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The Spectrum of Darkonium in the Sun

Chris Kouvaris kouvaris@cp3.sdu.dk    Kasper Langæble langaeble@cp3.sdu.dk    Niklas Grønlund Nielsen ngnielsen@cp3.sdu.dk CP3-Origins, Centre for Cosmology and Particle Physics Phenomenology University of Southern Denmark, Campusvej 55, 5230 Odense M, Denmark
Abstract

Dark matter that gets captured in the Sun may form positronium-like bound states if it self-interacts via light dark photons. In this case, dark matter can either annihilate to dark photons or recombine in bound states which subsequently also decay to dark photons. The fraction of the dark photons that leave the Sun without decaying to Standard Model particles have a characteristic energy spectrum which is a mixture of the direct annihilation process, the decays of ortho- and para- bound states and the recombination process. The ultimate decay of these dark photons to positron-electron pairs (via kinetic mixing) outside the Sun creates a distinct signal that can either identify or set strict constraints on dark photon models.
Preprint: CP3-Origins-2016-029 DNRF90

I Introduction

Dark matter (DM) is approximately five times more abundant than baryonic matter in the Universe. Although DM can be in the form of more conventional compact objects like primordial black holes Carr:2009jm , there is also the possibility that DM might be in the form of particles. No Standard Model (SM) particle can play the role of DM. Therefore, in the case DM is in the form of particles, it must be related to physics beyond the SM. The simplest example of such a realization is the Weakly Interacting Massive Particle (WIMP) paradigm. In that case, WIMPs are produced in the early Universe and occasionally annihilate to SM particles. If the annihilation cross section is appropriate, annihilations are sufficient to produce the DM abundance we observe today. Such a scenario can potentially be tested. Annihilation of WIMPs in the Sun and the center of the Galaxy to SM particles could create observable signals. Similarly, this scenario allows production of WIMPs in collider experiments as long as there is enough energy to produce them or create nuclear recoils when WIMPs scatter off nuclei in underground detectors.

A minimal extension of the SM that could facilitate the above characteristics can be realized by adding a new U(1)U(1) gauge symmetry which breaks spontaneously providing the dark photon with a mass Kobzarev:1966qya ; Okun:1982xi . In this scenario, the DM particle is charged under the U(1)U(1) symmetry and since it is possible to have a small kinetic mixing between the dark photon and the SM photon under very generic grounds Holdom:1985ag , the dark and bright sectors are linked. As we mentioned above, a particular way of testing this scenario is by searching for signals of DM annihilation in the Sun. DM particles can be trapped in the Sun simply by interacting with nuclei or electrons as they cross it. Trapped DM particles may thermalize with the interior of the Sun and sink to the center where they can meet each other and annihilate to SM particles. In particular, annihilation to neutrinos (which can easily escape from the Sun) may potentially lead to detectable signals in Earth-based detectors. The capture and annihilation process in the Earth and the Sun as well as the produced neutrino spectrum from DM annihilation has been studied extensively in the past Press:1985ug ; Gould:1987ir ; Gould:1987ju ; Silk:1985ax ; Freese:1985qw ; Krauss:1985aaa ; Griest:1986yu . Within the context of dark photons, similar studies have also been made regarding indirect signals from the Sun and the Earth or direct detection Pospelov:2007mp ; Schuster:2009au ; Schuster:2009fc ; Meade:2009mu ; An:2013yfc ; An:2013yua ; Fradette:2014sza ; An:2014twa ; Feng:2015hja ; Feng:2016ijc .

In this paper we investigate fermionic DM that self-interacts via a light dark photon mediator. In particular, we are interested in the region of the parameter space, where DM captured by the Sun has a substantial probability of recombining to positronium-like bound states of DM and anti-DM, which we from now on call darkonium. Darkonium states can subsequently decay to either two dark photons in the case of para-darkonium (where the spin of DM and anti-DM are opposite) or to three dark photons in the case of ortho-darkonium (where the spin of DM and anti-DM are aligned). We assume that dark photons are linked to SM via kinetic mixing with the ordinary photons. At the end of the day, the spectrum of the produced dark photons in the Sun has four components: i) monochromatic dark photons of energy mXm_{X} (the mass of DM) which come from direct DM annihilation ii) monochromatic dark photons of energy mXΔ/2m_{X}-\Delta/2 where Δ\Delta is the binding energy of the para-darkonium iii) dark photons that span energy up to mXΔ/2m_{X}-\Delta/2 from the decay of ortho-darkonium states and iv) monochromatic photons of energy Δ\Delta produced from the recombination of DM to darkonium. We investigate under what conditions the aforementioned dark photons leave the Sun without decaying to SM particles. Those that exit the Sun intact, will decay sooner or later producing an electron-positron pair due to the kinetic mixing. Based on that, we find the precise positron spectrum that potentially could be observed by AMS-02 and we show how one can set constraints on these models. Interestingly, we find that there is parameter space where recombination dark photons could be detected earlier than the annihilation ones.

We should also mention at this point that the possibility of forming darkonium can also have important consequences in the physics of the early Universe. For instance, if DM is thermally produced by a freeze-out of DM annihilation into mediators, the effect of darkonium bound states is to delay the freeze-out until later times vonHarling:2014kha . Additionally, the effect of the bound states in indirect Galactic searches and on the Galactic structure has been investigated in An:2016gad ; Feng:2009mn . The indirect detection signal in models with light dark photons in the center of the Earth and the Sun have been recently investigated in Feng:2015hja ; Feng:2016ijc albeit neglecting DM bound states. As we will show, in the region of the parameter space where darkonium can form, the spectrum of positrons is dominated by the decay pattern of the bound states, and direct annihilation contributes a subleading part in the full signal.

The paper is structured as follows: In section II we review the DM model and the necessary formalism to calculate the solar DM and darkonium populations. In section III we demarcate the allowed parameter space in which darknonium can lead to a significant indirect detection signal. In section IV we review the kinematics and geometry of the positron signal from a decaying mediator emitted from the Sun. In section V we present the positron spectra and compare them with the flux observed by AMS-02. In section VI we make our concluding remarks.

Throughout the paper we use natural units, i.e. =c=kB=1\hbar=c=k_{\text{B}}=1.

II Dark matter in the Sun

We start by introducing a generic DM model that can accommodate the formation of darkonium bound states. The DM model includes a Dirac fermion XX (and its antiparticle X¯\bar{X}) which constitutes the bulk of the DM relic abundance. The DM candidate interacts through a dark U(1)U(1) gauge symmetry. The associated dark photon ϕ\phi interacts with the SM by kinetic mixing with the SM photon. The Lagrangian density of the model reads

=X¯(iγμDμmX)X14ΦμνΦμν+mϕ22ϕμϕμϵ2ΦμνFμν,\mathcal{L}=\bar{X}\left(i\gamma^{\mu}D_{\mu}-m_{X}\right)X-\frac{1}{4}\Phi_{\mu\nu}\Phi^{\mu\nu}+\frac{m_{\phi}^{2}}{2}\phi_{\mu}\phi^{\mu}-\frac{\epsilon}{2}\Phi_{\mu\nu}F^{\mu\nu}, (1)

where mXm_{X} is the DM mass, mϕm_{\phi} the mediator mass, ϵ\epsilon the kinetic mixing parameter and Dμ=μigXϕμD_{\mu}=\partial_{\mu}-ig_{X}\phi_{\mu} is the covariant derivative. FμνF_{\mu\nu} is the electromagnetic field strength tensor and Φμν=μϕννϕμ\Phi_{\mu\nu}=\partial_{\mu}\phi_{\nu}-\partial_{\nu}\phi_{\mu} is the dark U(1)U(1) field strength tensor. We further define α=e2/(4π)\alpha=e^{2}/(4\pi) and αX=gX2/(4π)\alpha_{X}=g_{X}^{2}/(4\pi) as the electromagnetic and dark fine structure constants. The kinetic mixing term can arise through integrating out a heavy particle that is charged under both the dark and electromagnetic gauge groups Holdom:1985ag ; Collie:1998ty , leading naturally to a small ϵ\epsilon. For the purposes of this paper we will treat ϵ\epsilon as a free, yet small, parameter.

The above generic model allows for self-interactions of DM of Yukawa type since the dark photon has a mass (either through a Higgs- or Stueckelberg-mechanism) of the form

V=±αXemϕrr,V=\pm\alpha_{X}\frac{e^{-m_{\phi}r}}{r}, (2)

rr being the distance between two DM particles. The potential is repulsive (++ sign) for XXXX or X¯X¯\bar{X}\bar{X} interactions, while XX¯X\bar{X} interactions are attractive (- sign) and can lead to formation of bound states. In fact DM self-interactions are welcome since they can solve a range of problems arising in the collisionless cold DM paradigm such as the too big to fail problem BoylanKolchin:2011de , the missing satellites problem Klypin:1999uc ; Moore:1999nt ; Kauffmann:1993gv ; Liu:2010tn ; Tollerud:2011wt ; Strigari:2011ps and the core-cusp problem Moore:1994yx ; Flores:1994gz ; Navarro:1996gj . Numerical simulations suggest that generally speaking DM self-interactions alleviate the aforementioned problems within approximately the range of σ/mX\sigma/m_{X} (σ\sigma being the DM-DM cross section) 0.11cm2/g0.1-1\,\text{cm}^{2}/\text{g} Rocha:2012jg ; Peter:2012jh .

The model has four free parameters: ϵ\epsilon, mϕm_{\phi}, mχm_{\chi} and αX\alpha_{X}. In this paper, we assume that the DM relic abundance ΩX0.23\Omega_{X}\simeq 0.23 is produced though the thermal freeze-out of X+X¯ϕ+ϕX+\bar{X}\to\phi+\phi, i.e. the DM density is fixed once the annihilation rate drops below the Hubble expansion rate, Γ(X+X¯ϕ+ϕ)H\Gamma(X+\bar{X}\to\phi+\phi)\lesssim H. We use this criterion to fix the value of αX\alpha_{X} as a function of mXm_{X}. The relation between αX\alpha_{X} and mXm_{X} has been calculated in detail in vonHarling:2014kha including the effects of both Sommerfeld enhancement and darkonium recombination111We note that the recombination cross sections used in vonHarling:2014kha differs from that used in An:2016gad . The coupling αX\alpha_{X} fixed by the DM relic abundance in vonHarling:2014kha differs slightly from the result of direct annihilation with Sommerfeld enhancement, while An:2016gad claims that the effect of recombination on freeze-out is negligible all together. For the purposes of removing αX\alpha_{X} as a free parameter we adopt the coupling found by vonHarling:2014kha ..

The decay rate of the dark photon into SM fermions is given by Feng:2016ijc

Γ(ϕff¯)=ϵ2qf2α(mϕ2+2mf2)3mϕ214mf2mϕ2,\Gamma(\phi\to f\bar{f})=\frac{\epsilon^{2}q_{f}^{2}\alpha(m_{\phi}^{2}+2m_{f}^{2})}{3m_{\phi}^{2}}\sqrt{1-\frac{4m_{f}^{2}}{m_{\phi}^{2}}}, (3)

where qfq_{f} is the electric charge of the fermion (in units of ee) and mfm_{f} is the fermion mass. The decay length into positron electron pairs is

L=Br(ϕe+e)(1.1109ϵ)2(mX/mϕ1000)(100MeVmϕ)R,L=\text{Br}(\phi\to e^{+}e^{-})\left(\frac{1.1\cdot 10^{-9}}{\epsilon}\right)^{2}\left(\frac{m_{X}/m_{\phi}}{1000}\right)\left(\frac{100\text{MeV}}{m_{\phi}}\right)R_{\odot}, (4)

where R=7.0108R_{\odot}=7.0\cdot 10^{8} m is the radius of the Sun, and the branching ratio to electron-positron pairs Br(ϕe+e)1\text{Br}(\phi\to e^{+}e^{-})\simeq 1, if the dark photon cannot decay to heavier particles, e.g. to muons mϕ<2mμ=211m_{\phi}<2m_{\mu}=211 MeV. The branching ratios for heavier dark photons has been calculated in Buschmann:2015awa .

II.1 Solar capture

We now proceed to calculate the number of DM particles captured in the Sun’s gravitational field after scattering on nuclei. We follow the procedure described in Gould:1987ir ; Feng:2016ijc . The capture rate of DM in the Sun for a particular nuclear species NN is given by

CcapN=nX(loc)d3rd3wnN(r)wf(w,r)𝑑ERdσNdER,C_{\text{cap}}^{N}=n_{X}^{\text{(loc)}}\int d^{3}\vec{r}\;d^{3}\vec{w}\;n_{N}(r)wf_{\odot}(w,r)\int dE_{R}\frac{d\sigma_{N}}{dE_{R}}, (5)

where nX(loc)=(ρDM/2)/mX=(0.2n_{X}^{\text{(loc)}}=(\rho_{\text{DM}}/2)/m_{X}=(0.2 GeV/cm)3/mX{}^{3})/m_{X} is the local number density of XX particles, nN(r)n_{N}(r) is the number density of the nuclear species NN as a function of the distance to the center of the Sun, ww is the DM-nucleus relative velocity, f(w,r)f_{\odot}(w,r) is the DM velocity distribution in the rest frame of the Sun, ERE_{R} is the recoil energy and dσN/dERd\sigma_{N}/dE_{R} is the elastic differential scattering cross section of DM on the nucleus NN. By energy conservation ww is related to the DM velocity asymptotically far from the Sun uu by

w2=u2+2GM(r)r.w^{2}=u^{2}+\frac{2GM(r)}{r}. (6)

The velocity distribution in the galactic rest frame is taken to be Baratella:2013fya

f(u)=N[exp(vgal2u2ku02)1]kΘ(vgalu),f(u)=N\left[\exp\left(\frac{v_{\text{gal}}^{2}-u^{2}}{ku_{0}^{2}}\right)-1\right]^{k}\Theta(v_{\text{gal}}-u), (7)

where we set the galactic escape velocity to be vgal=550v_{\text{gal}}=550 km/s and u0=245u_{0}=245 km/s. The parameter kk lies in the interval 1.5k3.51.5\leq k\leq 3.5. The normalization NN is chosen such that d3𝐮f(u)=1\int d^{3}\mathbf{u}f(u)=1. Liouville theorem dictates that f(w,r)=f(u+v)f_{\odot}(w,r)=f(\vec{u}+\vec{v}_{\odot}) (v\vec{v}_{\odot} being the velocity of the Sun with respect to the halo). In the rest frame of the Sun the boosted velocity distribution is

f¯(u)=1211𝑑cf(u2+u2+2uuc).\bar{f}(u)=\frac{1}{2}\int_{-1}^{1}dcf\left(\sqrt{u^{2}+u_{\odot}^{2}+2uu_{\odot}c}\right). (8)

The final capture rate has only a mild dependence on kk. We choose k=2k=2, so we can integrate Eq. 8 analytically:

f¯(u)=N4uu{e(u+u)2u02[4e(u+u)2u02uu4e(u+u)2+vgal22u02(e2uuu021)u02+evgal2u02(e4uuu021)u02]ifuvgalueu2+u2u02[e2uu+vgal2u02u024e(u+u)2+vgal22u02u02+eu2+u2u02(3u02(uu)2+vgal2)]ifvgalu<uvgal+u.\bar{f}(u)=\frac{N}{4uu_{\odot}}\begin{dcases*}e^{-\tfrac{(u+u_{\odot})^{2}}{u_{0}^{2}}}\left[4e^{\tfrac{(u+u_{\odot})^{2}}{u_{0}^{2}}}uu_{\odot}-4e^{\tfrac{(u+u_{\odot})^{2}+v_{\text{gal}}^{2}}{2u_{0}^{2}}}\left(e^{\tfrac{2uu_{\odot}}{u_{0}^{2}}}-1\right)u_{0}^{2}+e^{\tfrac{v_{\text{gal}}^{2}}{u_{0}^{2}}}\left(e^{\tfrac{4uu_{\odot}}{u_{0}^{2}}}-1\right)u_{0}^{2}\right]\\ \hskip 284.52756pt\text{if}\;\;u\leq v_{\text{gal}}-u_{\odot}\\ e^{-\tfrac{u^{2}+u_{\odot}^{2}}{u_{0}^{2}}}\left[e^{\tfrac{2uu_{\odot}+v_{\text{gal}}^{2}}{u_{0}^{2}}}u_{0}^{2}-4e^{\tfrac{(u+u_{\odot})^{2}+v_{\text{gal}}^{2}}{2u_{0}^{2}}}u_{0}^{2}+e^{\tfrac{u^{2}+u_{\odot}^{2}}{u_{0}^{2}}}\left(3u_{0}^{2}-(u-u_{\odot})^{2}+v_{\text{gal}}^{2}\right)\right]\\ \hskip 236.15796pt\text{if}\;\;v_{\text{gal}}-u_{\odot}<u\leq v_{\text{gal}}+u_{\odot}\end{dcases*}. (9)

The differential cross section for a non-relativistic elastic scattering is Feng:2015hja ; Feng:2016ijc

dσNdER=8πϵ2αXαZN2mNw2(2mNER+mϕ2)2|FN|2,\frac{d\sigma_{N}}{dE_{R}}=\frac{8\pi\epsilon^{2}\alpha_{X}\alpha Z_{N}^{2}m_{N}}{w^{2}(2m_{N}E_{R}+m_{\phi}^{2})^{2}}\left|F_{N}\right|^{2}, (10)

where mNm_{N} is the mass of the target nucleus, ZNZ_{N} is the number of protons and the Helm form factor is given by |FN|2=exp(ER/EN)|F_{N}|^{2}=\exp(-E_{R}/E_{N}) with EN=0.114AN5/3GeVE_{N}=0.114\,A_{N}^{-5/3}\,\text{GeV}. The recoil energy must be at least Emin=mXu2/2E_{\text{min}}=m_{X}u^{2}/2 for DM to be captured in the Sun’s gravitational potential in a single scattering. The maximum recoil energy in an elastic scattering is Emax=2μN2w2/mNE_{\text{max}}=2\mu_{N}^{2}w^{2}/m_{N}, where μN=mXmN/(mX+mN)\mu_{N}=m_{X}m_{N}/(m_{X}+m_{N}) is the DM-nucleus reduced mass. With these integration limits the capture rate can be expressed as Feng:2015hja

CcapN=32π3ϵ2αXαnXZN2mNENexp(mϕ22mNEN)ccapN,C_{\text{cap}}^{N}=\frac{32\pi^{3}\epsilon^{2}\alpha_{X}\alpha n_{X}Z_{N}^{2}}{m_{N}E_{N}}\exp\left(\frac{m_{\phi}^{2}}{2m_{N}E_{N}}\right)c_{\text{cap}}^{N}, (11)

where ccapNc_{\text{cap}}^{N} is the integral

ccapN=0R𝑑rr2nN(r)0𝑑uuf¯(u)×Θ(ΔxN)[exNxN+Ei(xN)]xNmaxxNmin,c_{\text{cap}}^{N}=\int_{0}^{R_{\odot}}dr\,r^{2}n_{N}(r)\int_{0}^{\infty}du\,u\bar{f}(u)\times\Theta(\Delta x_{N})\left[\frac{e^{-x_{N}}}{x_{N}}+\text{Ei}(-x_{N})\right]_{x_{N}^{\text{max}}}^{x_{N}^{\text{min}}}, (12)

with xN=(2mNER+mϕ2)/(2mNEN)x_{N}=(2m_{N}E_{R}+m_{\phi}^{2})/(2m_{N}E_{N}) and Ei(z)=z𝑑tt1exp(t)\text{Ei}(z)=-\int_{-z}^{\infty}dt\,t^{-1}\exp(-t). The total capture rate is given by Ccap=NCcapNC_{\text{cap}}=\sum_{N}C_{\text{cap}}^{N}, where the density profiles of relevant nuclei are taken from the solar composition model AGSS09222The solar composition model is publicly available at http://wwwmpa.mpa-garching.mpg.de/~aldos/solar_main.html. Serenelli:2009yc ; Serenelli:2009ww . We make the simplifying approximation that the composition of the Sun has been well-described by this model throughout its lifetime.

II.2 Annihilation of free dark matter

When DM particles interact through a light mediator, and the relative velocity between annihilating DM particles is low, the cross section is significantly enhanced compared to the tree-level annihilation cross section Cassel:2009wt ; Slatyer:2009vg ; Feng:2010zp . This effect is parametrised by the Sommerfeld enhancement factor SS

σannv=Sσannv0\langle\sigma_{\text{ann}}v\rangle=S\;\langle\sigma_{\text{ann}}v\rangle_{0} (13)

where σannσ(X+X¯ϕ+ϕ)\sigma_{\text{ann}}\equiv\sigma(X+\bar{X}\to\phi+\phi) and

σannv0=παX2mX2(1mϕ2/mX2)3/2(1mϕ2/(2mX2))2,\langle\sigma_{\text{ann}}v\rangle_{0}=\frac{\pi\alpha_{X}^{2}}{m_{X}^{2}}\frac{(1-m_{\phi}^{2}/m_{X}^{2})^{3/2}}{(1-m_{\phi}^{2}/(2m_{X}^{2}))^{2}}, (14)

is calculated in the Born regime. The Sommerfeld enhancement factor for the ss-wave process can be found using Hulthén’s potential to approximate the Yukawa potential, yielding

Ss=πasinh(2πac)cosh(2πac)cos(2πca2c2),S_{s}=\frac{\pi}{a}\frac{\sinh(2\pi ac)}{\cosh(2\pi ac)-\cos(2\pi\sqrt{c-a^{2}c^{2}})}, (15)

where a=v/(2αX)a=v/(2\alpha_{X}) and c=6αXmX/(π2mϕ)c=6\alpha_{X}m_{X}/(\pi^{2}m_{\phi}). We take the full Sommerfeld-enhancement factor to be SSsS\approx\langle S_{s}\rangle, where =d3ve12v2/v02/(2πv02)3/2\langle\cdot\rangle=\int d^{3}ve^{-\tfrac{1}{2}v^{2}/v_{0}^{2}}/(2\pi v_{0}^{2})^{3/2} is the thermal average, with v0v_{0} the typical relative velocity. When the annihilating DM particles are non-relativistic, the dark photons will have energy EϕmXE_{\phi}\simeq m_{X}. The distribution of dark photons as a function of energy when DM particles undergo a direct annihilation process is therefore a delta function,

dNϕ(ann)dEϕ=2δ(EϕmX).\frac{dN_{\phi}^{(\text{ann})}}{dE_{\phi}}=2\delta(E_{\phi}-m_{X}). (16)

II.3 Recombination

Darkonium bound states (DD) in this model can form by emission of an on-shell dark photon. At low energies the cross section for forming darkonium may be larger than direct annihilation, i.e. σrec>σann\sigma_{\text{rec}}>\sigma_{\text{ann}} where σrecσ(X+X¯D+ϕ)\sigma_{\text{rec}}\equiv\sigma(X+\bar{X}\to D+\phi). This suggests that recombination can have a big impact on DM freeze-out (as noted in vonHarling:2014kha ) and on indirect detection. If the binding energy of darkonium is less than the mass of the dark photon, the radiated recombination photon must be virtual. The cross section is in this scenario suppressed by a factor ϵ2\epsilon^{2}, and darkonium formation becomes negligible. In the Coulomb limit mϕ0m_{\phi}\to 0, the binding energy of the nnth excited state is Δn=αX2mX/(4n2)\Delta_{n}=\alpha_{X}^{2}m_{X}/(4n^{2}) (henceforth we drop the index on the ground state binding energy, i.e. ΔΔ1\Delta\equiv\Delta_{1}). The recombination cross section to the nnth state has been estimated in BetheSalpeter_QM ; Lifshitz_RelativisticQM . Having a non-zero mediator mass means that there is a highest state which can be populated, nmax=αXmX/(4mϕ)n_{\text{max}}=\alpha_{X}\sqrt{m_{X}/(4m_{\phi})}. Beyond nmaxn_{\text{max}} the binding energy is too low to emit an on-shell dark photon. Although highly excited states decay slowly to dark photons, they can make a transition quickly to lower states, if the difference in binding energy allows for emission of an on-shell dark photon. The highest excited state n~\tilde{n}, where transitions from n~\tilde{n} to n~1\tilde{n}-1 can take place by emission of an on-shell ϕ\phi is n~(αX2mX/(2mϕ))1/3\tilde{n}\approx(\alpha_{X}^{2}m_{X}/(2m_{\phi}))^{1/3} when n~1\tilde{n}\gg 1. Thus the n~(2nmax2)1/3\tilde{n}\approx(2n_{\text{max}}^{2})^{1/3} lowest lying states can quickly cascade to the n=1n=1 state. Since the transition is quick, we will treat all darkonium decays of states below n~\tilde{n} as decays of the ground state. We note that the 2S2S-state can also decay Alonso:2016faw , but we expect that ignoring this introduces only a small error in our estimate. In the case of a non-zero mediator mass, we do not have an analytic expression for the wavefunctions of neither the discrete nor the continuous spectrum. Instead we obtain the recombination cross section by partial wave expansion and solving the Schrödinger equation approximating energy levels and out-going wave functions to be those of the hydrogen atom. We detail in appendix C our numerical procedure for obtaining the recombination cross section. The procedure uses as a first step the same approach as Tulin:2013teo for calculating the scattering cross section.

The authors of An:2016gad recently found that the recombination cross section of the present DM model is much larger than that of direct DM annihilation, when the relative velocity of an XX¯X\bar{X} pair is in the interval 2mϕ/mX<v<2mϕ/mX2m_{\phi}/m_{X}<v<2\sqrt{m_{\phi}/m_{X}}, where vv is the relative velocity of the XX¯X\bar{X} pair. In this region the two are approximately related by333This relation is most correct in the limit where many darkonium states can be populated. If only a few states can be populated by emission of an on-shell dark photon, the relation breaks down.

σrecv6433πln(αX2mXmϕ)σannv.\langle\sigma_{\text{rec}}v\rangle\approx\frac{64}{3\sqrt{3}\pi}\ln\left(\frac{\alpha_{X}}{2}\sqrt{\frac{m_{X}}{m_{\phi}}}\right)\langle\sigma_{\text{ann}}v\rangle. (17)

This cross section accounts for all darkonium states up to nmaxn_{\text{max}}. If the relative velocity v2mϕ/mXv\ll 2m_{\phi}/m_{X} the recombination rate becomes suppressed with respect to the annihilation rate. We emphasise that the indirect detection signal from recombination photons can dominate over the annihilation signal in particular energy bins, even if σrec<σann\sigma_{\text{rec}}<\sigma_{\text{ann}}. This is related to the fact that the positron spectrum comes in flat box-shapes, as we will discuss in detail in section IV. The width of the box spectrum is determined by the mediator energy. In the case of recombination, the mediator energy is the ground state binding energy Δ\Delta, whereas in direct annihilation is mXm_{X}. The box from direct annihilation spans over a much larger energy range than recombination photons. Thus even if σrec<σann\sigma_{\text{rec}}<\sigma_{\text{ann}}, recombination photons although fewer than annihilation ones, span over a much smaller energy range and therefore can dominate the low energy bins.

Neglecting hyperfine splitting, ground state (1S1S) darkonium can be in the spin zero singlet state para-darkonium (pp), or the spin one triplet state ortho-darkonium (oo). At leading order the pp-darkonium state decays back-to-back (in the rest frame) into two dark photons. The photons from the pp-darkonium state are thus distributed in energy as

dNϕ(p)dEϕ=2δ(EmXΔ/2).\frac{dN_{\phi}^{(p)}}{dE_{\phi}}=2\delta(E-m_{X}-\Delta/2). (18)

The oo-darkonium state on the other hand decays at leading order into three dark photons. As a consequence the spectrum of dark photons is more complicated. The photon spectrum is similar to that from decaying ortho-positronium which was calculated for the first time in 1949 by Ore and Powell Ore:1949te . According to the Ore-Powell spectrum, the most likely decay (in the rest frame) is into two nearly back-to-back photons along with a single soft photon. In An:2016gad and An:2015pva An et al. calculated the distribution of bound state decays into three dark photons taking the mass of the dark photon into account. They found the following formula

dNϕ(o)dEϕ=94(π29)y2y(83y)+(y1)y2(y26y+16)log(1y)mXΔ/2mϕ3mϕ2/(4mX2Δ),\frac{dN_{\phi}^{(o)}}{dE_{\phi}}=\frac{9}{4(\pi^{2}-9)y^{2}}\frac{y(8-3y)+\frac{(y-1)}{y-2}(y^{2}-6y+16)\log(1-y)}{m_{X}-\Delta/2-m_{\phi}-3m_{\phi}^{2}/(4m_{X}-2\Delta)}, (19)

where y=Eϕ/(mXΔ/2)y=E_{\phi}/(m_{X}-\Delta/2) is the dark photon energy in units of the darkonium mass, which runs from ymin=mϕ/(mXΔ/2)y_{\text{min}}=m_{\phi}/(m_{X}-\Delta/2) to ymax=13mϕ2/(16mX8Δ)2y_{\text{max}}=1-3m_{\phi}^{2}/(16m_{X}-8\Delta)^{2}.

Dark photons emitted in the recombination process will have energy equal to the binding energy of darkonium. Again we neglect the kinetic energy of the recombining DM. Every time a pair of XX¯X\bar{X} recombines we obtain one recombination photon. We approximate the distribution in energy to be a delta function centered at the ground state energy

dNϕ(rec)dEϕδ(EϕΔ).\frac{dN_{\phi}^{(\text{rec})}}{dE_{\phi}}\simeq\delta(E_{\phi}-\Delta). (20)

This approximation is best in the limit, where only few states can be populated by emission of an on-shell dark photon.

II.4 Boltzmann equations

Here we combine the rates described in the previous subsection to calculate the DM population in the Sun. We assume that DM particles thermalize in a time scale much shorter than the other time scales we are going to consider. A posteriori this approximation is justified in the parameter space we are interested in. DM in the Sun can be either free or bound in darkonium states. The abundances of each component are described by a system of Boltzmann equations given by

dNXdt\displaystyle\frac{dN_{X}}{dt} =Ccap(Cann+Crec)NX2,\displaystyle=C_{\text{cap}}-(C_{\text{ann}}+C_{\text{rec}})N_{X}^{2}, (21a)
dNodt\displaystyle\frac{dN_{o}}{dt} =34CrecNX2CoNo,\displaystyle=\frac{3}{4}C_{\text{rec}}N_{X}^{2}-C_{\text{o}}N_{o}, (21b)
dNpdt\displaystyle\frac{dN_{p}}{dt} =14CrecNX2CpNp.\displaystyle=\frac{1}{4}C_{\text{rec}}N_{X}^{2}-C_{\text{p}}N_{p}. (21c)

Here NXN_{X} is the number of free DM particles XX. We omit the equation for anti-DM, since DM is symmetric and NX=NX¯N_{X}=N_{\bar{X}} at all times. The number of darkonium in oo- and pp-states are given by No/pN_{\text{o/p}}, CcapC_{\text{cap}} is the rate at which the Sun captures XX-particles from the DM halo (not counting anti-DM) as described in section II.1, and Co/pC_{o/p} are the decay rates of the oo- and pp-states, which are given by Stroscio:1975fa

Co\displaystyle C_{o} =2(π29)9παX6mX0.06αX6mX,\displaystyle=\frac{2(\pi^{2}-9)}{9\pi}\alpha_{X}^{6}m_{X}\simeq 0.06\alpha_{X}^{6}m_{X},
Cp\displaystyle C_{p} =αX52mX.\displaystyle=\frac{\alpha_{X}^{5}}{2}m_{X}. (22)

We consider DM heavier than \sim 4 GeV and therefore particle evaporation is negligible Gaisser:1986ha ; Griest:1986yu . The rates of annihilation and recombination are obtained by integrating over the DM number density inside the Sun, i.e. Cann=NX2d3𝐱nX2(r)σannvC_{\text{ann}}=N_{X}^{-2}\int d^{3}\mathbf{x}\;n_{X}^{2}(r)\langle\sigma_{\text{ann}}v\rangle and similar for CrecC_{\text{rec}}. The distribution of DM inside the Sun is given by

nX(r)=n0exp(r2rth2),n_{X}(r)=n_{0}\exp\left(-\frac{r^{2}}{r_{\text{th}}^{2}}\right), (23)

where n0n_{0} is the central number density of XX-particles and rthr_{\text{th}} is the thermal radius, which by the virial theorem is

rth=3T2πGρmX.r_{\text{th}}=\sqrt{\frac{3T_{\odot}}{2\pi G\rho_{\odot}m_{X}}}. (24)

T1.55107T_{\odot}\approx 1.55\cdot 10^{7} K and ρ151\rho_{\odot}\approx 151 g/cm3 are the temperature and density in the center of the Sun, respectively. Taking NX=d3𝐱nX(r)N_{X}=\int d^{3}\mathbf{x}\;n_{X}(r) the annihilation and recombination rates become

Cann\displaystyle C_{\text{ann}} =σannv(2π)3/2rth3,\displaystyle=\frac{\langle\sigma_{\text{ann}}v\rangle}{(2\pi)^{3/2}r_{\text{th}}^{3}},
Crec\displaystyle C_{\text{rec}} =σrecv(2π)3/2rth3.\displaystyle=\frac{\langle\sigma_{\text{rec}}v\rangle}{(2\pi)^{3/2}r_{\text{th}}^{3}}. (25)

The factors 1/4 and 3/4 in equations 21b and 21c denote the different multiplicities of the ortho- and para- states i.e. the ortho-darkonium has three spin states, while the para only one. In Eqs. 21a - 21c we have neglected a number of subdominal effects: ionization of darkonium, populating higher excited darkonium states and DM self-capture. In appendix A we verify that these effects can be neglected for the parameter space we investigate. The Boltzmann equations Eqs. 21a - 21c admit the analytical solutions

NX(t)\displaystyle N_{X}(t) =CcapCann+CrectanhtτX,\displaystyle=\sqrt{\frac{C_{\text{cap}}}{C_{\text{ann}}+C_{\text{rec}}}}\tanh\frac{t}{\tau_{X}}, (26a)
Ni(t)\displaystyle N_{i}(t) =eCit2Ci(2+CiτX){2e(Ci+2τX)tCi2qiτX2F12(1,2+CiτX2,4+CiτX2,e2tτX)+\displaystyle=\frac{e^{-C_{i}t}}{2C_{i}(2+C_{i}\tau_{X})}\left\{2e^{\left(C_{i}+\tfrac{2}{\tau_{X}}\right)t}C_{i}^{2}q_{i}\tau_{X}^{2}{}_{2}F_{1}\left(1,\tfrac{2+C_{i}\tau_{X}}{2},\tfrac{4+C_{i}\tau_{X}}{2},-e^{\tfrac{2t}{\tau_{X}}}\right)+\right.
qi(2+CiτX)[2(eCitCiτX1)+Ci2τX2(ψ0(2+CiτX4)ψ0(CiτX4))\displaystyle\qquad q_{i}(2+C_{i}\tau_{X})\left[2\left(e^{C_{i}t}-C_{i}\tau_{X}-1\right)+C_{i}^{2}\tau_{X}^{2}\left(\psi_{0}(\tfrac{2+C_{i}\tau_{X}}{4})-\psi_{0}(\tfrac{C_{i}\tau_{X}}{4})\right)\right.-
2CiτXeCit(F12(1,CiτX2,2+CiτX2,e2tτX)+tanhtτX)]},\displaystyle\qquad\left.\left.2C_{i}\tau_{X}e^{C_{i}t}\left({}_{2}F_{1}\left(1,\tfrac{C_{i}\tau_{X}}{2},\tfrac{2+C_{i}\tau_{X}}{2},-e^{\tfrac{2t}{\tau_{X}}}\right)+\tanh\frac{t}{\tau_{X}}\right)\right]\right\}, (26b)

where Ni(Ci)N_{i}\;(C_{i}) refer to either No(Co)N_{o}\;(C_{o}) or Np(Cp)N_{p}\;(C_{p}), the qiq_{i}s are given by qo=3CrecCcap/(4(Crec+Cann))q_{o}=3C_{\text{rec}}C_{\text{cap}}/(4(C_{\text{rec}}+C_{\text{ann}})) and qp=qo/3q_{p}=q_{o}/3, ψ0(x)=Γ(x)/Γ(x)\psi_{0}(x)=\Gamma^{\prime}(x)/\Gamma(x) is the digamma function and Fmn{}_{n}F_{m} are the hypergeometric functions. The characteristic time τX\tau_{X} before NXN_{X} reaches the steady state is given by

τX=1Ccap(Cann+Crec),\tau_{X}=\frac{1}{\sqrt{C_{\text{cap}}(C_{\text{ann}}+C_{\text{rec}})}}, (27)

whereas the characteristic steady state time scale for darkonium is

τo/p=max{τX,1Co/p}.\tau_{o/p}=\max\left\{\tau_{X},\;\frac{1}{C_{o/p}}\right\}. (28)
Refer to caption
Refer to caption
Figure 1: This figure shows the solar population of free DM (blue) and darkonium (red) as a function of time illustrating the relevant time scales involved. We have arbitrarily normalised NXss=1N_{X}^{\text{ss}}=1 (dashed blue line) and Niss=1/10N_{i}^{\text{ss}}=1/10 (dashed red line). In the left figure we have chosen Co/p1=τX/10C_{o/p}^{-1}=\tau_{X}/10, and in the right figure we set Co/p1=100τXC_{o/p}^{-1}=100\,\tau_{X}. The figures reflect the fact that the time scale for steady state for the darkonium population is given by Eq. 28.

For all the parameters we will consider 1/Co/pτX1/C_{o/p}\ll\tau_{X} and therefore τo/p=τX\tau_{o/p}=\tau_{X}. Once the DM has reached the steady state, the populations are

NXss\displaystyle N_{X}^{\text{ss}} =CcapCann+Crec,\displaystyle=\sqrt{\frac{C_{\text{cap}}}{C_{\text{ann}}+C_{\text{rec}}}},
No/pss\displaystyle N_{o/p}^{\text{ss}} =qo/pCo/p.\displaystyle=\frac{q_{o/p}}{C_{o/p}}. (29)

The free DM and darkonium populations in the Sun described by Eqs. 26a and 26b are shown in Fig. 1. The behaviour of the darkonium build-up has two qualitatively different behaviours depending on whether τX\tau_{X} is smaller or larger than Co/p1C_{o/p}^{-1}. We require darkonium to have reached the steady state population within the lifetime of the Sun, such that the dark photon emission is not suppressed by a too slow build-up of DM, i.e. we require τo/p<τ4.6\tau_{o/p}<\tau_{\odot}\approx 4.6 Gyr. Since the inequality τX>Co/p1\tau_{X}>C_{o/p}^{-1} is true for all parameters we will consider, it will suffice to find the region where τX<τ\tau_{X}<\tau_{\odot}.

III Parameter space

In this section we map the allowed and interesting region of the parameter space. The parameter space allowed by observations, which simultaneously permits bound state formation, is quite complex. It is beyond the scope of this paper to make a detailed analysis and scan over all possible parameter sets. Instead we list the most important constraints within the interesting region of darkonium formation. The available regions in parameter space is demarcated by the requirements listed below. Bullets 1-5 are regions of interest (not constraints), while bullets 6-8 contain observational constraints.

  1. 1.

    Bound state formation: Darkonium bound states can in principle exist if 1/mϕ1/m_{\phi} is longer than the Bohr length, a0=2/(αXmX)a_{0}=2/(\alpha_{X}m_{X}). However, a stronger requirement arises by demanding the darknonium to be able to form in the first place by emission of an on-shell dark photon. This condition can be written as mϕ<Δ=αX2mX/4m_{\phi}<\Delta=\alpha_{X}^{2}m_{X}/4.

  2. 2.

    Electron-positron decay: We require that the dark photon can decay into an electron-positron pair, i.e. mϕ>2mem_{\phi}>2m_{e}. Within the model we consider, this inequality is always fulfilled if the observational constraints 6-8 are obeyed. We would also like the branching into electron-positrons to be close to one, and therefore keep mϕ<2mμm_{\phi}<2m_{\mu}.

  3. 3.

    Scattering unitarity: To keep our model self-consistent we need to impose unitarity of DM self-scattering. This limits the coupling from above to be αX0.54\alpha_{X}\lesssim 0.54. Correspondingly, by assuming a thermal relic DM abundance limits the DM mass below mX139m_{X}\lesssim 139 TeV vonHarling:2014kha .

  4. 4.

    Efficient recombination: It is useful to note the Coulombic regime where the mediator mass is smaller than the transferred momentum mϕ<μvm_{\phi}<\mu v but larger than the kinetic energy of the scattering, mϕ>μv2/2m_{\phi}>\mu v^{2}/2. If the lower limit is respected it is a good approximation to use Coulombic energy levels An:2016gad . The region can be written as 2mϕ/mX<v<2mX/mϕ2m_{\phi}/m_{X}<v<2\sqrt{m_{X}/m_{\phi}}. Within this range the recombination cross section is much larger than the direct annihilation cross section and approximately given by the analytic expression of Eq. 17. In the Sun the velocity of a thermalized DM particle is

    vth=2TmX5.1×105TeVmX.v_{\text{th}}=\sqrt{\frac{2T_{\odot}}{m_{X}}}\approx 5.1\times 10^{-5}\sqrt{\frac{\text{TeV}}{m_{X}}}. (30)

    Taking the relative velocity of colliding DM particles to be v=2vthv=\sqrt{2}v_{\text{th}}, the lower limit translates to the following inequality on the mediator mass

    mϕ<vthmX2=36MeVmXTeV.m_{\phi}<\frac{v_{\text{th}}m_{X}}{\sqrt{2}}=36\text{MeV}\sqrt{\frac{m_{X}}{\text{TeV}}}. (31)

    We stress that satisfying this inequality only ensures that the analytic expression in Eq. 17 is well described when nmax1n_{\text{max}}\gg 1. For somewhat heavier mediators the recombination rate may still be larger than the direct annihilation rate, although Eq. 17 breaks down. As already discussed, even if the recombination rate is far smaller, the indirect signal from recombination photons may be important nonetheless.

  5. 5.

    Solar steady state: For the solar signal to be maximal, the Sun’s age must be longer than the time it takes to reach the darkonium steady state population, i.e. τo/p<τ4.6\tau_{o/p}<\tau_{\odot}\approx 4.6 Gyr, where τo/p=τX\tau_{o/p}=\tau_{X} for the parameters we will consider, and is thus given by Eq. 27.

  6. 6.

    Self-interaction constraints: NN-body simulations suggests that DM self-interactions may flatten the core of dwarf spheroidal galaxies, alleviating tension with observations. Self-interactions stronger than roughly 0.110cm2/g0.1-10\text{cm}^{2}/\text{g} will however reduce the central densities too much. Furthermore, at higher velocity dispersions, the ellipticity of the Milky Way is threatened if the cross section is stronger than roughly 0.11cm2/g0.1-1\text{cm}^{2}/\text{g} Tulin:2013teo . The scattering cross section when mXv/αX1m_{X}v/\alpha_{X}\gg 1 is well described by the classical momentum transfer cross sections defined by 𝑑Ω(1cosθ)𝑑σ/𝑑Ω\int d\Omega(1-\cos\theta)d\sigma/d\Omega Khrapak1 ; Khrapak:2014xqa

    σatt={4πmϕ2β2log(1+β1)β1018πmϕ2β2(1+1.5β1.65)1101β103πmϕ2(1+logβ12logβ)2β103,\sigma_{\text{att}}=\begin{dcases}\tfrac{4\pi}{m_{\phi}^{2}}\beta^{2}\log\left(1+\beta^{-1}\right)&\beta\lesssim 10^{-1}\\ \tfrac{8\pi}{m_{\phi}^{2}}\beta^{2}\left(1+1.5\beta^{1.65}\right)^{-1}&10^{-1}\lesssim\beta\lesssim 10^{3}\\ \tfrac{\pi}{m_{\phi}^{2}}\left(1+\log\beta-\tfrac{1}{2\log\beta}\right)^{2}&\beta\gtrsim 10^{3}\end{dcases}, (32)

    in the case of attractive interactions and

    σrep={2πmϕ2β2log(1+β1)β1πmϕ2(log2βloglog2β)2β1,\sigma_{\text{rep}}=\begin{dcases}\tfrac{2\pi}{m_{\phi}^{2}}\beta^{2}\log\left(1+\beta^{-1}\right)&\beta\lesssim 1\\ \tfrac{\pi}{m_{\phi}^{2}}\left(\log 2\beta-\log\log 2\beta\right)^{2}&\beta\gtrsim 1\end{dcases}, (33)

    for repulsive ones, where β=2αXmϕ/(vmX)\beta=2\alpha_{X}m_{\phi}/(vm_{X}). The typical vv for dwarf galaxies is of the order of v010v_{0}\sim 10 km/s, while galactic velocity dispersions are significantly larger at the order of v0200v_{0}\sim 200 km/s in the case of the Milky Way. Since symmetric DM with a vector mediator interacts attractively between XX¯X\bar{X} pairs and repulsively between XXXX or X¯X¯\bar{X}\bar{X}, the total cross section per mass is σ/mX=σatt+σrep/(2mX)\langle\sigma\rangle/m_{X}=\langle\sigma_{\text{att}}+\sigma_{\text{rep}}\rangle/(2m_{X}). Here =d3ve12v2/v02/(2πv02)3/2\langle\cdot\rangle=\int d^{3}ve^{-\tfrac{1}{2}v^{2}/v_{0}^{2}}/(2\pi v_{0}^{2})^{3/2} is the velocity average. The DM self-interactions are mapped in Fig. 2.

    Refer to caption
    Figure 2: This figure shows the mϕm_{\phi} vs mXm_{X} parameter space. The dark coupling αX\alpha_{X} is fixed such that ΩX0.23\Omega_{X}\simeq 0.23. The blue shaded contours map DM self-interactions. From darkest to lightest blue the regions are σ/mX>0.1\langle\sigma\rangle/m_{X}>0.1, 11 and 1010 cm/2{}^{2}/g, with σ\langle\sigma\rangle evaluated at dwarf galaxy velocity dispersion v010v_{0}\sim 10 km/s. The red dotted (dashed) contours correspond to σ/mX=1\langle\sigma\rangle/m_{X}=1 cm/2{}^{2}/g (σ/mX=0.1\langle\sigma\rangle/m_{X}=0.1 cm/2{}^{2}/g) at Milky Way velocity dispersion v0200v_{0}\sim 200 km/s. To the left of the black dashed line bound states cannot exist. To the left of the black solid line, bound states cannot recombine by emission of an on-shell dark photon. The green crosses correspond to our benchmark values.
  7. 7.

    Direct detection: Direct detection places an upper bound on ϵ\epsilon for a particular choice of mXm_{X} and mϕm_{\phi}. Currently the strongest limits are placed by the LUX-experiment’s 2013 results Akerib:2013tjd . Following the procedure of DelNobile:2015uua , we find the exclusion contours at 90% confidence level in the ϵ\epsilon versus mϕm_{\phi} parameter space summarized in Fig. 3. For heavy mediator masses, ϵ\epsilon is less constrained. Notice, that the bounds become roughly constant when mϕ<q2μNvm_{\phi}<q\approx\sqrt{2}\mu_{N}v_{\odot}, where qq is the typical value of the transferred momentum in a nuclear recoil, with μN\mu_{N} the reduced DM-nucleus mass and vv_{\odot} the Sun’s velocity in the galactic frame.

  8. 8.

    Cosmology: If the dark photon is abundant in the early universe and decays into SM particles, predictions of the Big Bang nucleosynthesis (BBN) may be adversely affected. To avoid this possibility we can demand that the mediator decays before BBN begins, i.e. the decay rate of the dark photon is Γϕαemmϕϵ2/3>1s1\Gamma_{\phi}\approx\alpha_{\text{em}}m_{\phi}\epsilon^{2}/3>1\,\text{s}^{-1}.

    For non-thermal DM the cosmic microwave background (CMB) constrains the dark matter coupling αX<0.17(mX/TeV)1.61\alpha_{X}<0.17(m_{X}/\text{TeV})^{1.61} from the imprints annihilation products would leave in the CMB. This upper limit is a fit of the results in Slatyer:2015jla obtained by Feng:2016ijc . The couplings we consider are always smaller than this upper limit.

Refer to caption
Refer to caption
Refer to caption
Figure 3: Constraints on ϵ\epsilon as a function of mϕm_{\phi}. The gray contours are excluded by the LUX 2013 data at 90% confidence level. The blue contours signify the region where the DM population in the Sun has not reached its steady state yet. Below the red line, the mediator decay time is longer than one second and could potentially be at odds with big bang nucleosynthesis. The vertical green lines show the binding energy of the ground state, when mϕ>Δm_{\phi}>\Delta the recombination rate is suppressed by ϵ2\epsilon^{2}.

To illustrate the behaviour of the signal, we choose three dark matter masses as benchmark points. For each benchmark the mediator mass is varied in the region compatible with efficient bound state formation in the Sun. The benchmark points are chosen to be:

  1. (B1)

    For our first benchmark we choose the (nearly) lightest DM mass where recombination can take place with DM self-interaction within the range solving the collisionless DM problems (see Fig. 2): mX=400m_{X}=400 GeV and αX=1.1102\alpha_{X}=1.1\cdot 10^{-2}. The mediator mass is chosen to be mϕ=10m_{\phi}=10 MeV, slightly below the binding energy of the ground state which is Δ12\Delta\approx 12 MeV. The smallest kinetic mixing parameter for which the mediator decay is faster than one second is ϵmin1.61010\epsilon_{\text{min}}\approx 1.6\cdot 10^{-10}, while the maximum allowed by direct detection is ϵmax3.31010\epsilon_{\text{max}}\approx 3.3\cdot 10^{-10}.

  2. (B2)

    Our second benchmark point corresponds to the point where the energy threshold of AMS-02 (0.5\sim 0.5 GeV) is close to the maximum positron energy from a decaying recombination photon. This corresponds to mX=2m_{X}=2 TeV and αX=4102\alpha_{X}=4\cdot 10^{-2}, for which the ground state binding energy is Δ=0.8\Delta=0.8 GeV. We choose three values of the mediator mass: (a) mϕ=5m_{\phi}=5 MeV, (b) mϕ=15m_{\phi}=15 MeV and (c) mϕ=70m_{\phi}=70 MeV.

  3. (B3)

    For the last benchmark point we choose the heaviest DM particle allowed by unitarity of scattering. We adopt the value reported in vonHarling:2014kha which is mX=139m_{X}=139 TeV and αX=0.54\alpha_{X}=0.54. Again we choose three values of the mediator mass: (a) mϕ=2m_{\phi}=2 MeV, (b) mϕ=20m_{\phi}=20 MeV and (c) mϕ=100m_{\phi}=100 MeV. The value of nmaxn_{\text{max}} is very large for this benchmark. However, Eq. 17 is well satisfied within the range of the chosen parameters of this benchmark and therefore we use it for the recombination cross section in this case.

In table 2 of appendix B we summarize key quantities for each benchmark.

IV Kinematics of mediator decay

In this section we review the formalism necessary to extract the positron spectrum from DM annihilating in the Sun. It is well known that the received gamma-ray flux emerging from the decay of a monochromatic (single energy) particle to two photons has a characteristic box-like spectrum (see e.g. Ibarra:2012dw ), i.e the gamma-ray flux is independent of energy. Alternatively, if the mediator is a Dirac fermion with chiral interactions, the spectrum form a triangle/trapezoid Ibarra:2016fco . In our scenario dark photons are produced through either direct annihilation of DM particles or via recombination and subsequent darkonium decay. An addittional population is produced because a dark photon is emitted each time a recombination takes place inside the Sun. Dark photons created through direct annihilations, pp-darkonium state decays and recombination are monochromatic, whereas dark photons originating from oo-darkonium state decays are distributed according to Eq. 19. Decays of monochromatic dark photons to positron-electron pairs produce a box-like spectrum similar to the one of the gamma-rays.

In principle, the energy of recombination photons depends on the excitation of the formed bound state. As already discussed, we make the simplifying approximation that all recombination photons have the ground state energy. As a further simplification, we neglect all dark photons, which may be emitted in transitions between darkonium states. For light mediators (<2mμ<2m_{\mu}) the branching into electrons is almost 100%. The signal is for the most part heavily boosted, and therefore clearly directed towards the Sun. For highly energetic positrons, the bending in the magnetic field of the Sun will be small. Since the lightest DM particle we consider has a mass of 400400 GeV, the typical energy of positrons will be quite large. The positrons resulting from decays of recombination photons will in general be less energetic and thus experience a stronger effect. For simplicity we neglect all effects from the solar magnetic field.

Refer to caption
Figure 4: Geometry of mediator decay. Dark photons are emitted from the Sun, and decay to positron electron pairs after distance rr. Positrons reach the Earth with an angle θd\theta_{\text{d}} with respect to the center of the Sun.

We now want to extract the flux of positrons in a solid angle directed towards the Sun. When the mediator is more boosted than the positrons there exists a maximum detector angle θdmax\theta_{\text{d}}^{\text{max}}, beyond which no positrons reach the Earth; see figure 4 for definitions of lengths and angles. The flux is described by the integral

ϕ+=0θdmax𝑑θdsinθddN+dAdtdcosθddEd,\phi_{+}=-\int_{0}^{\theta_{\text{d}}^{\text{max}}}d\theta_{\text{d}}\sin\theta_{\text{d}}\frac{dN_{+}}{dAdtd\cos\theta_{\text{d}}dE_{\text{d}}}, (34)

where θdmax=θl(Ed)\theta_{\text{d}}^{\text{max}}=\theta_{\text{l}}(E_{\text{d}}) is the maximal detector angle for a specific detector energy EdE_{\text{d}} (it is easy to understand why θdmax=θl\theta_{\text{d}}^{\text{max}}=\theta_{\text{l}} since two angles in a triangle sum to less than π\pi, i.e. πθl+θd<π\pi-\theta_{\text{l}}+\theta_{\text{d}}<\pi). When comparing the flux with AMS-02 we smear out the signal in the regions where the maximum angle is smaller than experimental resolution, i.e. θdmax<θAMS(Ed)\theta_{\text{d}}^{\text{max}}<\theta_{\text{AMS}}(E_{\text{d}}), where θAMS(Ed)=(5.8)2/(Ed/GeV)+(0.23)2\theta_{\text{AMS}}(E_{\text{d}})=\sqrt{(5.8^{\circ})^{2}/(E_{\text{d}}/\text{GeV})+(0.23^{\circ})^{2}} is the angular resolution of AMS-02 Gallucci:2015fma . In order to determine the integrand in Eq. 34 we estimate the flux of positrons with energy EdE_{\text{d}} arriving at a detector close to the Earth integrating over the volume 2πR2dcosθddR2\pi R^{2}d\cos\theta_{\text{d}}dR

dN+dAdtdEd=0𝑑R0𝑑EϕdNϕdVdtdEϕ12πR2dΓdcosθl(2πR2dcosθd)δ(EdE+)Θ(rR),\frac{dN_{+}}{dAdtdE_{\text{d}}}=\int_{0}^{\infty}dR\int_{0}^{\infty}dE_{\phi}\frac{dN_{\phi}}{dVdtdE_{\phi}}\frac{1}{2\pi R^{2}}\frac{d\Gamma}{d\cos\theta_{\text{l}}}(2\pi R^{2}d\cos\theta_{\text{d}})\delta(E_{\text{d}}-E_{+})\Theta(r-R_{\odot}), (35)

where E+E_{+} is the positron energy, dΓ/dcosθld\Gamma/d\cos\theta_{\text{l}} is the fraction of positrons emitted at a particular angle, such that it reaches the detector with energy E+E_{+}. Rearranging Eq. 35 gives the integrand of Eq. 34 444We note that our formula disagrees with Eq. 21 of Ajello:2011dq .

dN+dAdtdcosθddEd=0𝑑R0𝑑EϕdNϕdVdtdEϕdΓdcosθlδ(EdE+)Θ(rR).\frac{dN_{+}}{dAdtd\cos\theta_{\text{d}}dE_{\text{d}}}=\int_{0}^{\infty}dR\int_{0}^{\infty}dE_{\phi}\frac{dN_{\phi}}{dVdtdE_{\phi}}\frac{d\Gamma}{d\cos\theta_{\text{l}}}\delta(E_{\text{d}}-E_{+})\Theta(r-R_{\odot}). (36)

The last term is a Heaviside function that excludes positrons created inside the Sun. The first term in the integrand is the number of mediator decays per time, volume and energy EϕE_{\phi} at a distance rr from the center of the Sun. It can be written as

dNϕdVdtdEϕ=er/LLΓϕ(Eϕ)4πr2,\frac{dN_{\phi}}{dVdtdE_{\phi}}=\frac{e^{-r/L}}{L}\frac{\Gamma_{\phi}(E_{\phi})}{4\pi r^{2}}, (37)

where LL is the decay length of ϕ\phi in Eq. 4 and Γϕ(Eϕ)\Gamma_{\phi}(E_{\phi}) is the rate of emitted mediators per energy EϕE_{\phi}. The form of Γϕ\Gamma_{\phi} changes depending on the specific DM model. If only direct annihilation is taken into account the rate is just Γϕ(Eϕ)=Ccap2δ(EϕmX)\Gamma_{\phi}(E_{\phi})=C_{\text{cap}}2\delta(E_{\phi}-m_{X}). In our case Γϕ\Gamma_{\phi} is significantly more involved

Γϕ(Eϕ)=Ccap(kodNϕ(o)dEϕ+kpdNϕ(p)dEϕ+kanndNϕ(ann)dEϕ+(ko+kp)dNϕ(rec)dEϕ),\Gamma_{\phi}(E_{\phi})=C_{\text{cap}}\left(k_{o}\frac{dN_{\phi}^{(o)}}{dE_{\phi}}+k_{p}\frac{dN_{\phi}^{(p)}}{dE_{\phi}}+k_{\text{ann}}\frac{dN_{\phi}^{(\text{ann})}}{dE_{\phi}}+(k_{o}+k_{p})\frac{dN_{\phi}^{(\text{rec})}}{dE_{\phi}}\right), (38)

where kik_{i} is the fraction of DM particles that are converted to photons through either direct annihilation or decay of the oo- and pp-darkonium states. By inspection of the Boltzmann equations Eqs. 21a-21c and using the steady state values of Eq. 29, we get ko=3kp=3Crec/(4(Crec+Cann))k_{o}=3k_{p}=3C_{\text{rec}}/(4(C_{\text{rec}}+C_{\text{ann}})) and kann=Cann/(Crec+Cann)k_{\text{ann}}=C_{\text{ann}}/(C_{\text{rec}}+C_{\text{ann}}). dNϕ(i)/dEϕdN_{\phi}^{(i)}/dE_{\phi} are given by Eqs. 16, 18, 19 and 20. The factor 1/4πr21/4\pi r^{2} in Eq. 37 assumes that the mediators are radiated isotropically from the Sun. Eq. 36 can be simplified significantly by noting that ϕ\phi decays isotropically in its center of mass (cm) frame, and that the energy of a positron in the lab frame is only a function of the decay angle in the cm frame θcm\theta_{\text{cm}}

E+=γϕmϕ2(1+v+vϕcosθcm).E_{+}=\frac{\gamma_{\phi}m_{\phi}}{2}(1+v_{+}v_{\phi}\cos\theta_{\text{cm}}). (39)

Here vϕ=(1mϕ2/mX2)1/2v_{\phi}=(1-m_{\phi}^{2}/m_{X}^{2})^{1/2}, v+=(14me2/mϕ2)1/2v_{+}=(1-4m_{e}^{2}/m_{\phi}^{2})^{1/2} and γϕ=(1vϕ2)1/2\gamma_{\phi}=(1-v_{\phi}^{2})^{-1/2}. Each angle θcm\theta_{\text{cm}} corresponds to a particular angle in the lab frame

cosθl=γϕ(cosθcm+α)γϕ2(cosθcm+α)2+sin2θcm,\cos\theta_{\text{l}}=\frac{\gamma_{\phi}\left(\cos\theta_{\mathrm{cm}}+\alpha\right)}{\sqrt{\gamma_{\phi}^{2}\left(\cos\theta_{\mathrm{cm}}+\alpha\right)^{2}+\sin^{2}\theta_{\mathrm{cm}}}}\,, (40)

where α=vϕ/v+\alpha=v_{\phi}/v_{+}. Combining Eq. 39 and 40 we can write θl(E+)\theta_{l}(E_{+}). When α1\alpha\geq 1, there is a maximum angle θlmaxπ/2\theta_{\text{l}}^{\text{max}}\leq\pi/2, such that for each θl<θlmax\theta_{\text{l}}<\theta_{\text{l}}^{\text{max}} there are two corresponding angles in the center of mass frame and thus two positron energies. We note, that the width of the positron energy spectrum in the lab frame is given by ΔE+=γϕmϕv+vϕ\Delta E_{+}=\gamma_{\phi}m_{\phi}v_{+}v_{\phi}. We can now rewrite the last terms of the integrand by applying the chain rule and the identity δ[f(x)]=δ(xx0)/|f(x0)|\delta[f(x)]=\delta(x-x_{0})/|f^{\prime}(x_{0})|

dΓdcosθlδ(EdE+)\displaystyle\frac{d\Gamma}{d\cos\theta_{\text{l}}}\delta(E_{\text{d}}-E_{+}) =dΓdcosθcm|dcosθcmdcosθl|δ(EdE+)\displaystyle=\frac{d\Gamma}{d\cos\theta_{\text{cm}}}\left|\frac{d\cos\theta_{\text{cm}}}{d\cos\theta_{\text{l}}}\right|\delta(E_{\text{d}}-E_{+})
=dΓdcosθcm|dE+dcosθcmdcosθldR|1δ(RR0)\displaystyle=\frac{d\Gamma}{d\cos\theta_{\text{cm}}}\left|\frac{dE_{+}}{d\cos\theta_{\text{cm}}}\frac{d\cos\theta_{\text{l}}}{dR}\right|^{-1}\delta(R-R_{0})
=1γϕmϕv+vϕr3sin2θdD2δ(RR0),\displaystyle=-\frac{1}{\gamma_{\phi}m_{\phi}v_{+}v_{\phi}}\frac{r^{3}}{\sin^{2}\theta_{\text{d}}D_{\odot}^{2}}\delta(R-R_{0}), (41)

where the absolute value in the first line ensures that a positive number of particles are emitted in the interval dcosθld\cos\theta_{\text{l}}, D=1D_{\odot}=1 a.u. =1.501011=1.50\cdot 10^{11} m is the distance to the Sun, dΓ/dcosθcm=1/2d\Gamma/d\cos\theta_{\text{cm}}=-1/2 from isotropy and dE+/dcosθcm=γϕmϕv+vϕ/2dE_{+}/d\cos\theta_{\text{cm}}=\gamma_{\phi}m_{\phi}v_{+}v_{\phi}/2. In the last line we use dcosθl/dR=sin2θdD2/r3d\cos\theta_{\text{l}}/dR=-\sin^{2}\theta_{\text{d}}D_{\odot}^{2}/r^{3} which follows from the geometric identity

cosθl=DcosθdRr,\cos\theta_{\text{l}}=\frac{D_{\odot}\cos\theta_{\text{d}}-R}{r}, (42)

with r2=R2+D22RDcosθdr^{2}=R^{2}+D_{\odot}^{2}-2RD_{\odot}\cos\theta_{\text{d}}. When evaluating the RR-integral in Eq. 36 it is useful to know R0R_{0} in Eq. 41 which for a particular detector energy (or equivalently a particular θl\theta_{\text{l}}) can be found from Eq. 42

R0=(cosθdsinθdcotθl)D.R_{0}=\left(\cos\theta_{\text{d}}-\sin\theta_{\text{d}}\cot\theta_{\text{l}}\right)D_{\odot}. (43)

For a fixed detector angle, the distance rr is only a function of RR. For evaluating the angular integral it is also useful to note the quantity r0=r(R0)r_{0}=r(R_{0}) which is

r0=sinθdcscθlD.r_{0}=\sin\theta_{\text{d}}\csc\theta_{\text{l}}D_{\odot}. (44)

After trivially integrating over RR (by using the delta function) Eq. 36 can be written as

dN+dAdtdcosθddEd=0𝑑EϕΓϕ(Eϕ)cscθl4πEϕv+vϕDLcscθdesinθdcscθlD/LΘ(sinθdcscθlDR),\frac{dN_{+}}{dAdtd\cos\theta_{\text{d}}dE_{\text{d}}}=-\int_{0}^{\infty}dE_{\phi}\frac{\Gamma_{\phi}(E_{\phi})\csc\theta_{\text{l}}}{4\pi E_{\phi}v_{+}v_{\phi}D_{\odot}L}\,\csc\theta_{\text{d}}e^{-\sin\theta_{\text{d}}\csc\theta_{\text{l}}D_{\odot}/L}\Theta(\sin\theta_{\text{d}}\csc\theta_{\text{l}}D_{\odot}-R_{\odot}), (45)

where Eϕ=γϕmϕE_{\phi}=\gamma_{\phi}m_{\phi} is the energy of the mediator and Γϕ(Eϕ)\Gamma_{\phi}(E_{\phi}) is the rate Eq. 38 . In the case where α>1\alpha>1, θdmax=θl(Ed)<θAMS(Ed)1\theta_{\text{d}}^{\text{max}}=\theta_{\text{l}}(E_{\text{d}})<\theta_{\text{AMS}}(E_{\text{d}})\ll 1, ϕ+\phi_{+} becomes approximately

ϕ+=0𝑑EϕΓϕ(Eϕ)4πEϕv+vϕD2(eR/LeD/L),\phi_{+}=\int_{0}^{\infty}dE_{\phi}\frac{\Gamma_{\phi}(E_{\phi})}{4\pi E_{\phi}v_{+}v_{\phi}D_{\odot}^{2}}\,\left(e^{-R_{\odot}/L}-e^{-D_{\odot}/L}\right)\,, (46)

where the last term is the fraction of dark photons with energy EϕE_{\phi}, which decays between the surface of the Sun and the Earth. The three processes; annihilation, recombination and para-decay contribute to Γϕ(Eϕ)\Gamma_{\phi}(E_{\phi}) in the form of delta-functions. In these cases, when Eq. 46 is valid, the signal is independent on EdE_{d}. Hence, when the mediator is more boosted than the electron-positron pair it decays into, the corresponding spectrum is approximately a box. However, for α<1\alpha<1, cosθl\cos\theta_{\text{l}} takes values in its full range, and for energies EdE_{\text{d}} where θl(Ed)>θAMS(Ed)\theta_{\text{l}}(E_{\text{d}})>\theta_{\text{AMS}}(E_{\text{d}}), the signal is spread over more than one angular bin of AMS. In this case, we should also subtract positrons emitted behind the Sun. The width of the spectrum is given by ΔE+=γϕmϕv+vϕ\Delta E_{+}=\gamma_{\phi}m_{\phi}v_{+}v_{\phi}. The height of the signal scales linearly with the capture rate, and inversely with the width of the spectrum. Furthermore, Eq. 46 shows the dependence on the decay length LL. For LRL\ll R_{\odot} all the decays happen within the Sun, whereas for LDL\gg D_{\odot} all decays occur past the Earth. From Eq. 4 and 11, we get that Lϵ2L\propto\epsilon^{-2}, Ccapϵ2C_{\text{cap}}\propto\epsilon^{2}, and conclude that for each pair γϕ,mϕ\gamma_{\phi},m_{\phi} there is an optimum value of ϵ\epsilon that maximizes the detected positron flux. When combining the positron spectrum from mediators emitted in different processes, the signal will not scale uniformly with ϵ\epsilon.

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Figure 5: Sketch of the combined positron spectrum. The thick, gray curve depicts the total signal, whereas the colored curves are the contributions from annihilation, recombination and decays of pp- and oo-bound states.

Since Γϕ(Ed)\Gamma_{\phi}(E_{\text{d}}) has four contributions, where three are proportional to delta-functions and the last is proportional to the Ore-Powell spectrum, the final flux will be a sum of three boxes of unequal height and width, along with a fourth contribution which depends on EdE_{\text{d}}. From the width of each box, we get information about the energy carried by the dark photon. Particularly, the dark matter mass, mXm_{X}, and the binding energy, Δ\Delta. The height and shape of the signal will, in turn, determine the kinetic mixing, ϵ\epsilon, and the mediator mass, mϕm_{\phi}. In Fig. 5, we show a sketch of the combined positron spectrum with color-coded composition.

V Results

In this section we present the spectra of positrons from DM annihilating in the Sun using the formalism of the previous section. The main results of the paper are contained in Fig. 6. This figure shows the positron flux from the Sun as a function of energy for our benchmark parameters. In Fig. 6 we have superimposed the 1σ1\sigma uncertainty contours of the isotropic positron flux measured by AMS-02. Since AMS-02 measures an isotropic positron flux and the DM signal is anisotropic and directed towards the Sun, the signal must be smaller than the uncertainty on the isotropic flux measurement. We indeed find that this uncertainty is exceeded by the DM signal from the Sun in some cases. We will however refrain from placing new constraints on the parameter space, since we lack data on the positron flux in the angular bins directed towards the Sun. Specifically, to place new constraints on the model’s parameter space we need the measured solar positron flux ϕ\phi_{\odot} and the associated statistical error δϕ\delta\phi_{\odot}. We would then require the anisotropic DM signal ϕDM\phi_{\text{DM}} to be lower than the difference in the solar and isotropic fluxes, i.e. ϕDM<ϕϕiso+δϕiso+δϕ\phi_{\text{DM}}<\phi_{\odot}-\phi_{\text{iso}}+\delta\phi_{\text{iso}}+\delta\phi_{\odot}, where ϕiso\phi_{\text{iso}} and δϕiso\delta\phi_{\text{iso}} are the isotropic positron flux and the associated error. To be conservative, we add the statistical errors on the isotropic and solar fluxes.

In Fig. 6 we see that for all benchmarks the spectra are dominated by the signal from the recombination photons and the Ore-Powell (ortho-decay) photons. The dependence of the spectrum on ϵ\epsilon is subtle. On the one hand large values of ϵ\epsilon increase the capture rate and potentially the positron signal. On the other hand large ϵ\epsilon values decrease the decay length. For high energetic dark photons e.g. from direct annihilation, the decay length is sufficiently large so the overall effect of increasing ϵ\epsilon corresponds to an increase in the overall positron spectrum. On the contrary for not so energetic dark photons like those of recombination, the decay length might not be so large to make it out of the Sun, thus increasing the value of ϵ\epsilon reduces the positron flux. This is depicted e.g. in B1. As we shall see this is not a universal feature i.e. other benchmark points have larger positron fluxes for larger values of ϵ\epsilon even in the recombination part of the spectrum.

In panel B1, the recombination signal lies at much lower energies than those probed by AMS-02. The recombination photons have relatively small boost factors, hence the signal is not entirely box-shaped. The right side of the recombination box signal is from positrons emitted forward in the lab frame with a small angle θl(Ed)<θAMS(Ed)\theta_{\text{l}}(E_{\text{d}})<\theta_{\text{AMS}}(E_{\text{d}}), such that AMS would detect the full signal within one angular bin. When going to the left side of the box-like signal, the angle θl(Ed)\theta_{\text{l}}(E_{\text{d}}) increases and part of the signal exceeds θAMS(Ed)\theta_{\text{AMS}}(E_{\text{d}}) leading to a lower detected flux, thus smearing the left side of the box. For θl(Ed)>π/2\theta_{\text{l}}(E_{\text{d}})>\pi/2, the positrons are emitted at distances R>DR>D_{\odot} and a significant part of the signal is obstructed by the Sun. The low boost factor of the recombination photon makes the signal decrease with increasing ϵ\epsilon because the decays occur predominantly inside the Sun. Contrary to this, the signal from the highly boosted Ore-Powell photons increase with increasing ϵ\epsilon. The gray dashed curves indicate the flux for ϵ\epsilon between ϵmin\epsilon_{\text{min}} and ϵmax\epsilon_{\text{max}}. We note that the full range of allowed values for ϵ\epsilon gives rise to a spectrum which exceeds the error on the isotropic signal from AMS-02 in the high energy end of the data. For B2a, mϕΔm_{\phi}\ll\Delta such that the recombination photons are highly boosted, and the whole spectrum is elevated when ϵ\epsilon is increased. Again in this case, the high energetic part of the spectrum is above the AMS error. The recombination signal is now within the energy range of AMS, but more than an order of magnitude below the error. By increasing the mediator mass, the width of the recombination signal broadens, since v+1v_{+}\to 1, and ϵmax\epsilon_{\text{max}} is increased. For B2b, the high energetic Ore-Powell photons are still above the AMS error. When increasing the mediator mass further, we reach a point where the recombination signal resembles the one in B1, and similarly decreases with ϵ\epsilon. For B2c, the recombination signal is only visible in the lower end of the allowed range of ϵ\epsilon. Likewise, the lower end of the Ore-Powell spectrum is no longer increasing with ϵ\epsilon. In spite of this, the upper part of the spectrum rises above the AMS error for most of the allowed range for ϵ\epsilon. When going to the largest dark matter mass, shown in panel B3a-c, we get a similar series of pictures to B2a-c. However, now the binding energy is clearly within the positron energy range for AMS. Furthermore, the effect on the width of the recombination signal is more pronounced when comparing B3a with B3c. For B3a-b, the positron signal is below the error on AMS, while for B3c the positron isotropic uncertainty of AMS-02 barely touches the positron signal from dark recombination photons (for the maximum possible value of ϵ\epsilon). This is quite interesting because in this case AMS-02 will be able to probe the recombination dark photons before the annihilation ones.

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Figure 6: These figures show the solar positron spectra from DM annihilation. The red (blue) curve assumes the maximum (minimum) allowed ϵ\epsilon for each benchmark. The solid black curve is the uncertainty in the isotropic positron flux measured by AMS-02.

Apart from positron spectra, there are identical electron spectra. Furthermore, the dark photon can decay into three real photons, although with a suppressed branching Br(ϕ3γ)0.02α3=8109\sim\text{Br}(\phi\to 3\gamma)\simeq 0.02\alpha^{3}=8\cdot 10^{-9} Glover:1993nv in the case memϕm_{e}\ll m_{\phi}.

Our results show that AMS-02 can potentially discover a whole spectrum of positrons produced from dark photon decays outside the Sun. Alternatively this can be used to constrain DM models with dark photons. AMS-02 is only directed towards the Sun 1/80th of its livetime Feng:2016ijc . The uncertainty in the subset of the data from the Sun is likely much larger than the isotropic error. Collection of more data and knowledge of the measurements in the bins directed towards the Sun would potentially impose strong constraints.

VI Conclusions

In this paper we studied the positron spectrum produced by decaying dark photons that originate in the Sun. We consider dark photons that are produced inside the Sun via direct annihilation of XX¯X\bar{X}, decay of bound states XX¯X\bar{X} and bound state formation. These photons decay to positron-electron pairs and those decays that take place outside the Sun can potentially create a positron flux on Earth, that could be detected e.g. by AMS-02. We demonstrated that the spectrum has distinct features as a function of the positron energy that could distinguish it from any other astrophysical background of positrons. These features are due to contributions from different types of dark photons i.e. coming from direct annihilation, decay of para- or ortho-darkonium and recombination. More importantly we find that there is parameter space where AMS-02 or equivalent experiments would be able to pick up the contribution from the dark recombination photons before they have a chance to observe the positrons that come from dark photons produced by the typical direct annihilation of DM inside the Sun. This result appears to be surprising since in principle recombination photons are fewer and less energetic than those from direct annihilation. However as we have argued, the positrons produced from the decay of recombination photons span a much narrower energy band than the rest, leading to higher numbers in lower energy bins. Possible discovery of a positron spectrum with the morphology of our Fig. 5 not only can associate beyond any doubt the positron signal to its DM origin, but it could establish the type and the mass of the mediator, thus understanding how DM self-interacts.

Acknowledgements

The CP3-Origins centre is partially funded by the Danish National Research Foundation, grant number DNRF90. We would also like to thank Jordan Smolinsky for valuable correspondence regarding the solar capture rate.

Appendix A Verification of approximations

When solving the Boltzmann equations inside the Sun we have neglected a number of effects. Below we discuss the various effects we have neglected. The approximations are verified in table 1.

  1. 1.

    Darkonium ionization is negligible with respect to decay:
    The ionization cross section is related to the recombination cross section by the Milne-relation

    σion=mX2v28ω2σrecmX2vth24Δ2σrec,\sigma_{\text{ion}}=\frac{m_{X}^{2}v^{2}}{8\omega^{2}}\sigma_{\text{rec}}\approx\frac{m_{X}^{2}v_{\text{th}}^{2}}{4\Delta^{2}}\sigma_{\text{rec}}, (47)

    where ω=Δ+mXv2/4Δ\omega=\Delta+m_{X}v^{2}/4\approx\Delta is the energy of the photon. For our benchmark parameters, Eq. 17 describes σrec\sigma_{\text{rec}} within an order of magnitude, so we use this expression in the following estimate. If the mean free path for a dark photon ionizing darkonium is much larger than the thermal radius where DM is concentrated in the Sun, then ionization from recombination photons can be neglected. The ionization mean free path is λion1/(σionnD)\lambda_{\text{ion}}\sim 1/(\sigma_{\text{ion}}n_{D}) where nDn_{D} is the number density of darkonium. We use the steady state darkonium number densities to estimate the probability (Pion=1erth/λionrth/λionP_{\text{ion}}=1-e^{-r_{\text{th}}/\lambda_{\text{ion}}}\approx r_{\text{th}}/\lambda_{\text{ion}}) to ionize a darkonium particle before leaving the Sun. The values are given in table 1. Since recombination photons and darkonium are produced in the ratio 1:1, ionization will be negligible if recombination photons are very likely to leave the Sun. One might worry that the larger number of dark photons from annihilation and darkonium decay can mitigate the small likelihood of ionizing a darkonium state such that ionization becomes relevant. However, these dark photons have higher energy (mX\simeq m_{X}) and their likelihood for ionizing darkonia is much smaller. As a result ionization remains completely negligible.

  2. 2.

    Only ground state darkonium is appreciably populated in the Sun.
    When an excited state of darkonium makes a transition to the ground state by emission of a Lyman series photon, this photon can resonantly excite another ground state. This process can only be efficient if the mean free path of the Lyman-α\alpha dark photon is small compared to the thermal radius. The excitation cross section near resonance is Peebles:1994xt

    σLα=3λ28πγ2(ωω0)2+γ2/4\sigma_{\text{L}\alpha}=\frac{3\lambda^{2}}{8\pi}\frac{\gamma^{2}}{(\omega-\omega_{0})^{2}+\gamma^{2}/4} (48)

    where λ=2π/ω\lambda=2\pi/\omega, ω0=ΔΔ2=3αX2mX/16\omega_{0}=\Delta-\Delta_{2}=3\alpha_{X}^{2}m_{X}/16 is the photon energy, γ\gamma is the decay rate of the 2p2p state. Exactly on resonance the cross section becomes

    σLα=512π3αX4mX2.\sigma_{\text{L}\alpha}=\frac{512\pi}{3\alpha_{X}^{4}m_{X}^{2}}. (49)

    As before, we estimate the excitation probabilities by replacing σion\sigma_{\text{ion}} with σLα\sigma_{\text{L}\alpha} and summarise in table 1. The conclusion is that the effect of exciting ground state darkonia by absorbsion of Lyman-α\alpha dark photons is negligible.

  3. 3.

    Dark photons do not scatter before leaving the Sun.
    We now verify that the dark photons escape from the Sun with a negligible probability of scattering on DM or solar SM particles. The mean free path is λC(T)=1/(nTσC(T))\lambda_{\text{C}}^{(T)}=1/(n_{T}\sigma_{\text{C}}^{(T)}), where nTn_{T} is the number density of targets and σC\sigma_{\text{C}} is the Compton scattering cross section on target TT. If we take the target to be DM particles, we must have λC(X)rth\lambda_{\text{C}}^{(X)}\gg r_{\text{th}}, whereas for electrons, we must have λC(e)R\lambda_{\text{C}}^{(e)}\gg R_{\odot}. Among the SM particles we consider electrons because with a mean density of ne1030/n_{e}\sim 10^{30}/m3 constitute the most efficient target. The ϕ\phi-electron Compton scattering at the energies of interest i.e. sme\sqrt{s}\gg m_{e} is

    σC(e)=2πϵαXαslogsme2.\sigma_{\text{C}}^{(e)}=\frac{2\pi\epsilon\alpha_{X}\alpha}{s}\log\frac{s}{m_{e}^{2}}. (50)

    The largest value for the cross section is achieved for ϕ\phi produced in recombination where s=Δ\sqrt{s}=\Delta.

    For ϕ\phi scattering off DM particles, we use the cross section

    σC(X)=8παX23mX2.\sigma_{\text{C}}^{(X)}=\frac{8\pi\alpha_{X}^{2}}{3m_{X}^{2}}. (51)

    Again we summarise the scattering probabilities in table 1.

  4. 4.

    DM self-capture is negligible when the DM population in the Sun is at its steady state value.
    For DM self-capture to be negligible, the self-capture rate must be small compared to that on nuclei. In the steady state this requirement can be written as Cself-capNXSSCcapC_{\text{self-cap}}N_{X}^{\text{SS}}\ll C_{\text{cap}}. Equivalently, we must have τX1/Cself-cap\tau_{X}\ll 1/C_{\text{self-cap}}. Reference Feng:2016ijc has verified this is true if only direct annihilations are taken into account. Since Feng:2016ijc neglected recombination and τX=1/Ccap(Cann+Crec)\tau_{X}=1/\sqrt{C_{\text{cap}}(C_{\text{ann}}+C_{\text{rec}})}, the time scale is even smaller in our work, and self-capture remains negligible.


Benchmark mX/TeVm_{X}/\text{TeV} αX\alpha_{X} mϕ/MeVm_{\phi}/\text{MeV} ϵ2rth/λion\epsilon^{-2}r_{\text{th}}/\lambda_{\text{ion}} ϵ2rth/λLα\epsilon^{-2}r_{\text{th}}/\lambda_{\text{L}\alpha} ϵ2rth/λC(X)\epsilon^{-2}r_{\text{th}}/\lambda_{\text{C}}^{(X)} ϵ2R/λC(e)\epsilon^{-2}R_{\odot}/\lambda_{\text{C}}^{(e)}
B1 0.40.4 0.0110.011 1010 210222\cdot 10^{-22} 510245\cdot 10^{-24} 210282\cdot 10^{-28} 61086\cdot 10^{8}
B2a 22 0.0400.040 55 102610^{-26} 103110^{-31} 210322\cdot 10^{-32} 10610^{6}
B2b 22 0.0400.040 1515 210272\cdot 10^{-27} 210322\cdot 10^{-32} 410334\cdot 10^{-33} 10610^{6}
B2c 22 0.0400.040 7070 410294\cdot 10^{-29} 810348\cdot 10^{-34} 103410^{-34} 10610^{6}
B3a 139139 0.540.54 22 410404\cdot 10^{-40} 210502\cdot 10^{-50} 610436\cdot 10^{-43} 0.20.2
B3b 139139 0.540.54 2020 210412\cdot 10^{-41} 210512\cdot 10^{-51} 410444\cdot 10^{-44} 0.20.2
B3c 139139 0.540.54 100100 510435\cdot 10^{-43} 410534\cdot 10^{-53} 104510^{-45} 0.20.2
Table 1: Tabulated probabilities for a dark photon to ionize or excite ground state darkonium, as well as the likelihood of scattering on either DM or electrons before escaping from the Sun. The largest numbers appear in the last column, i.e. the largest effect we have neglected is scattering on electrons. Once the numbers are scaled by the relevant ϵ2\epsilon^{2} (typically around 102010^{-20}), scattering on electrons inside the Sun also become highly unlikely.

Appendix B Benchmark values


Benchmark mX/TeVm_{X}/\text{TeV} αX\alpha_{X} mϕ/MeVm_{\phi}/\text{MeV} Δ\Delta/GeV nmaxn_{\text{max}} n~\tilde{n} Ccap/(ϵ2/s)C_{\text{cap}}/(\epsilon^{2}/\text{s}) τX/(yr/ϵ)\tau_{X}/(\text{yr}/\epsilon) σrec/σann\sigma_{\text{rec}}/\sigma_{\text{ann}} NXss/ϵN_{X}^{\text{ss}}/\epsilon Noss/ϵ2N_{o}^{\text{ss}}/\epsilon^{2} Npss/ϵ2N_{p}^{\text{ss}}/\epsilon^{2} rth/Rr_{\text{th}}/R_{\odot} ϵmin1010\epsilon_{\text{min}}\cdot 10^{10} ϵmax1010\epsilon_{\text{max}}\cdot 10^{10}
B1 0.40.4 0.0110.011 1010 0.0120.012 11 11 1.210391.2\cdot 10^{39} 0.00370.0037 3.13.1 1.410441.4\cdot 10^{44} 1.010251.0\cdot 10^{25} 4.510214.5\cdot 10^{21} 0.00540.0054 1.61.6 3.33.3
B2a 22 0.0400.040 55 0.800.80 1212 77 3.810383.8\cdot 10^{38} 0.000480.00048 13.513.5 5.910425.9\cdot 10^{42} 3.610203.6\cdot 10^{20} 5.710175.7\cdot 10^{17} 0.00240.0024 2.32.3 3.13.1
B2b 22 0.0400.040 1515 0.800.80 77 55 8.710378.7\cdot 10^{37} 0.00110.0011 10.810.8 3.110423.1\cdot 10^{42} 8.010198.0\cdot 10^{19} 1.310171.3\cdot 10^{17} 0.00240.0024 1.31.3 3.53.5
B2c 22 0.0400.040 7070 0.800.80 33 33 3.010363.0\cdot 10^{36} 0.00710.0071 8.88.8 6.810416.8\cdot 10^{41} 2.710182.7\cdot 10^{18} 4.410154.4\cdot 10^{15} 0.00240.0024 0.620.62 1111
B3a 139139 0.540.54 22 1013310133 22512251 216216 2.110362.1\cdot 10^{36} 0.0000910.000091 30.330.3 5.910395.9\cdot 10^{39} 4.81094.8\cdot 10^{9} 1.01081.0\cdot 10^{8} 0.000290.00029 3.73.7 8.18.1
B3b 139139 0.540.54 2020 1013310133 712712 100100 1.410351.4\cdot 10^{35} 0.000380.00038 25.725.7 1.710391.7\cdot 10^{39} 3.21083.2\cdot 10^{8} 7.01067.0\cdot 10^{6} 0.000290.00029 1.21.2 1010
B3c 139139 0.540.54 100100 1013310133 318318 5959 3.610333.6\cdot 10^{33} 0.00250.0025 22.622.6 2.810382.8\cdot 10^{38} 8.11068.1\cdot 10^{6} 1.81051.8\cdot 10^{5} 0.000290.00029 0.520.52 4949
Table 2: Summary table of key benchmark values. The values for nmaxn_{\text{max}} and n~\tilde{n} have been rounded down to nearest integer.

Appendix C Self-interaction and Bound state formation

In this section, we present how we numerically obtain the cross sections for self-interaction (XXXX, XX¯X\bar{X}, X¯X¯\bar{X}\bar{X}) and bound state formation (XX¯DX\bar{X}\to D). We will use a non-relativistic approach where the scattering is described by a Yukawa potential

V(r)=±αXremϕr,V(r)=\pm\frac{\alpha_{X}}{r}e^{-m_{\phi}r}\,, (52)

where the plus (minus) is for repulsive (attractive) interactions. When comparing with constraints on self-interaction from DM distributions, the relevant quantity is the transfer cross section

σT=𝑑Ω(1cosθ)dσdΩ.\sigma_{T}=\int d\Omega\,(1-\cos\theta)\,\frac{d\sigma}{d\Omega}. (53)

Analytical results are known within the Born approximation and the classical regime. In between these regions, both quantum mechanical and non-perturbative effects are important. We therefore have to solve the Schrödinger equation and use partial wave analysis to express the transfer cross section as a sum over partial waves \ell

σTk24π==0(+1)sin2(δ+1δ),\frac{\sigma_{T}k^{2}}{4\pi}=\sum_{\ell=0}^{\infty}(\ell+1)\sin^{2}(\delta_{\ell+1}-\delta_{\ell}), (54)

where δ\delta_{\ell} is the phase shift for the partial wave \ell and k=μvk=\mu v with vv the relative velocity and μ=mX/2\mu=m_{X}/2 the reduced mass. We obtain the phase shifts δ\delta_{\ell} by solving the Schrödinger equation for the radial wave function R(r)R_{\ell}(r) for the reduced two-particle system,

1r2ddr(r2dRdr)+(k2(+1)r22μV(r))R=0\frac{1}{r^{2}}\frac{d}{dr}\Big{(}r^{2}\frac{dR_{\ell}}{dr}\Big{)}+\Big{(}k^{2}-\frac{\ell(\ell+1)}{r^{2}}-2\mu V(r)\Big{)}R_{\ell}=0 (55)

and match R(r)R_{\ell}(r) to its asymptotic solution

limrR(r)j(kr)cosδn(kr)sinδ,\lim_{r\to\infty}R_{\ell}(r)\propto j_{\ell}(kr)\,\cos\delta_{\ell}-n_{\ell}(kr)\,\sin\delta_{\ell}\,, (56)

expressed in terms of spherical Bessel (Neumann) functions jj_{\ell} (nn_{\ell}).

Within the dipole approximation, the cross section for bound state formation is given by An:2016gad

(σv)B=αD3πn,(ωn2+12mϕ2)ωn2mϕ2[|𝑑rr3R~nR1|2+(+1)|𝑑rr3R~nR+1|2],(\sigma v)_{\rm B}=\frac{\alpha_{D}}{3\pi}\sum_{n,\ell}\left(\omega_{n\ell}^{2}+\frac{1}{2}m_{\phi}^{2}\right)\sqrt{\omega_{n\ell}^{2}-m_{\phi}^{2}}\left[\ell\left|\int drr^{3}\tilde{R}_{n\ell}R_{\ell-1}\right|^{2}+(\ell+1)\left|\int drr^{3}\tilde{R}_{n\ell}R_{\ell+1}\right|^{2}\right]\ , (57)

where R(r)R_{\ell}(r) is the radial wavefunction of the incoming state, satisfying Eq. (55), while R~n\tilde{R}_{n\ell} is the radial wavefunction of the (n)(n\ell)’th bound state of the Yukawa potential. The quantity ωn=En+k2/(2μ)\omega_{n\ell}=E_{n\ell}+k^{2}/(2\mu) is the sum of the binding energy of the (n)(n\ell)’th bound state and the kinetic energy of the incoming state. In general, the binding energy of the Yukawa potential depends on both nn and \ell. However, since the size of those bound states, which are deep enough to emit an on-shell dark photon in their formation, is much smaller than 1/mϕ1/m_{\phi}, we will use the following approximations:

EnEn=αX2μ2n2R~nR~nCoulomb,E_{n\ell}\simeq E_{n}=\frac{\alpha_{X}^{2}\mu}{2n^{2}}\quad\quad\tilde{R}_{n\ell}\simeq\tilde{R}_{n\ell}^{\text{Coulomb}}\,, (58)

with

R~nCoulomb(r)=2n+2(2+1)!(n+)!(n1)!(2r)a0+3/2e(r/na0)F1(1+n,2+2,2rna0),\tilde{R}_{n\ell}^{\text{Coulomb}}(r)=\frac{2}{n^{\ell+2}(2\ell+1)!}\sqrt{\frac{(n+\ell)!}{(n-\ell-1)!}}\ \frac{(2r)^{\ell}}{a_{0}^{\ell+3/2}}e^{-\left(r/{na_{0}}\right)}F_{1}\left(1+\ell-n,2+2\ell,\frac{2r}{na_{0}}\right)\ , (59)

where a0=1/(αXμ)a_{0}=1/(\alpha_{X}\mu) is the Bohr radius and F1F_{1} is the Krummer confluent hypergeometric function.

In order to solve the problem numerically, we introduce dimensionless quantities.

χrR,xαXmXr,av2αX,bαXmXmϕ,\chi_{\ell}\equiv rR_{\ell}\,,\quad x\equiv\alpha_{X}m_{X}r\,,\quad a\equiv\frac{v}{2\alpha_{X}}\,,\quad b\equiv\frac{\alpha_{X}m_{X}}{m_{\phi}}\;, (60)

and rewrite the Schrodinger equation as

(d2dx2+a2(+1)x2±1xex/b)χ(x)=0.\left(\frac{d^{2}}{dx^{2}}+a^{2}-\frac{\ell(\ell+1)}{x^{2}}\pm\frac{1}{x}\,e^{-x/b}\right)\chi_{\ell}(x)=0\;. (61)
Refer to caption
Figure 7: Sketch of the contributions to the curvature of the solution.

We then use a slightly modified version of the numerical procedure in Tulin:2013teo to solve for χ(x)\chi_{\ell}(x) (Step 1 and 2) and extract δ\delta_{\ell} (Step 3) to be able to do the sum in Eq. 54 (Step 4) and the integration in Eq. 57 (Step 6):

  1. 1.

    Initial Conditions For xib,(+1)/ax_{i}\ll b,(\ell+1)/a, Eq. (61) is dominated by the angular momentum term, see Fig. 7, and the solution χ(x)x+1\chi_{\ell}(x)\propto x^{\ell+1}. We thus impose as initial condition:

    χ(xi)=1χ(xi)=(+1)/xi.\chi_{\ell}(x_{i})=1\quad\quad\chi_{\ell}^{\prime}(x_{i})=(\ell+1)/x_{i}\,. (62)

    For xi1x_{i}\ll 1 this is also true for =0\ell=0. The overall normalization is fixed in step 5.

  2. 2.

    Radial Solution We solve Eq. 61 numerically from xix_{i} to xex_{e}. The end point xex_{e} is determined so we can afterwards perform the steps matching, normalization and integration. The matching point xmx_{m} is determined by the condition a2exp(xm/b)/xma^{2}\gg\exp(-x_{m}/b)/x_{m}, where the potential term is suppressed compared to the kinetic term (see Fig. 7). For normalization we need a few free oscillations, xnorm>2π/ax_{norm}>2\pi/a, and we need to be able to do the integrals of Eq. 57, xint>1/mϕx_{int}>1/m_{\phi}.

  3. 3.

    Matching At x=xexmx=x_{e}\geq x_{m}, we match χ\chi_{\ell} (and its first derivative) onto the asymptotic solution, given by

    χ(x)xeiδ(cosδj(ax)sinδn(ax)).\chi_{\ell}(x)\propto x\,e^{i\delta_{\ell}}\big{(}\cos\delta_{\ell}\,j_{\ell}(ax)-\sin\delta_{\ell}\,n_{\ell}(ax)\big{)}\;. (63)

    Inverting Eq. (63), the phase shift is given by

    tanδ=axej(axe)βj(axe)axen(axe)βn(axe),β=xeχ(xe)χ(xe)1,\tan\delta_{\ell}=\frac{ax_{e}\,j^{\prime}_{\ell}(ax_{e})-\beta_{\ell}\,j_{\ell}(ax_{e})}{ax_{e}\,n^{\prime}_{\ell}(ax_{e})-\beta_{\ell}\,n_{\ell}(ax_{e})}\;,\quad\beta_{\ell}=\frac{x_{e}\chi_{\ell}^{\prime}(x_{e})}{\chi_{\ell}(x_{e})}-1, (64)

    in terms of our numerical solution for χ\chi_{\ell} at xex_{e}. The numerical method makes an initial guess for (xi,xm)(x_{i},x_{m}) and computes δ\delta_{\ell}, and then successively decreases (increases) xix_{i} (xmx_{m}) until δ\delta_{\ell} converges at 1%1\%.

  4. 4.

    Summation We compute σT\sigma_{T} by summing Eq. 54 over \ell, truncating at max\ell_{\rm max}. We iterate max\ell_{\rm max} until σT\sigma_{T} converges to 1%1\% and δmax<0.01\delta_{\ell_{\rm max}}<0.01 through ten successive iterations.

  5. 5.

    Normalization We normalize the solution χ(x)\chi_{\ell}(x) such that it has the same amplitude as the \ell-th partial wave for xe>x>xmx_{e}>x>x_{m}.

  6. 6.

    Integration We perform the integrals in Eq. 57 for all the energy levels satisfying En>mϕE_{n}>m_{\phi}.

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