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The interaction of neutrinos with matter is extremely weak, hence they easily penetrate celestial bodies. Determining the neutrino spectrum and flavor can shed light on their production reaction and environment. They are thus ideal probes for the Earth and Sun. Geoneutrinos are primarily generated by three types of long-lived radioactive isotopes, potassium-40 (
$ ^{\rm{40}} {\rm{K}}$ ), uranium-238 ($ ^{\rm{238}} {\rm{U}}$ ), and thorium-232 ($ ^{\rm{232}} {\rm{Th}}$ ). Their origin, composition, and distribution are highly interesting questions in geoscience. They can aid in the discovery of the physical and chemical structure of the Earth and even reveal its evolution.The KamLAND [1–4] and Borexino [5–7] experiments have made pioneering contributions to the discovery of geoneutrinos. Their detection is achieved by detecting inverse-beta-decay (IBD) signals in liquid-scintillator detectors. An IBD signal consists of a prompt positron signal and a delayed neutron-capture signal, and the prompt-delay-coincidence provides a clear signature of the interaction. The IBD cross-section is relatively high. The energy threshold for the reaction is 1.8 MeV, and only
$ ^{\rm{232}} {\rm{Th}}$ and$ ^{\rm{238}} {\rm{U}}$ geoneutrinos are accessible. Almost no directional information can be extracted for the initial neutrinos [8].Neutrinos originating in the mantle have a direct connection with the power that drives plate tectonics and mantle convection [9, 10]. However, the measurements on mantle geoneutrinos rely heavily on crust geoneutrino predictions. Consequently, the mantle component still has considerable uncertainty. In Ref. [11], Tanaka and Watanabe proposed to use a 6Li-load liquid scintillator to extract directional information on U and Th neutrinos using the IBD process and even image the Earth’s interior.
The K element is more mysterious than U and Th.
$ ^{\rm{40}} {\rm{K}}$ decays contribute roughly to 1/3 of the radiogenic heat of the Earth, however no experimental$ ^{\rm{40}} {\rm{K}}$ neutrino result has been reported to date. Because K is a volatile element, precipitating it into typical mineral phases is more difficult than for U or Th. Measuring the flux of$ ^{\rm{40}} {\rm{K}}$ neutrinos versus$ ^{\rm{238}} {\rm{U}}$ and$ ^{\rm{232}} {\rm{Th}}$ neutrinos can offer input to the understanding the formation process of the Earth [12]. The model of$ ^{\rm{40}} {\rm{K}}$ and$ ^{\rm{40}}{\rm{Ar}} $ in the air and the Earth also indicates the enriched and depleted mantle structure [13]. In [14], Leyton, Dye, and Monroe proposed to use directional neutrino detectors, like noble-gas time-projection chambers, to explore various geoneutrino components.Notably, thus far, the liquid scintillator detector of Borexino is the only one that achieved sub-MeV neutrino spectroscopy, where both large target mass and low background are realized. Solar neutrinos are detected through neutrino-electron scattering,
$ \nu+e^- \rightarrow \nu+e^-, $
(1) which has no theoretical threshold. There is a strong correlation between the initial neutrino and scattered electron direction, especially after imposing a requirement on the kinetic energy of the recoiling electron. In this study, we consider introducing directionality to the conventional liquid scintillator detector to suppress the intrinsic solar neutrino background and detect the
$ ^{\rm{40}} {\rm{K}}$ geoneutrinos.Because of the long emission time constant of scintillation radiation, the new type of liquid-scintillator Cherenkov neutrino detectors [15–17] can identify the small prompt Cherenkov radiation within the large amount of slow scintillation light. This unique feature can provide not only the reconstruction of both direction and energy, which has never been achieved in conventional liquid scintillation neutrino detectors, but also particle identification [18]. We consider two schemes for the liquid-scintillator Cherenkov neutrino detector. The first approach is to use a fast, high-light-yield liquid scintillator and fast photon detectors. In this case, the light yield can reach 10,000 photons per MeV with an emission time constant of a few nanoseconds, which is much longer than several picoseconds of timing precision of the photon detectors. The recent experimental development for this approach can be found in Refs. [19–21]. The second approach is to use a slow liquid scintillator and photomultiplier tubes (PMTs). The PMTs usually have a timing precision of about one nanosecond, while the emission time constant for the slow liquid scintillator is much longer, for example, 20 nanoseconds [22–24].
In this study, we focus on the latter scheme. We adopted the parameter set for pure linear alkylbenzene (LAB) [22] as a slow liquid-scintillator candidate, which is most favorable for the Cherenkov separation. The light yield is 2530 photons/MeV, and the emission rise and decay time constants are 12.2 ns and 35.4 ns, respectively. The time profile is shown in Fig. 1. The Cherenkov threshold is 0.178 MeV, assuming the refractive index of the liquid to be 1.49 [25].
Figure 1. (color online) Normalized time profile of scintillation light emitted by slow liquid scintillator, LAB [22].
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We consider an ideal terrestrial detector, located at the Earth’s equator, rotating along with the Earth. We define the solar z-axis,
$ z_{\odot} $ , from the Sun to the Earth, and an Earth z-axis,$ z_{\oplus} $ , from the center of the Earth to the detector (Fig. 2). Correspondingly, we define the angle between the recoiling electron and$ z_{\odot} $ as$ \theta_{\odot} $ , and the angle with$ z_{\oplus} $ as$ \theta_{\oplus} $ . Geoneutrinos and solar neutrinos are generated, and the kinetic energies of the recoiling electrons are recorded. With a cut on the recoiling electron kinetic energy at 0.7 MeV, the distributions of$ \cos\theta_{\odot} $ and$ \cos\theta_{\oplus} $ for the remaining neutrinos are shown in Fig. 3. The geoneutrinos (crust and mantle) are clearly separated from the solar-neutrino background. Since the energy range of the$ ^{\rm{40}} {\rm{K}}$ neutrinos is distinguishable from those of the$ ^{\rm{232}} {\rm{Th}}$ and$ ^{\rm{238}} {\rm{U}}$ neutrinos, there is a possibility to detect the$ ^{\rm{40}} {\rm{K}}$ component. Next, we consider a real detector. -
We adopted the detector scheme [26] shown in Fig. 4. The slow liquid scintillator, which is contained in a transparent container, is in the center, and it is surrounded by a non-scintillating material, such as water or mineral oil. The PMTs are installed with all photocathodes facing inward, forming a large spherical array. The PMTs are all immersed in the water or oil. The water behind the PMTs also serves as a veto layer, shielding the detector from radioactivities like betas, gammas, neutrons, and cosmic-ray muons. The number of signals is directly proportional to the target mass, and due to the required low-background rate, only the central region of the liquid scintillator, known as the fiducial volume, is accepted for signal detection.
Figure 4. (color online) Detector concept. Inside to outside: slow liquid scintillator (yellow), water (blue), PMT, and water.
The simulations of solar-neutrino generation, geo-neutrino generation, and neutrino-electron scattering are described in Appendix A, Appendix B, and Appendix C, respectively. Recoil electrons are simulated using Geant4 [27–29] including all possible electromagnetic processes. Because of multiple scattering, the initial direction of the electron is smeared out. Some electrons eventually turn back when they are close to stopping.
Both Cherenkov and scintillation light emissions are handled by Geant4; however, the production of scintillation light is customized according to LAB measurement [22].
All optical photons are recorded and undergo empirical simulations [26, 30], as the attenuation length of optical photons still requires more experimental research [22], and the target mass or volume is a parameter we want to test. The limited PMT photocathode coverage and photon attenuation and scattering will cause efficiency loss, hence we assume that practically only 66.7% (2/3) of the photons can reach the PMTs. The quantum efficiency of a PMT is assumed to be 30% for all photons within the range [300, 550] nm and to be zero for the rest, which is motivated by the high quantum efficiency of PMTs, according to Ref. [31]. In summary, the total efficiency for generating photoelectrons, PE, is 20% for photons within the range [300, 550] nm and zero outside of this wavelength range.
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From the simulation, we can determine the average energy scale, i.e., the number of PE per MeV, and thus the total number of detected PEs for each event is scaled to the detected energy. The detected-energy spectra of solar- and geo-neutrinos are shown in Fig. 5 and Fig. 6, respectively.
Figure 5. (color online) Detected kinetic-energy spectra of recoiling electrons produced by solar neutrinos in simulation.
Figure 6. (color online) Detected kinetic-energy spectra of recoiling electrons produced by geoneutrinos in simulation.
We use a weighted-center method to reconstruct the direction of the recoiling electrons,
$ \vec{R} $ . The formula is$ \vec{R} = \frac{1}{N_{\rm{PE}}}\sum\limits_{i = 1}^{N_{\rm{PE}}} \vec{r}_{i}, $
(2) where
$ \vec{r}_{i} $ is the direction of each photoelectron, and$ N_{\rm{PE}} $ is the number of photoelectrons.We attempted three groups of photons. In Case (1), we use all Cherenkov photons to study the best case and understand the scattering of electrons in the liquid scintillator. In Case (2), we apply the 20% efficiency cut, as described in Section 1.2. We use this study to understand the results with Cherenkov photons only. In Case (3), we tested a more realistic case, where the detection efficiency is considered, and the photoelectrons from the first two ns of scintillation radiation are introduced.
The angular response is plotted in Fig. 7 for electrons with kinetic energies in the range of [0.5, 2] MeV, where we show the cosine of the angle between the reconstructed direction and the initial electron direction for all three cases. For case (1), the angular resolution with 99% coverage is 116 degrees, and it is 124 and 125 degrees for the second and third cases, respectively. Comparing Case (1) with (2), which includes the 20% efficiency cut, the latter does not show significant degradation of the reconstructed angular distribution. The dominant factor affecting the performance of directional reconstruction is electron scattering in the liquid scintillator. After further introducing the scintillation photons as the background in Case (3), we find that the angular resolution is slightly worse than for Case (2). In the rest of this paper, we focus on Case (3), which is the more realistic one.
Figure 7. (color online) Angular-response distribution of reconstructed directions relative to electrons’ initial direction, where the electron kinetic energy is in range [0.5, 2] MeV. Upper and lower panels are the same, but the upper panel is plotted on a logarithmic scale to clearly show the non-negligible negative component.
The angular response as a function of energy is shown in Fig. 8 for Case (3). The resolution improves gradually with increasing energy.
Figure 8. (color online) Angular response versus energy. Projection on cos(θ) for [0.5, 2] MeV electrons is shown in Fig. 7.
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To extract the geoneutrino signals, we first determine an energy cut and a
$ \cos\theta_{\odot} $ cut, followed by a statistical subtraction to remove the solar-neutrino background. -
The event rate ratio of geo- to solar neutrinos as a function of energy is shown in Fig. 9, according to which we define three observation windows. One is the energy range [0.7, 2.3] MeV, where all
$ ^{\rm{40}} {\rm{K}}$ ,$ ^{\rm{232}} {\rm{Th}}$ , and$ ^{\rm{238}} {\rm{U}}$ geoneutrinos provide contributions. The second is the range [0.7, 1.1] MeV, which is dominated by$ ^{\rm{40}} {\rm{K}}$ neutrinos, and the third is the range [1.1, 2.3] MeV, which is populated by$ ^{\rm{232}} {\rm{Th}}$ and$ ^{\rm{238}} {\rm{U}}$ neutrinos. For events below 0.7 MeV, like the$ \nu_e $ component from$ ^{\rm{40}} {\rm{K}}$ decay, the directional reconstruction is rather poor, hence these events are not usable. For all three observation windows, the solar-neutrino background needs to be suppressed by a factor of 100-200 to enable us to extract geoneutrino signals. In the [0.7, 1.1] MeV window, the dominant solar-neutrino backgrounds are the$ pep $ ,$ ^{13} {\rm{N}}$ , and$ ^{15} {\rm{O}}$ neutrinos, while the$ ^{15} {\rm{O}}$ and$ ^{8} {\rm{B}}$ neutrinos are in the [1.1, 2.3] MeV window.Figure 9. (color online) Signal-to-background ratio (geo-to-solar-neutrino ratio) as a function of electron kinetic energy.
Followingly, we determine the
$ \cos\theta_{\odot} $ cut. After applying the detected-energy cut of [0.7, 2.3] MeV, the$ \cos\theta_{\odot} $ of the remaining solar- and geo- neutrinos are both plotted in Fig. 10. With a cut at$ \cos\theta_{\odot}<-0.75 $ , the solar neutrinos are suppressed by a factor of 150, and the signal (geo) to background (solar) ratio is about 0.1, closer to unity than the other region. -
Using the data sample from our imagined experiment, the number of geoneutrino signals,
$ N_{\rm geo} $ , can be calculated by subtracting the solar-neutrino background:$ N_{\rm geo} = N_{\rm can}-N_{\rm bkg}\times \epsilon, $
(3) where
$ N_{\rm can} $ is the number of all candidates,$ N_{\rm bkg} $ is the background flux, e.g., the solar neutrinos, and$ \epsilon $ is the detection efficiency, including the energy-window cut and the$ \cos\theta_{\odot} $ cut.The uncertainty
$ \sigma_{\rm geo} $ in the geoneutrino counts is$ \sigma_{\rm geo} = \sqrt{\sigma_{\rm candidate}^2 + N_{\rm solar}^2\sigma_{\epsilon}^2 + \epsilon^2\sigma_{\rm solar}^2}, $
(4) where
$ \sigma_{\rm candidate} $ is the statistical uncertainty of the data sample,$ \sigma_{\rm solar} $ is the solar-neutrino-flux uncertainty, and$ \sigma_{\epsilon} $ is the uncertainty in the efficiency.For the solar-neutrino background, pep and B8 neutrinos are dominant. We expect that several proposed experimental approaches, like Jinping [32], LENA [33], THEIA [17], and [34], will improve their uncertainty to a 1% precision. Calibration sources can be deployed to multiple locations of the detector [35]. The calibration source can be a beta source enclosed in a small metal box with a small pinhole as a collimator. With sufficient statistics, a 1% precision is expected.
From our experience, we assume that the detection-efficiency uncertainty, including the energy and the
$ \cos\theta_{\odot} $ cuts, can also reach 1%.For the
$ ^{\rm{40}} {\rm{K}}$ energy window, we further need to subtract the$ ^{\rm{238}} {\rm{U}}$ and$ ^{\rm{232}} {\rm{Th}}$ geoneutrino components as backgrounds. With the advantage of a low reactor-neutrino background, the Jinping Neutrino Experiment can measure the total flux of these neutrinos to better than 5%. -
From the discussion above and the results obtained for angular resolution and expected systematic uncertainties, we can now estimate the precision of the geoneutrino-flux measurement as a function of exposure. We express the sensitivity as
$ {\rm sensitivity} = N_{\rm geo}/\sigma_{\rm geo}, $
(5) which provides the relative precision or the deviation from the null assumption. The study is performed for each of the three energy windows defined in Section 1.4.1 above: one for all geoneutrinos, [0.7, 2.3] MeV, another for the
$ ^{\rm{40}} {\rm{K}}$ geoneutrinos, [0.7, 1.1] MeV, and the third for the$ ^{\rm{238}} {\rm{U}}$ and$ ^{\rm{232}} {\rm{Th}}$ components, [1.1, 2.3] MeV. The results are shown in Fig. 11, Fig. 12, and Fig. 13, respectively.Figure 13. (color online) Discovery sensitivity for 238U and 232Th genoneutrinos as a function of exposure.
Among these results, the most attractive is the one for the
$ ^{\rm{40}} {\rm{K}}$ geoneutrinos, Fig. 12. With a three-kiloton target mass and 20-year data-acquisition time, a 3-σ observation is possible. With a 20-kiloton detector, a 5-σ observation is expected.For the
$ ^{\rm{232}} {\rm{Th}}$ and$ ^{\rm{238}} {\rm{U}}$ region, even with the better signal-to-background ratio shown in Fig. 9, the result is still limited by low statistics. Hence, the expectation is worse than for the$ ^{\rm{40}} {\rm{K}}$ geoneutrinos. -
We used the Standard Solar Model to provide energy sampling of solar neutrinos. Ref. [45] provides the neutrino-energy spectra of all solar neutrinos. We used the neutrino-flux predictions on Earth with the high-metallicity assumption from Ref. [46] as normalization. The characteristic energies and fluxes are summarized in Table A1, and the neutrino energy spectra are shown in Fig. B1.
${{E} }_{\rm{Max} }$ or${{E} }_{\rm{Line} }$ /MeVFlux/( $\times10^{10}$ ${\rm{s}}^{-1}$ ${\rm{cm}}^{-2}$ )$pp$ 0.42 $5.98(1\pm0.006)$ $^7{\rm{Be}}$ 0.38 $0.053(1\pm0.07)$ 0.86 $0.447(1\pm0.07)$ $pep$ 1.45 $0.0144(1\pm0.012)$ $^{13}{\rm{N}}$ 1.19 $0.0296(1\pm0.14)$ $^{15}{\rm{O}}$ 1.73 $0.0223(1\pm0.15)$ $^{17}{\rm{F}}$ 1.74 $5.52\times10^{-4}(1\pm0.17)$ $^8{\rm{B}}$ 15.8 $5.58\times10^{-4}(1\pm0.14)$ $hep$ 18.5 $8.04\times10^{-7}(1\pm0.30)$ Table A1. Characteristic energies and total fluxes of solar neutrinos.
${E}_{\rm{Max}}$ depicts maximum energy for continuous spectra, and${E}_{\rm{Line}}$ depicts discrete lines.Figure B1. (color online) Predicted non-oscillating solar electron-neutrino energy spectra on Earth, where the unit for continuous spectra is 1010/(cm2 s MeV), and for discrete lines is 1010/(cm2 s).
Solar neutrinos are generated as pure electron neutrinos. Taking into account the oscillation between different neutrino flavors during transit
$\rm{is} $ the Sun [47, 48], the survival probability of electron neutrinos is [49, 50]:$\tag{A1} P^{\odot}_{ee} = \cos^4\theta_{13}\left(\frac{1}{2}+\frac{1}{2}\cos2\theta^M_{12}\cos2\theta_{12}\right), $
where
$ \sin^2\theta_{12} $ = 0.307,$ \sin^2\theta_{13} $ = 0.0241, and$ \theta^M_{12} $ is the revised matter oscillation angle [47–50], which is neutrino energy and electron number density dependent [51].The appearance probability of
$ \nu_{\mu} $ or$ \nu_{\tau} $ is$\tag{A2} P^{\odot}_{e\mu(\tau)} = 1-P^{\odot}_{ee}. $
The probability
$ P^{\odot}_{ee} $ ranges from 0.3 to 0.6. We did not consider neutrino oscillations in the Earth, because the change in probability is less than 5%, which is insignificant for our study. -
There are three dominant heat-producing isotopes in the Earth:
$ ^{\rm{238}} {\rm{U}}$ ,$ ^{\rm{232}} {\rm{Th}}$ , and$ ^{\rm{40}} {\rm{K}}$ . Neutrinos are produced in their decay chains or direct decays:$\tag{B1} \begin{align} ^{238}\rm{U} \rightarrow ^{206}\rm{Pb} + 8\alpha + 6e^- + 6\bar\nu_e + 51.698\; MeV, \end{align} $
$\tag{B2} \begin{align} ^{232}\rm{Th} \rightarrow ^{207}\rm{Pb} + 7\alpha + 4e^- + 4\bar\nu_e + 46.402\; MeV, \end{align} $
$\tag{B3} ^{40}\rm{K} \rightarrow ^{40}\rm{Ca} + e^- + 4\bar\nu_e + 1.311\; MeV\; (89.3\%), $
$\tag{B4} ^{40}\rm{K} + e^- \rightarrow ^{40}\rm{Ar} + \nu_e + 1.505\; MeV\; (10.7\%). $
Electron-antineutrinos are dominant, however 10.7% of the
$ ^{\rm{40}} {\rm{K}}$ decays occur through electron capture, producing electron-neutrinos with an energy of 0.043 MeV. This decay branch is ignored, because it is hard to distinguish using the method proposed in this study. The characteristic energies of these neutrinos are listed in Table B1, and their energy spectra are shown in Fig. B2.Isotope ${E}_{\rm Max}$ /MeVFlux/( $\times10^{10}$ ${\rm{s}}^{-1}$ ${\rm{cm}}^{-2}$ )Crust 40K 1.31 0.00160 232Th 2.26 0.00043 238U 3.27 0.00047 Mantle 40K 1.31 0.00057 232Th 2.26 0.00005 238U 3.27 0.00008 Table B1. Characteristic energies and total fluxes of geoneutrinos. EMax depicts maximum energy for continuous spectra.
Figure B2. (color online) Predicted non-oscillating geo electron-antineutrino energy spectra on the Earth's surface.
We used a layered Earth model to simulate the geoneutrinos. In this model, the Earth is assumed to consist of three layers: the core, mantle, and crust. We assume that the mantle and crustal layers have uniform distributions of
$ ^{40} {\rm{K}}$ ,$ ^{232} {\rm{Th}}$ and$ ^{238} {\rm{U}}$ , and that there is no radioactivity from the core.The entire volume of the Earth is divided into many small cells, each of which has a coordinate
$ \vec{r} $ . Electron antineutrinos are sampled from each cell. The differential flux of electron antineutrinos from each cell to the surface neutrino detector at$ \vec{d} $ can be written as [40, 41]:$\tag{B5} {\rm d}\phi(\vec{r})_{e} = \frac{X \lambda N_A}{\mu} n_{\nu} P_{ee}^\oplus \frac{A(\vec r) \rho(\vec{r})}{4\pi |\vec{r}-\vec{d}|^2}{\rm d}v, $
where X is the natural isotopic mole fraction of each isotope, λ is the corresponding decay constant,
$ N_A $ is the Avogadro's number, µ is the atomic mole mass,$ n_{\nu} $ is the number of neutrinos per decay,$ P_{ee}^\oplus $ is the average survival probability,$ A(\vec r) $ is the abundance of each element in kg/kg,$ \rho(\vec r) $ is the local density at each location, and$ |\vec{r}-\vec{d}| $ provides the distance from each cell$ \vec{r} $ to our detector at$ \vec{d} $ .We take the outer radii of the core, mantle and crust to be 3480, 6321, and 6371 km [52], respectively, with their corresponding densities at 11.3, 5.0, and 3.0 g/cm3. The element abundances of K, Th, and U are set to match the integrated flux predictions, as in Refs. [40, 41], and the values are given in Table B2. This simplified layered model is not as sophisticated as that provided in Ref. [53]; however, it is nevertheless sufficient for our demonstration purposes. The rest of the parameters are taken from Ref. [41]. The total fluxes of the predicted geoneutrinos are summarized in Table B1. The non-oscillating neutrino spectra of
$ ^{40} {\rm{K}}$ ,$ ^{232} {\rm{Th}}$ , and$ ^{238} {\rm{U}}$ at the detection site are shown in Fig. B2.K [kg/kg] Th [kg/kg] U [kg/kg] Crust 1.16 × 10−2 5.25 × 10−6 1.35 × 10−6 Mantle 152 × 10−6 21.9 × 10−9 8.0 × 10−9 Table B2. Element abundance of K, Th and U in the mantle and crust used for this study.
The geoneutrino oscillation probability varies only by about 2% within the energy range [0, 3.5] MeV [40], hence it is treated as a constant, i.e.,
$ P_{ee}^\oplus = 0.553 $ . The appearance probability of the$ \nu_{\mu} $ or$ \nu_{\tau} $ components is$ \tag{B6} P^{\oplus}_{e\mu(\tau)} = 1-P^{\oplus}_{ee}. $
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The differential scattering cross-sections for neutrinos of energy
$ E_{\nu} $ and recoil electrons with kinetic energy$ T_e $ can be written, e.g. in Ref. [54], as:$\tag{C1} \frac{{\rm d}\sigma(E_{\nu},T_e)}{{\rm d}T_e} = \frac{\sigma_0}{m_e}\left[g_1^2+g_2^2\left(1-\frac{T_e}{E_{\nu}}\right)^2-g_1g_2\frac{m_eT_e}{E_{\nu}^2}\right], $
where
$ m_e $ represents the electron mass. For$ \nu_e $ and$ \bar\nu_e $ ,$ g_1 $ and$ g_2 $ are:$ \tag{C2} \begin{split} g_1^{(\nu_e)} =& g_2^{(\bar\nu_e)} = \frac{1}{2}+\sin^2\theta_W\simeq0.73,\\ g_2^{(\nu_e)} =& g_1^{(\bar\nu_e)} = \sin^2\theta_W\simeq0.23, \end{split} $
where
$ \theta_W $ depicts the Weinberg angle, and for$ \nu_{\mu,\tau} $ ,$ g_1 $ and$ g_2 $ are:$ \tag{C3} \begin{split} g_1^{(\nu_{\mu,\tau})} =& g_2^{(\bar\nu_{\mu,\tau})} = -\frac{1}{2}+\sin^2\theta_W\simeq-0.27,\\ g_2^{(\nu_{\mu,\tau})} =& g_1^{(\bar\nu_{\mu,\tau})} = \sin^2\theta_W\simeq0.23. \end{split} $
The constant
$ \sigma_0 $ is$ \tag{C4} \sigma_0 = \frac{2G_F^2m_e^2}{\pi}\simeq88.06\times10^{-46}\ \rm{cm}^2. $
The differential cross-section is shown in Fig. C1. The antineutrino cross-section is lower than that of the neutrinos by several factors, and the recoil electrons produced by
$ \bar\nu_e $ tend to have lower kinetic energies.Figure C1. (color online) Neutrino-electron-scattering differential cross-section for
$ \nu_e, \nu_{\mu,\tau}, \bar\nu_e$ , and$ \bar\nu_{\mu,\tau}$ at neutrino energies 1 and 2 MeV.With the above formulas, the distribution of the recoiling electrons' kinetic energy is calculated:
$\tag{C5} \frac{{\rm d}N}{{\rm d}T} = N_e\int \left [ \sum\limits_{\nu} \frac{{\rm d}\sigma(E_{\nu},T_e)}{{\rm d}T_e} P_{e\nu}\right ] F(E_{\nu}){\rm d}E_{\nu}, $
where
$ \frac{{\rm d}N}{{\rm d}T} $ is the number of scattered electrons N per unit electron kinetic energy T, and$ N_e $ is the number of target electrons. The integral spans all neutrino energies$ E_{\nu} $ , and the sum spans all neutrino flavors$ \nu $ , which are$ \nu_e $ ,$ \nu_{\mu} $ $ \nu_{\tau} $ ,$ \bar\nu_e $ ,$ \bar\nu_{\mu} $ , and$ \bar\nu_{\tau} $ .$ \frac{{\rm d}\sigma(E_{\nu},T_e)}{{\rm d}T_e} $ is given by Eq. (C1),$ P_{e\nu} $ is the oscillation probability, and$ F(E_{\nu}) $ is the flux of neutrinos.With the condition of energy and momentum conservation, the cosine of the scattering angle between the initial neutrino direction and the scattered-electron direction can be determined from:
$ \tag{C6} \cos\theta = \frac{1+m_e/E_{\nu}}{\sqrt{1+2m_e/T_e}}. $
The resulting
$ \cos\theta $ distribution is shown in Fig. C2. Notably, although the directional correlation between the incoming neutrino and the recoil electron is weak at low energies, for example, at 1 MeV, with a cut of the kinetic energy of the recoil electron, the correlation still exists and can be employed. This feature is also shown in Fig. C2.Figure C2. (color online) Cosine distribution of scattering angle between initial neutrino direction and recoiling electron. In this plot, we use 1 MeV
$ \nu_e$ as an example. Shaded area shows result with a cut on the electron kinetic energy at 0.7 MeV.After considering neutrino oscillation and neutrino-electron scattering, the kinetic energy spectrum of recoiling electrons of solar- and geo-neutrinos are shown in Fig. C3, and Fig. C4, respectively.