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In this work, the target process is Majoron emission in orbit (MEIO)
$ \mu \to eJ $ , while the dominant background process is decay in orbit (DIO). The energy spectra of the electrons from these two processes have been calculated by theoretical works [31, 32], which are shown in Fig. 1. The difference between the two energy spectra will be used to seek Majoron events. Utilizing about$ 10^{18} $ muon events taken by COMET Phase-I, the energy spectra of electrons are measured precisely. To improve the sensitivities, the distribution of detector acceptance is of great significance to obtain an accurate spectrum, which will be evaluated in Section III.B.Figure 1. (color online) Spectra of
$ \mu^{-} \to e^{-} \nu_{\mu} \bar{\nu_{e}} $ (red) and$\mu \to $ $ e J$ (blue).To extract the difference between the spectra, likelihood analysis method is used in this work.
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Likelihood analysis is a very important and popular method of data analysis in particle physics. For an observable influenced by a host of involved parameters that include constants of nature in putative or speculative laws of physics as θ, the probability of obtaining a specific collection of measurements x of the observable can be expressed as
$ p(x\mid\theta) $ or$ p(x;\theta) $ . However in the actual experiments, usually we need to estimate parameters θ after obtaining the collection of observations x. In this case we evaluate the expression$ p(x\mid\theta) $ only for the specific x that is observed, and then examine how it varies as θ is changed. By constructing a likelihood function$ {\cal{L}}(\theta) $ , often also denoted as$ {\cal{L}}(x \mid \theta) $ and sometimes$ {\cal{L}}(\theta \mid x) $ :$ {\cal{L}}(\theta) = p(\theta \mid x) = p(x\mid\theta) $ , which is evaluated at the given observed x and considered to be a function of θ, we can statistically describe how well the models with parameters fit the observations. This is referred to as the likelihood method [34].In this work, the energy spectrum of electrons is expected to be the sum of the spectra of MEIO and DIO processes with a ratio r that can be expressed by the formula
$ f(E)_{{\rm excepted}} = f(E)_{{\rm DIO}} + r f(E)_{{\rm MEIO}} $ , where$ f(E)_{{\rm excepted}} $ is the expected spectrum, and$ f(E)_{{\rm DIO}} $ and$ f(E)_{{\rm MEIO}} $ denote the spectra of the DIO and MEIO processes, respectively. By comparing with the measured spectrum$ f(E)_{{\rm measured}} $ using the likelihood method, the ratio r can be determined.Since the COMET experiment is still waiting for data acquisition, simulation results are used in this work to predict the possibility of searching for Majoron.
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For the COMET experiment, the branching fraction of
$ \mu \to eJ $ is determined by$ {\cal{B}}(\mu \to e J) = \frac{N_{J}/(Acc_{J}f_{J})}{N_{{\rm \mu}}}\ , $
(1) where
$ N_J $ is the number of signal events,$ N_{\rm \mu} $ is the total number of decayed orbital muons,$ f_{J} $ is the fraction of$ \mu \to e J $ within the available phase space constrained by the COMET detectors, and$ Acc_{J} $ is the acceptance of the signal events.In the case where Majoron is not observed,
$ N_J $ should be less than the statistical fluctuation of the total number of electrons$ N_{\rm e} $ that could be detected. Assuming$ N_{e} $ follows a normal distribution, we have:$ N_J < 1.645\sigma_{e}\; (90\%{\rm \; C.\; L.}), $
(2) where
$ \sigma_{\rm e} $ denotes the standard deviation of$ N_{e} $ . Considering that all of the detected electrons are from decayed orbital muons regardless of beam background,$ N_{e} $ can be described by:$ N_{e} = N_{\mu}Acc_{\rm dec}f_{\rm dec}, $
(3) where
$ f_{\rm dec} $ is the fraction of electrons within the available phase space constrained by the COMET detectors and$ Acc_{\rm dec} $ is the acceptance of electrons in the signal region. Then$ \sigma_e $ will be:$ \sigma_{e} = \sqrt{N_{\mu}Acc_{\rm dec}f_{\rm dec}}. $
(4) Combining Eqs. (1), (2) and (4), we have:
$ {\cal{B}}(\mu \to e J) < 1.645 \times \sqrt{ \frac{1} {N_{\mu} Acc_{\rm dec} f_{\rm dec}} } \frac{Acc_{\rm dec} f_{\rm dec}} {Acc_{J} f_{J}}\ , $
(5) which is proportional to two terms:
1. Statistics factor: term
$ \sqrt{\dfrac{1}{N_{\mu}Acc_{\rm dec}f_{\rm dec}}} $ is limited by the trigger rate, which results from the beam structure and tolerance of the detector;2. Significance factor: term
$ \dfrac{Acc_{\rm dec}f_{\rm dec}}{Acc_{J}f_{J}} $ is decided by the energy spectra and the bias of detector acceptance.A muonic atom will normally either decay in orbit or be captured by the nucleus
$ \mu^{-} N(A,Z) \to \nu_{\mu} N(A,Z-1) $ . For the$ \mu - e $ conversion experiments, the total number of decayed orbital muons is determined by$ N_{\mu} = \frac{1}{S.E.S._{\mu e}Acc_{\mu e}}\frac{\Gamma_{\rm decay}}{\Gamma_{\rm capture}}\ , $
(6) where
$ S.E.S._{\mu e} $ is the single-event sensitivity of the$ \mu - e $ conversion experiment,$ Acc_{\mu e} $ is the acceptance of$ \mu - e $ conversion events that are electrons with$ 104.971\; {\rm MeV} $ energy,$ \Gamma_{{\rm decay}} $ is the ratio of decayed muons over total orbital muons, and$ \Gamma_{{\rm capture}} $ is the ratio of muons captured by nuclei over total orbital muons. Considering that only electrons will be recorded no matter whether for MEIO or DIO, the acceptance of the two processes are the same, namely$ Acc_{\rm dec} = Acc_{J} = Acc_{e} $ , where$ Acc_{e} $ means the total acceptance of electrons within the signal range, so that the branching fraction can be finally determined by$ \begin{array}{l} {\cal{B}}(\mu \to e J)< 1.645 \times \sqrt{\dfrac{\Gamma_{\rm capture} Acc_{\mu e} S.E.S._{\mu e}}{\Gamma_{\rm decay}}} \frac{1}{S}\ , \\ \qquad \qquad S = \sqrt{\dfrac{Acc_{e} f_{J}^{2}}{f_{\rm dec}}}\ , \end{array} $
(7) where S is a significance factor that can be optimized to the maximum by changing the signal window.
With the upper limit of the signal window fixed at
$ 105\; {\rm MeV} $ , a distribution of S can be obtained by varying the lower limit. Several cases of COMET Phase-I and Phase-II are taken into consideration together with the ideal situation where the acceptance is 100%. It is shown in Fig. 2 that S reaches a maximum when the lower limit is around$ 80\; {\rm MeV} $ in the case of COMET Phase-I.Figure 2. (color online) Distributions of the significance factor when varying the lower limit of the signal window. The blocker is implemented in COMET Phase-II to control the hit rate in the detector, which will be explained in detail in Section IV.B
Therefore, the sensitivity to search for Majoron can be improved significantly by extending the signal window.
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The COherent Muon to Electron Transition (COMET) experiment [30] at the Japan Proton Accelerator Research Complex (J-PARC) in Tokai, Japan, aims to search for the neutrinoless coherent transition of a muon to an electron (
$ \mu - e $ conversion) in the field of a nucleus, with its single event sensitivity of$ 2 \times 10^{-17} $ , which is more than four orders of magnitude improvement over the current upper limit of$ 7 \times 10^{-13} $ at 90% C.L. from the SINDRUM II experiment [35]. -
To control potential backgrounds, the COMET experiment will be better optimized by precisely measuring the muon beam. Therefore, a two-stage approach is adopted [30, 36]. Figure 3 shows the facilities of COMET Phase-I and Phase-II. A solenoid with
$ 90^{\circ} $ bend is used to transport pions, which decay into muons along the beam line. A hollow, cylindrical detector system (CyDet) surrounding the muon stopping target is specially designed and placed at the exit of the solenoid. Both the muon beam and the detector system are different between Phase-I and Phase-II, leading to different acceptance of signals. -
To obtain a credible signal acceptance, a full simulation is completed utilizing the geometry of detectors described in the COMET technical design report (TDR) [30]. A uniform magnetic field is used within the detector region because the real field map is not available in this work. By scanning the energy of electrons from
$ 74\; {\rm MeV} $ to$ 105\; {\rm MeV} $ with a step of$ 25\; {\rm keV} $ , the acceptance distribution of Phase-I is drawn in Fig. 4, which is the foundation of our study of searching for$ \mu \to eJ $ on COMET Phase-I.Figure 4. (color online) Acceptance distributions of COMET Phase-I by full simulation with uniform magnetic fields of 0.9 T (red), 0.95 T (blue) and 1.0 T (black). The strength of the magnetic field is 1.0 T in the official design of COMET Phase-I.
As described in Section III.A, only tracks at least able to reach the inner wall of CyDet will be detected and reconstructed. In this case tracks with low momenta can never be detected if a magnetic field exists, which explains why acceptance goes to zero as the electron energy gets lower. Natually, this is the most simple and efficient way to change the acceptance by changing the strength of the magnetic field in the detector area, which impacts the radius of electron tracks.
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Finally, the expected energy spectrum of electrons can be obtained by convolving the theoretical spectrum shown in Fig. 1 with the acceptance distribution shown in Fig. 4, where the momentum resolution of the detectors has been taken into account by smearing the spectrum using a Gaussian distribution with
$ \sigma = 150\; {\rm keV}/c $ . Analyzed with the likelihood method in the case of 1.0 T using parameters listed in Table 1, the upper limit of the branching fraction is determined to beParameter Description Value $B_{\rm detector}$ The strength of the magnetic field in the detector area 1 T $\sigma_{\rm rec}$ The momentum resolution of reconstructed tracks $150 ~ {\rm keV}/c$ $ S.E.S. $ The single event sensitivity of the COMET experiment $ 3 \times 10^{-15} $ for COMET Phase-I$ Acc_{\mu e} $ The acceptance of $ \mu-e $ conversion eventsAbout 20% $ \Gamma_{{\rm decay}} $ The ratio of decayed muons over total orbital muons 0.39 $ \Gamma_{{\rm capture}} $ The ratio of muons captured by nucleus over total orbital muons 0.61 $E_{\rm signal}$ The energy range of the signal window [74, 105] $ {\rm{MeV}} $ Table 1. Parameters used in the likelihood analysis of COMET Phase-I.
$ {\cal{B}}(\mu \to e J) < 2.3 \times 10^{-5}\ . $
(8) The high event rate of DIO (
$ R_{\rm DIO} $ ) could be a limit to the search for Majoron in the COMET experiment and is a concerned of many interested parties. Approximately estimated by our analysis,$ R_{\rm DIO} $ is given as$ 16.7\; {\rm kHz} $ . Compared with the effective trigger rate dedicated by the COMET DAQ system, which is no greater than 20 kHz [30], it seems to be tolerable for the trigger of COMET Phase-I. However, it has to be mentioned that there is an optimization of the online trigger system performed by COMET Phase-I to reject the tracks of low-energy particles, after which the trigger rate is reduced to about 1.3 kHz. Therefore, some further studies are necessary to achieve a balance between the large quantity of statistics demanded in our research and the low event rate required by COMET Phase-I, which is beyond the scope of this study. -
As mentioned above, the significance factor S reaches a maximum at around
$ 80\; {\rm MeV} $ , so a proposal is made to shift the peak of acceptance distribution to lower energy region by reducing the strength of magnetic field in the detector area. Two more simulations are performed with uniform fields of 0.95 T and 0.9 T and the acceptance distributions are obtained in these two cases, as shown in Fig. 4. Using the new distributions, the upper limits of$ {\cal{B}}(\mu \to e J) $ are calculated at the 90% C.L. and shown in Table 2.Magnetic Field 1 T 0.95 T 0.9 T Upper Limit $ 2.3 \times 10^{-5} $ $ 1.4 \times 10^{-5} $ $ 6.9 \times 10^{-6} $ Event rate of DIO $ 16.7 \; {\rm kHz} $ $ 75.3 \; {\rm kHz} $ $ 394.6 \; {\rm kHz} $ Table 2. Estimated upper limits after reducing the strength of magnetic field of COMET Phase-I.
Although sensitivity benefits from reducing the strength of magnetic field, the increase in
$ R_{\rm DIO} $ is unacceptable for the existing design of COMET Phase-I. -
COMET Phase-II uses an
$ 8\; {\rm GeV} $ proton beam with electric power of$ 56\; {\rm kW} $ from the J-PARC Main Ring. Pions produced in the collision of proton beams on the target are captured by a 5 T magnetic field. Inside a transport solenoid bent by$ 180^{\circ} $ that provides a 3 T magnetic field, the pions decay into muons. The muons are stopped by 17 thin flat aluminum disks (muon stopping targets) while the electrons are detected by a spectrometer inside a 1 T magnetic field composed by$20\; {\rm \mu m}$ thin straw tubes and an electromagnetic calorimeter (EMC) [30, 36]. Figure 5 shows the layout of the solenoid and detectors. -
To study the acceptance distribution of COMET Phase-II, a fast simulation is finished without considering the material effects and the uncertainty of magnetic field so that the tracks of electrons are standard helices. Electrons are generated randomly and isotropically from 17 muon stopping targets. In a curved solenoid, the central axis of this trajectory drifts in the direction perpendicular to the plane of curvature. This drift can be estimated by [30]
$ D = \frac{1}{qB}\left(\frac{s}{R}\right)\frac{p}{2}\left(\cos\theta + \frac{1}{\cos\theta}\right), $
(9) where q is the signed electric charge of the particle, B is the strength of magnetic field along the center-of-beam axis, θ is the pitch angle of the track, and s and R are the path length along the axis direction and the radius of curvature of the curved solenoid, respectively. As is shown in Eq. (9), the drifts of electrons with different energy are different so that a blocker can be placed near the exit of solenoid to eliminate events with low momenta. Finally, the energy distribution of electrons at the exit of the solenoid, multiplied by a roughly estimated detection efficiency, is used to calculate the acceptance distribution.
A blocker is designed at the exit of the solenoid to control the hit rate in the detector, while a large quantity of statistics is demanded in our research to obtain a more precise spectrum of DIO for comparison. An optimization of the blocker is done to balance
$ R_{\rm DIO} $ and sensitivity. Several designs of blocker are used in this work for comparison since the blocker is still being optimized. In the case of a common design in which a flat blocker is assembled, the acceptance distributions obtained by varying the height of the flat blocker from$ 3\; {\rm mm} $ to$ 600\; {\rm mm} $ are shown in Fig. 6. To optimize the performance, the acceptance distributions obtained by varying the height of a circular blocker with a radius of$ 300\; {\rm mm} $ are also used in this study, and are shown in Fig. 7. -
With the parameters listed in Table 3 and
$ R_{\rm DIO} $ estimated approximately to be$ 232.4\; {\rm MHz} $ by our analysis, the upper limit of searching for$ \mu \to eJ $ in COMET Phase-II is estimated using the likelihood method to beParameter Description Value $B_{\rm detector}$ The strength of the magnetic field in the detector area 1 T $\sigma_{\rm rec}$ The momentum resolution of reconstructed tracks $ 150 \; {\rm keV}/c $ $ S.E.S. $ The single event sensitivity of the COMET experiment $ 2.6 \times 10^{-17} $ for COMET Phase-II$ Acc_{\mu e} $ The acceptance of $ \mu-e $ conversion eventsAbout 60% $ \Gamma_{{\rm decay}} $ The ratio of decayed muons over total orbital muons 0.39 $ \Gamma_{{\rm capture}} $ The ratio of muons captured by nucleus over total orbital muons 0.61 $E_{\rm signal}$ The energy range of signal window [35, 105] $ {\rm{MeV}} $ Table 3. Parameters used in the likelihood analysis of COMET Phase-II.
$ {\cal{B}}(\mu \to e J) < 4.6 \times 10^{-9}, $
(10) where material effects are not considered and the blocker is not implemented.
Meanwhile, the analysis results with different designs of blocker are shown in Fig. 8 and Fig. 9. The upper limit becomes a little better after simple optimization with circular blockers. Assuming an ideal step-type acceptance distribution with a maximum of 60%, the relationship between the upper limit and
$ R_{\rm DIO} $ is calculated when varying the lower limit of the signal region, which is used to evaluate the potential of searching for$ \mu \to eJ $ on COMET Phase-II.Figure 8. (color online) Predicted
$ {\cal{B}}(\mu \to e J) $ versus$ R_{\rm DIO} $ in COMET Phase-II with different designs of blocker ($ 0\; {\rm MHz}< $ $ R_{\rm DIO}<140\; {\rm MHz} $ ).Figure 9. (color online) Predicted
$ {\cal{B}}(\mu \to e J) $ versus$ R_{\rm DIO} $ in COMET Phase-II with different designs of blocker ($ 0\; {\rm MHz}< $ $ R_{\rm DIO}<1\; {\rm MHz} $ ).The likelihood analysis shows that
$ {\cal{B}}(\mu \to e J) $ varies between$ O(10^{-8}) $ and$ O(10^{-9}) $ with different designs of blockers. As is implied in Fig. 8, smaller blocker provides higher precision but also leads to higher$ R_{\rm DIO} $ , which requires better detector performance. Given that the data are taken for one year [36] with a duty factor of$ 0.2 $ (beam-on time divided by the accelerator cycle, which is$ 0.5/2.48 \approx 0.2 $ ) [30, 37],$ R_{\rm DIO} $ varies within the range of$ O(10^{2}) $ to$ O(10^{3})\; {\rm MHz} $ if the sensitivity is required to reach$ O(10^{-9}) $ . In this case,$ R_{\rm DIO} $ is too high for the current detector technology. As is implied in Fig. 9, sensitivity of searching for Majoron on COMET Phase-II can reach$ O(10^{-8}) $ even with$ R_{\rm DIO} $ of$ O(10^{2})\; {\rm kHz} $ , which is a much more realistic prediction.
Search for Majoron at the COMET experiment
- Received Date: 2022-07-14
- Available Online: 2023-01-15
Abstract: A new Goldstone particle named Majoron is introduced in order to explain the origin of neutrino mass via some new physics models assuming that neutrinos are Majorana particles. By expanding the signal region and using likelihood analysis, it becomes possible to search for Majoron using experiments originally designed to search for