<105.1 gives 0.05 DIO per AeA parametric curve 0.25 0 10-4 1 Log scale Linear scaleAcceptance, Back as Ethresh varied

  17. Sources of Background, continued • Radiative muon capturein atomic orbit (RMC)- (Regular muon capture + photon):- + A(N,Z))bounde A’(N+1,Z-1) +  followed by asymmetric photon conversion in matter, Ae+e- • Lower endpoint energy than DIO and N->eN • e- Endpoint energy = Endpoint energy = Endpoint(e) - (MA’-MA)c2 • Radiative captureof pions in atomic orbit (RPC), B.R. ~ 1.2% Examples- + A(N,Z))bound A’*(N+1,Z-1) - + A(N,Z))boundX followed by asymmetric eeconversion in matter • Maximum energy ~ 139 MeV, distribution peaks ~ 110 MeV. • A potentially serious source of e- background in the 100-106 MeV region • Pions in the beam line must be greatly suppressed For Al, Emax = 102.5 MeV (Compare 104.96 MeV for NeN) P(E> 100.5 MeV) = 4 x 10-9 P( e+e-, Ee>100.5 MeV)=2.5 x 10-5

  18. Backgrounds, continued • Antiprotons: annihilation on the target or in the beam line can produce background electrons. • The ’s, which come from 0’s, radiative  capture, and other mechanisms, can be very energetic. Pair production, e+e-, can make electrons 100-106 MeV near the conversion electron energy. • An 8 GeV proton beam (FNAL) is above the antiproton production threshold, but the production cross section is low. (SINDRUM II and TRIUMF experiments used 600 MeV proton beam and had no antiprotons). • antiprotons in the beam line must be highly suppressed • In-flight muon decay: Muons with p>75 MeV/c can decay to an electron with E>100 MeV, and need to be suppressed. • Electrons: beam electrons with E> 100 MeV, especially those which scatter from the stopping target, need to be suppressed.

  19. Pulsed Muon Beam • In SINDRUM II and TRIUMFe experiments • Continuous beams of muons were used, fluxes up to few x 107 Hz • Prompt backgrounds (mainly pions) were suppressed by A) vetoing detector events in close time coincidence with signals in beam counters, and/or B) pions were suppressed using degrader in the beam line (range pions~1/2 muons). • Veto method limits the incident muon rate to ~few x 107 Hz. Beam lines at PSI are limited to ~107-108 Hz. Implies ~109-1010 seconds of beam would be required to reach the MECO goal of Re< 10-16. • Approach proposed for FNAL: MECO-like approach • No incident beam counters or pion absorbers. • Use an intensepulsedmuon beam to suppress prompt background • Stop large flux of muons in a target in a narrow time bunch (< 100 ns): ~1011 Hz muon stopping rate, injection pulse spacing ~1.6 s, comparable to muon lifetime of ~0.88 s in atomic orbit in Al • Wait 700 ns after injection until prompt background and background from particles slowly traversing the beam line disappear • Activate detector system from ~ 700 ns after injection until next injection • Attenuate incident beam x109 between injection bunches (extinction) to suppress prompt background (mainly from radiative pion capture) • Build a detector system with high acceptance and good energy resolution for e originating in the stopping target and in energy range 100-106 MeV; and make acceptance as low as possible at lower energies where DIO electrons are copious. • Design a beam line which delivers maximum muon flux but minimal electron background between 100 and 106 MeV for t 00 ns. Minimize number of particles at other energies: antiprotons, muons with p>75 MeV/c, pions

  20. Promptbackgrounds Pulsed Proton Beam Proton pulse • BNL-AGS at reduced energy, 8 GeV, 21013 protons s-1 – 50 kW beam power. FNAL-Booster operates at 8 GeV. • BNL-AGS Revolution time = 2.7 ms with 6 RF buckets for protons. FNAL-Debuncher revolution time=1.6 ms • Match 0.88 ms lifetime of muons in atomic Al: fill 2 AGS RF buckets -> 1.35 ms pulse spacing. Put one bunch in FNAL debuncher -> 1.6 ms pulse spacing • Resonant extraction of temporally narrow (~ 100 ns) bunches • Collect data >700 ns after injection, after most prompt particles in bema are gone. • To eliminate prompt backgrounds, we require< 10-9 protons between bunches for each proton in bunch. We call this the beam extinction. Detection time

  21. 8 GeV Proton sources Proton Linac (H-) 8 GeV? H- t

  22. Mu2e and SNUMI Phase 2 • SNUMI 1: • Uses recycler as an 8 GeV pre-stacker • SNUMI 2: • Use Accumulator, presently used in the antiproton source, to coalesce 3 booster batches at a time, allowing 18 batches to be loaded as 6 boxcar batches into the recycler. • Debuncher ring is not utilized in this scheme, making it available as a slow spill facility for mu2e: inject bunches not used by neutrino program from accumulator into debuncher. • Make one narrow bunch in the Debuncher, then slow extract to Mu2e

  23. 22 cycles = 1467 ms PROTON SOURCE RING USAGE Booster Batches 4.61012 p/batch NEUTRINO PROGRAM MUONS Accumulator (NuMI +Muons) Recycler 56 1012 p/sec (NuMI) Debuncher (Muons) 44.61012 p/1467ms = 12.5 1012 p/sec 0.1s 1.367s 23

  24. TECHNICAL ISSUES • Booster to Accumulator Transfer Line ( also needed for the future neutrino program in the proton plan). • Radiation limits (same as for NuMI program). • Rebunching • Slow Extraction from Debuncher • Debuncher Beam Dump Location • Extinction Factor • Experiment Location 24

  25. The MECO Beam and Detector T5 3 1 B (Tesla) vs. s along beam 10 m x 0.95 m rad     m 0 10 20 30 13 m x 0.25 m rad 4m x 0.75 m rad  

  26. Graded Solenoid Field For adiabatic motion in a straight solenoid with a field gradient, pt12/B1= pt22/B2or sin2sin2 where sin() = pt/p, pt = component of p transverse to B field • When the muon spirals from a low field region, B1, to a high field region, B2 it will be reflected back when sin2(=1, or when sin2(1)=B1/B2. • pt/p decreases as B decreases  particle movement is enhanced in the direction of decreasing gradient. Effect is acceleration of particle in the direction of decreasing field. • Production Solenoid: Following the MELC scheme: apply a graded field at the primary productiontarget to collect and accelerate muons to downstream direction, and reflect a portion of upstream-going muons + pions back to the downstream direction in order to enhance pion/muon collection efficiency: going downstream, B goes from 5 Tto2.5 T. • Detector Solenoid: Use graded field at muon stopping target to reflect upstream-going electrons produced there to the downstream direction toward the detectors, to increase acceptance. Going downstream, B goes from 2T to1T. • Transfer Solenoid, which connects the Production Solenoid to the muon stopping target and Detector Solenoid has a small continuous decline of B moving downstream. (Exception is in curved parts of solenoids).This prevents local trapping of charged particles, which could lead to delayed beam particles reaching the stopping target in the measurement window  700 ns after injection.

  27. Charged particle motion in a toroid Drift Property in the curved (toroid) portion of Transport Solenoid • For a toroid, charged particles spiraling around the B-field lines drift perpendicular to the toroid bend plane. For R= toroid bending radius, s =distance of travel along the particle’s central orbit, ppar=component of p parallel to B, pperp=component of p perpendicular to B, the vertical displacement is: • Unwanted positively charged particles and high-energy negatively charged particles (e.g. E(e-)>100 MeV, p(m-)>75 MeV/c) are displaced vertically after passing curved solenoid portions in the Transport Solenoidand are collimated away.

  28. Production Solenoid • 4 m long x 0.75 radius • 0.30 radius inside radiation/heat shield is available for particle transport • 10-20 x 1012protons/s, bunch spacing ~1.6 s • Protons enter at a 10 degree angle, toward the upstream direction to reduce background particle flux into transport line • Water-cooled platinum or gold target, 0.4 cm radius x 16 cm long • B-field tapers going downstream from 5 T to 2.5 T to reflect upstream-travelling low-E pions and muons back downstream toward the transport solenoid. Particles are accelerated downstream by the gradient. Transport solenoid downstream upstream B=2.5 T B=5 T

  29. Transport Solenoid • Separates detectors from production target:no straight-line path for neutrals • Selects  in momentum range <0.08 GeV/c • Eliminates electrons >100 MeV • Absorbs +, e, p, pbar, pi • Components include: B=2.5 T 13m x 0.25m radius • Vacuum system • Collimators • Thin beryllium Pbar absorbing window • Neutron absorbers • Stopping Target: 17x.02 cm Al disks ~8 cm radius, 5 cm spacing B=2.0 T

  30. Detector Solenoid • 10 m long x 0.95 m radius • Detector solenoid is evacuated to avoid: scattering of background and signal particles; and capture of muons in residual gas downstream of stopping target • B graded from 2 T to 1 T in first 4 m in target region • Al target is in a graded field in order to • reflect portion of upstream-going electrons back toward detector • reduce the transverse momentum of beam electrons with E>100 MeV to have helix radii< 38 cm so that they do not hit the detectors • B=1 T, uniform to 0.2% in tracking region, 1.0 % in calorimeter region to obtain necessary energy resolution • Thin low-Z shields around the target absorb protons from muon capture • Central region r<38 cm of detectors is free of material. Charged particles from target with pt<55 MeV/c pass without interacting to downstream beam dump • Specially enclosed beam dump minimizes particle albedo B=1 T B=2 T

  31. Magnetic Spectrometer for Conversion Electron Momentum Measurement Sample event- this onefirst travels upstream, is reflected by B gradient back toward detector Electron starts upstream, reflects in field gradient Shown: Longitudinal straw option Straws: 2.6 m length  5mm dia., 25 m wall thickness to minimize multiple scattering – 2800 total • tracker will intercept between 2 and 3 helical turns

  32. Cross section of longitudinal tracker Noteof e- from DIO have pt>55 MeV/c • Geometry: Octagon with eight vanes, each ~30 cm wide x 2.6 m long • Straws: 2.6 m length  5mm dia., 25 mm wall thickness to minimize multiple scattering – 2800 total • Three layers per plane, outer two resistive, inner conducting • Pads: 30 cm  5mm wide cathode strips affixed to outer straws - 16640 total pads • Position Resolution: 0.2 mm (r,)  1.5 mm (z) per hit is goal • Energy loss and straggling in the target and multiple scattering in the chambers dominate energy resolution of 1 MeV FWHM pt=105 MeV/c target pt=55 MeV/c pt=91 MeV/c

  33. Alternative: Transverse Tracker • Geometry: 18 Modules of three planes each, 30° rotation between successive planes • Straws: 70 – 130 cm length  5mm diameter, 15 or 25 m thickness • 12960 total straws • One layer per plane, all • straws are conducting • Baseline: no z-coordinate, charge • division was being considered • Position Resolution: 0.2 mm (x,y) • Readout Channels: 13k • L and T tracker performances are • similar in simulations, and more • prototype work is needed to decide • on the best option. 136 cm

  34. Calorimeter • Function: provide initial trigger to system (E>75 MeV gives trigger rate ~1 kHz), and secondary position and energy information to clean up tracks • 1024 PbWO4 crystals, 3.75 x 3.75 x 12 cm3 arranged in four vanes. Density 8.3g/cm3, Rad. Length 0.89 cm, R(moliere)=2.3 cm, decay time 25 ns • Each crystal is equipped with two large area Avalanche Photo-Diodes: gives larger light yield and allows rejection of charged particles traversing photodiode • Both the front end electronics (amplifier/shapers) and the crystals themselves are cooled to -240 C to improve PbWO4 light yield and reduce APD dark current. • Single crystal performance has been demonstrated with cosmic rays: 38 p.e./MeV, electronic noise 0.7 MeV, for electrons, ~5-6 MeV at 100 MeV, position<1.5 cm

  35. Cosmic Ray Veto and Shielding • Passive shielding: heavy concrete plus 0.5 m magnet return steel. Latter also shields CRV scintillator from neutrons coming from stop target. • Hermetic active veto: Three overlapping layers of scintillator consisting of 10 cm x 1 cm x 4.7 m strips • Goal: Inefficiency of active shielding  • Cost-efficient solution: MINOS approach- extruded rather than cast scintillator, read out with 1.4 mm dia. wavelength-shifting fiber. • Use multi-anode PMT readout

  36. Probability Rate (proton flux=1-2x1013 Hz) Events (run time= 2-4x107 seconds, total p’s =4x1020) Prob. Muon stopped in target per proton 0.0025 0.25-0.5x1011 Hz 1x1018 Prob.  capture (Al target) 0.60 1.5-3x1010 Hz 6x1017 Fraction of captures in detector time window 0.45 (> 700 ns ) 0.7-1.4x1010 Hz 3x1017 Track fitting and selection criteria 0.19 1.2-2.5x109 Hz 5x1016 Detected events for Re=10-16 10-16 1.2-2.5x10-7 Hz 5  single-event sensitivity 2x10-17 Estimated background 0.45 Old MECO andnewmu2ebeam rates and sensitivity

  37. Backgrounds (Assumptions: extinction ~ 10-9, energy resolution 1 MeV FWHM, 4x1020 protons)

  38. PRISM=Phase Rotated Intense Slow Muon source, PRIME=PRISM Mu e, FFAG= Fixed-Field Alternating Gradient synchrotron

  39. mu2e PRISM/PRIME Re goal   Proton beam 8 GeV, 10 x1012 Hz, ~1/1.6 MHz bunch rate 50 GeV(JPARC), 100 x1012 Hz, ~10-100 Hz bunch rate (JPARC and FFAG cycle limits) Muon momentum <77 MeV/c 68 MeV/c +- 3%  thin target Muon stop rates .25x1011 Hz, 4 year run ? 1011 to 1012 Hz, 5 year run ? Extinction use internal and external kickers FFAG suppresses pions, etc. to high order Target Al or perhaps Ti, begin data at > 700 ns after injection Ti or higher Z (minimal detector measurement delay) Detector Detector displaced downstream from stopping target in a straight solenoid FWHM<1 MeV Target and detector separated by momentum-selecting toroid and line-of sight shielding FWHM<0.3 MeV Comparison of mu2e and PRISM/PRIME

  40. e exRe for photonic processes (-) Signal: coincidence of back-to-back e and  Large accidental background rate:E(e+) = E() ~ 52.83 MeV, where there is a huge background of positrons from ordinary muon decay, e (+) Low-energy muon flux, (surface beam) Requires state-of-the-art detector Current limit BR(ex MEG (PSI) goal: BR<10-13. Long-term with upgrade, BR<10-14 (+) Funded and under construction Comparison withe e-N eRe for non-photonic processes  Far less background at the signal energy than eand noaccidental coincidences • Requires special muon source • MECO: Re<10-16 • PRISM/PRIME: Re<10-18

  41. A substantial fraction of the MECO Collaboration is interested in a m- e- conversion experiment at Fermilab, if there is a possibility. • A group of Fermilab scientists is also interested, and has been exploring the beam options. • No show stoppers have been identified, and it seems possible there is an attractive solution that would enable a m- e- conversion experiment to run at Fermilab in parallel with the neutrino program. • A meeting was held at Fermilab on Sept 15-16, 2006: about 50 physicists attended. Conclusions at the meeting: • substantial interest from physics community • preliminary look says m- e- is highly adaptable to the presentFNAL accelerator complex • next steps are under discussion- letter of intent, or some other approach??? (we would like to get support for studies of needed transfer lines, extinction, RF issues, extraction studies…) . STATUS 41

  42. Summary • The physics potential of eN is excellent. • The beam line magnet systems for MECO received funding priority, and an advanced design was produced at MIT: a great asset to any future effort • The detector systems and DAQ are at the detailed conceptual stage- no potential show-stoppers are seen. A very good detector is needed, but no new inventions are required. Some initial prototype work has been done for the trackers, calorimeters and cosmic ray veto counters. • Groups were awaiting funding to build prototypes when the project was cancelled- so there is lots of hands-on development work to do. • A lot of detailed simulation work has been done, but more is needed. For example with the detailed magnet design, we can study the cost drivers in detail and perhaps find some savings, or more studies of backgrounds and shielding, L vs. T trackers, etc. • The MECO concept is highly viable as a candidate experimental arrangement, with many man-years of design effort invested, and with many successful detailed reviews. • There is the possibility that the design could be modified to improve performance and/or to reduce cost.

  43. Summary (Continued) • Participation is open, none of the tasks have been parceled out. • There is plenty of interesting development work to do. • You are invited to join in!

  44. Distribution of electron energies from  decay in orbit (DIO) Free muon decay, Ee(max)=52.8 MeV Bound muon decay Aluminum Aluminum 1s state Endpoint energy=104.96 Lifetime=0.88 s • To keep DIO contribution to Re negligible, need detector electronenergy resolution<1 MeV (FWHM) for 100-106 MeV electrons, with minimal high-side tails. • Detector acceptance needs to be high for 100-106 MeV electrons, but to control rates needs to be minimized to avoid copious low energy electrons. • Backgrounds need to be eliminated between 100-106 MeV

  45. Major Background: Decay of a Muon Bound in Atomic Orbit bound ee(DIO) • With nucleus to absorb momentum, neutrinos can carry zero momentum, with electron recoiling off of the nucleusendpoint energysameasa potential conversion electron For Z=13 (Al), Atomic BE=0.529 MeV, Recoil energy=0.208 MeV  Ee(max)=104.96 MeV • Rate near the maximum energy falls very rapidly. Near endpoint: proportional to (Ee(max)-E)5 Mostimportantpotential source of background- Discriminate against it by measuring electron energy to better than ~1 MeV FWHM. • Accept events from 103.6-105.1 MeV 0.05 DIO/(eN) if Re~10-16 Ee(max)=mc2-Recoil-AtomicBE Endpoint E (Al)=104.96 MeV

  46. Cosmic Ray Veto and Shield • Passive shielding: heavy concrete plus 0.5 m magnet return steel • Inefficiency of active + passive shielding  • Three overlapping layers of scintillator

  47. Fermilab proton source for a muon beam line • Adapt existing facility for μ-e conversion experiment • Current intensity • Accumulator to stack protons • Debuncher for beam formation and extraction • Protons for muon source – A-D configuration • extract beam for mu-e conversion • atom captures muon, muon decays to e without neutrinos • MECO- or PRISM/PRIME –like experiment

  48. Muon to electron conversion • Measure rate of the lepton flavor violating (LFV) reaction: neutrinoless muonto electron conversion in the field of a nucleus, relative to the ordinary muon capture rate on a nucleus. • Goal: Re< 10-16 which is ~ 6000x better than the current limit from SINDRUM II: Re<6.1x10-13 Reis the ratio of rates measured in a muonic atom, Re={Rate(-+A(N,Z) e-+A(N,Z)} / {Rate(-+A(N,Z) +A’(N+1,Z-1)} L=+1,Le=0  L=0,Le=+1 • In SM, suppressed far below experimental accessibility. • Experimentally accessible rates are commonly predicted in new physics models excellent process to use in the search for new physics.

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