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 muon to 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  e is 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,L e =0  L  =0,L e =+1 The conversion electron is monochromatic and has an energy which is typically well above most of the background flux.

5. Discovery of  - N  e - N or a similar charged lepton flavor violating (LFV) process will be unambiguous evidence for physics beyond the Standard Model. For non-degenerate neutrino masses, oscillations can occur. Discovery of neutrino oscillations required changing the Standard Model to include massive. Charged LFV processes occur through intermediate states with mixing. Small mass differences and mixing angles  expected rate is well below what is experimentally accessible. Charged LFV processes occur in nearly all scenarios for physics beyond the SM, in many scenarios at a level that Mu2e will detect. Effective mass reach of sensitive searches is enormous: well beyond that accessible with direct searches. What Will Observation of  - N  e - N Teach Us? ed  d  One example of new physics, with leptoquarks  e W

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

7. History of Lepton Flavor Violation Searches 1 10 -2 10 -4 10 -16 10 -6 10 -8 10 -10 10 -14 10 -12 1940 1950 1960 1970 1980 1990 2000 2010 FNAL  e Goal   - N  e - N  +  e +   +  e + e + e - K 0    + e - K +    +  + e - SINDRUMI I MEG Goal(  e  ) 

8. Why   A  e - A ? Some Options to   A  e - A :  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.  e  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    . What could change before next   A  e - A? –MEG (PSI) may see  e  at 10 -13 to 10 -14 –LHC may discover new particles (e.g. supersymmetry).   A  e  A will be needed to help sort things out, e.g. the flavor structure..

9. Why    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  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  Z 2 /n 2 : 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: R nl (r)  r l Z 3/2 for small r. Prob. of overlap between nucleus and muon wavefunction is proportional to r 2l Z 3 which for small r is large only when l=0. Ordinary Muon Capture Rate  -  A(N,Z)    A’(N’,Z’)  a   bn  cp: ~2, ~2, ~0.1 Fundamental process:    p ->   n Proportional to: (# protons)x(nuclear overlap) ~ Z 4. Capture ~ decay rate for Z=12 Muon Conversion Rate  - + A(N,Z)  A(N,Z) + e  Coherent process  proportional to (# nucleons) 2 x(nuclear overlap) ~Z 5  R  e  high Z preferred. But… Nucleus --

11. negligible 95.56 MeV10.08 MeV.0726  s ~0.8-1.5Au(79,~197) 0.16 0.45 Prob decay >700 ns 104.18 MeV 104.97 MeV Conversion Electron Energy 1.36 MeV.328  s 1.7Ti(22,~48) 0.47 MeV.88  s 1.0Al(13,27) Atomic Bind. Energy(1s) Bound lifetime R  e (Z) / R  e (Al) Nucleus  ->e Conversion Rates vs. Z (Rates Normalized to Z=13, Aluminum) Kitano, et al.  PRD 66, 096002 (2002) Plot of R  e (Z)/R  e (Z=13) For various photon couplings Aluminum is nominal choice for MECO

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

13. Classes of background 1.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 E e <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) 2.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 3.Cosmic Rays- Back/Signal proportional to (run time)/(beam intensity)

14. Decay of a Muon Bound in Atomic Orbit 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 same as a potential conversion electron, but fortunately the probability is very low. E e (max)= (m  c 2  NuclearRecoilEnergy  AtomicBindingEnergy) For Z=13 (Al), Atomic BE=0.529 MeV, Recoil energy=0.208 MeV  E e (max)=104.96 MeV (   + N(A,Z)) bound -> N(A,Z) + e  + e +  (DIO) Muon decay in Al 1s bound state, endpoint=104.96 MeV Free muon decay, endpoint =52.8 MeV 104.96 MeV

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

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

17. Sources of Background, continued Radiative muon capture in 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) - (M A’ -M A )c 2 Radiative capture of 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-, E e >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 10 7 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 10 7 Hz. Beam lines at PSI are limited to ~10 7 -10 8 Hz. Implies ~10 9 -10 10 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 intense pulsed muon beam to suppress prompt background Stop large flux of muons in a target in a narrow time bunch (< 100 ns): ~10 11 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 x10 9 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. Pulsed Proton Beam BNL-AGS at reduced energy, 8 GeV, 2  10 13 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  s Match 0.88  s lifetime of muons in atomic Al: fill 2 AGS RF buckets  1.35  s pulse spacing. Put one bunch in FNAL debuncher  1.6  s 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. Proton pulse Prompt background s Detection time

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

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. PROTON SOURCE RING USAGE 23 Booster Batches Accumulator Recycler Debuncher 22 cycles = 1467 ms 4.6  10 12 p/batch 4  4.6  10 12 p/1467ms = 12.5  10 12 p/sec 56  10 12 p/sec 0.1s1.367s NEUTRINO PROGRAMMUONS (NuMI +Muons) (NuMI) (Muons)

24. TECHNICAL ISSUES 24 1.Booster to Accumulator Transfer Line ( also needed for the future neutrino program in the proton plan). 2.Radiation limits (same as for NuMI program). 3.Rebunching 4.Slow Extraction from Debuncher 5.Debuncher Beam Dump Location 6.Extinction Factor 7.Experiment Location

25. The MECO Beam and Detector     4m x 0.75 m rad 13 m x 0.25 m rad 10 m x 0.95 m rad m 0 10 20 30 T531T531 B (Tesla) vs. s along beam

26. Graded Solenoid Field For adiabatic motion in a straight solenoid with a field gradient, p t1 2 /B 1 = p t2 2 /B 2 or sin 2      sin 2     where sin(  ) = p t /p, p t = component of p transverse to B field When the muon spirals from a low field region, B 1, to a high field region, B 2 it will be reflected back when sin 2 (    =1, or when sin 2 (  1 )=B 1 /B 2. p t /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 production target 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, p par =component of p parallel to B, p perp =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(   )>75 MeV/c) are displaced vertically after passing curved solenoid portions in the Transport Solenoid and are collimated away.

28. Production Solenoid B=5 T B=2.5 T 4 m long x 0.75 radius 0.30 radius inside radiation/heat shield is available for particle transport 10-20 x 10 12 protons/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

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: Vacuum system Collimators Thin beryllium Pbar absorbing window Neutron absorbers Stopping Target: 17x.02 cm Al disks ~8 cm radius, 5 cm spacing B=2.5 T B=2.0 T 13m x 0.25m radius

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 B=2 T B=1 T Central region r<38 cm of detectors is free of material. Charged particles from target with p t <55 MeV/c pass without interacting to downstream beam dump Specially enclosed beam dump minimizes particle albedo

31. Magnetic Spectrometer for Conversion Electron Momentum Measurement Sample event- this one first travels upstream, is reflected by B gradient back toward detector tracker will intercept between 2 and 3 helical turns 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

32. Cross section of longitudinal tracker p t =105 MeV/c p t =91 MeV/c p t =55 MeV/c target Note  of e - from DIO have p t >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

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 PbWO 4 crystals, 3.75 x 3.75 x 12 cm 3 arranged in four vanes. Density 8.3g/cm 3, 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 -24 0 C to improve PbWO 4 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. Old MECO and new mu2e beam rates and sensitivity 0.45Estimated background 5  single-event sensitivity 2x10 -17 1.2-2.5x10 -7 Hz10 -16 Detected events for R  e =10 -16 5x10 16 1.2-2.5x10 9 Hz0.19Track fitting and selection criteria 3x10 17 0.7-1.4x10 10 Hz0.45 (> 700 ns ) Fraction of captures in detector time window 6x10 17 1.5-3x10 10 Hz0.60 Prob.  capture (Al target) 1x10 18 0.25-0.5x10 11 Hz0.0025Prob. Muon stopped in target per proton Events (run time= 2-4x10 7 seconds, total p’s =4x10 20 ) Rate (proton flux=1-2x10 13 Hz) Probability

37. Backgrounds (Assumptions: extinction ~ 10 -9, energy resolution 1 MeV FWHM, 4x10 20 protons)

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

39. Comparison of mu2e and PRISM/PRIME Ti or higher Z (minimal detector measurement delay) Al or perhaps Ti, begin data at > 700 ns after injection Target 68 MeV/c +- 3%  thin target <77 MeV/cMuon momentum 50 GeV(JPARC), 100 x10 12 Hz, ~10-100 Hz bunch rate (JPARC and FFAG cycle limits) 8 GeV, 10 x10 12 Hz, ~1/1.6 MHz bunch rate Proton beam     R  e goal Target and detector separated by momentum-selecting toroid and line-of sight shielding FWHM<0.3 MeV Detector displaced downstream from stopping target in a straight solenoid FWHM<1 MeV Detector    FFAG suppresses pions, etc. to high order    use internal and external kickers Extinction 10 11 to 10 12 Hz, 5 year run ?.25x10 11 Hz, 4 year run ?Muon stop rates PRISM/PRIMEmu2e

40. Comparison with    e      e - N    e   R  e for non- photonic processes  Far less background at the signal energy than    e   and no accidental coincidences Requires special muon source MECO: R  e <10 -16 PRISM/PRIME: R  e <10 -18    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

41. STATUS 41 1.A substantial fraction of the MECO Collaboration is interested in a    e  conversion experiment at Fermilab, if there is a possibility. 2.A group of Fermilab scientists is also interested, and has been exploring the beam options. 3.No show stoppers have been identified, and it seems possible there is an attractive solution that would enable a    e  conversion experiment to run at Fermilab in parallel with the neutrino program. 4.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    e  is highly adaptable to the present FNAL 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…).

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) To keep DIO contribution to R  e negligible, need detector electron energy 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 AluminumAluminum Aluminum 1s state Endpoint energy=104.96 Lifetime=0.88  s Free muon decay, E e (max)=52.8 MeV Bound muon decay

46. 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 energy same as a potential conversion electron For Z=13 (Al), Atomic BE=0.529 MeV, Recoil energy=0.208 MeV  E e (max)=104.96 MeV Rate near the maximum energy falls very rapidly. Near endpoint: proportional to (E e (max)-E) 5 Most important potential 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 E e (max)=m  c 2 -Recoil-AtomicBE Endpoint E (Al)=104.96 MeV

48. 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

49. 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

50. Muon to electron conversion Measure rate of the lepton flavor violating (LFV) reaction: neutrinoless muon to 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  e is 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,L e =0  L  =0,L e =+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.

51. negligible 95.56 MeV10.08 MeV.0726  s ~0.8-1.5Au(79,~197) 0.16 0.45 Prob decay >700 ns 104.18 MeV 104.97 MeV Conversion Energy 1.36 MeV.328  s 1.7Ti(22,~48) 0.47 MeV.88  s 1.0Al(13,27) Atomic Bind. Energy(1s) Bound lifetime R  e (Z) / R  e (Al) Nucleus  ->e Conversion Rates vs. Z (Rates Normalized to Z=13, Aluminum) Kitano, et al.  PRD 66, 096002 (2002) Plot of R  e (Z)/R  e (Z=13) For various photon couplings Aluminum is nominal choice for MECO