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Constraining Axion Mass Constraining Axion Mass through Gamma-ray Observations of Pulsars Sheridan J. Lloyd, a) Paula M. Chadwick, b) and Anthony M. Brown c) Centre for Advanced Instrumentation, Dept. of Physics, University of Durham, South Road, Durham, DH1 3LE, UK (Dated: 12 August 2019) We analyze 9 years of pass 8 Fermi -LAT data in the 60-500 MeV range and determine flux upper limits (UL) for 17 gamma-ray dark pulsars as a probe of axions produced by nucleon-nucleon Bremsstrahlung in the pulsar core. Using a previously published axion decay gamma-ray photon flux model for pulsars which relies on a high core temperature of 20 MeV, we improve the determination of the UL axion mass (m a ), at 95 percent confidence level, to 9.6 × 10 -3 eV, which is a factor of 8 improvement on previous results. We show that the axion emissivity (energy loss rate per volume) at realistic lower pulsar core temperatures of 4 MeV or less is reduced to such an extent that axion emissivity and the gamma-ray signal becomes negligible. We consider an alternative emission model based on energy loss rate per mass to allow m a to be constrained with Fermi -LAT observations. This model yields a plausible UL m a of 10 -6 eV for pulsar core temperature <0.1 MeV but knowledge of the extent of axion to photon conversion in the pulsar B field would be required to make a precise UL axion mass determination. The peak of axion flux is likely to produce gamma-rays in the 1 MeV energy range and so future observations with medium energy gamma-ray missions, such as AMEGO and e-ASTROGAM, will be vital to further constrain UL m a . Keywords: astroparticle physics – axion: general – gamma-rays: general – pulsars: general I. INTRODUCTION The axion, a Nambu-Goldstone boson, is a solution to the strong CP problem of QCD and a plausible cold dark matter candidate [1–3]. The mass of the axion m a can be constrained by astrophysical arguments such as the dura- tion of the neutrino burst of SN-1987A (m a <5 × 10 -3 eV) [4] or by direct detection experiments such as ADMX [5] where Galactic halo axions convert to microwave photons in a magnetic field, excluding m a in the range (1.9-3.53) × 10 -6 eV [6–10]. The authors of [11] have used cool- ing simulations, combined with surface temperature mea- surements of 4 thermal X-ray emitting pulsars (PSRs), to determine m a <(0.06-0.12 eV). In the gamma-ray regime, the authors of [12] have used 5 years of pass 7 Fermi - LAT gamma-ray observations of radiative axion decay in 4 nearby PSRs to constrain m a <0.079 eV. The latest data release of the Fermi -LAT is now pass 8, which incorporates improvements to further reduce gamma-ray background uncertainty, improve instrument effective area and point spread function (PSF) and to per- mit low-energy analysis down to 60 MeV. In this paper we will seek to refine the work of [12] to take advantage of the improved low-energy analysis in pass 8, coupled with improved photon statistics (9 years of event data) and a larger sample of 17 gamma-ray dark PSRs. This should allow a more robust determination of UL m a than was possible previously. This paper is structured as follows. In Section II we describe the phenomenology of the axion and its pro- duction in neutron stars. In Section III we describe the criteria used to select pulsars for analysis. In Section IV we describe our analysis method for the determina- tion of gamma-ray upper limits from the pulsar sample. In Section V we present UL energy and photon flux de- terminations for the pulsar sample and from these derive the axion mass upper limit m a by two independent meth- ods. In Section VI we discuss the validity of the UL m a determination with respect to pulsar core temperature. Finally in Section VII we summarise our findings and make suggestions for future work. II. PHENOMENOLOGY In this section we discuss the mechanism for axion pro- duction in degenerate pulsar cores and describe how this process is modelled through a spin structure function. We then restate how the axion emissivity or energy loss rate per volume is expressed in terms of this spin struc- ture function. We use a published astrophysical model for the photon flux arising from axion emission and de- cay in pulsars to derive an expression for UL axion mass. Finally we derive an alternative expression for UL axion mass by using the expected energy loss rate per mass due to axion production to give an expected gamma-ray lu- minosity for a canonical pulsar and then equate this to the measured gamma-ray upper limits of the pulsars we consider. Axions may be produced in pulsar cores through the process of nucleon-nucleon Bremsstrahlung as depicted in the Feynman diagram of Fig. 1. The Bremsstrahlung process assumes a one pion exchange (OPE) approxima- tion [13] and the nucleons involved are considered to be neutrons. Incoming nucleons N 1 ,N 2 and outgoing nucle- arXiv:1908.03413v1 [astro-ph.HE] 9 Aug 2019
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Page 1: Constraining Axion Mass through Gamma-ray …Constraining Axion Mass 3 t= 23:2s eV m a 2 (7) By combining Eqn. 6 and Eqn. 7 the UL axion mass can be expressed in terms of the UL gamma-ray

Constraining Axion Mass

Constraining Axion Mass through Gamma-ray Observations of Pulsars

Sheridan J. Lloyd,a) Paula M. Chadwick,b) and Anthony M. Brownc)

Centre for Advanced Instrumentation, Dept. of Physics, University of Durham, South Road,

Durham, DH1 3LE, UK

(Dated: 12 August 2019)

We analyze 9 years of pass 8 Fermi -LAT data in the 60−500 MeV range and determineflux upper limits (UL) for 17 gamma-ray dark pulsars as a probe of axions produced bynucleon-nucleon Bremsstrahlung in the pulsar core. Using a previously published axion decaygamma-ray photon flux model for pulsars which relies on a high core temperature of 20 MeV,we improve the determination of the UL axion mass (ma), at 95 percent confidence level, to9.6 × 10-3 eV, which is a factor of 8 improvement on previous results. We show that the axionemissivity (energy loss rate per volume) at realistic lower pulsar core temperatures of 4 MeVor less is reduced to such an extent that axion emissivity and the gamma-ray signal becomesnegligible. We consider an alternative emission model based on energy loss rate per mass toallow ma to be constrained with Fermi -LAT observations. This model yields a plausible ULma of 10-6 eV for pulsar core temperature <0.1 MeV but knowledge of the extent of axionto photon conversion in the pulsar B field would be required to make a precise UL axionmass determination. The peak of axion flux is likely to produce gamma-rays in the ≤ 1 MeVenergy range and so future observations with medium energy gamma-ray missions, such asAMEGO and e-ASTROGAM, will be vital to further constrain UL ma.

Keywords: astroparticle physics – axion: general – gamma-rays: general – pulsars: general

I. INTRODUCTION

The axion, a Nambu-Goldstone boson, is a solution tothe strong CP problem of QCD and a plausible cold darkmatter candidate [1–3]. The mass of the axion ma can beconstrained by astrophysical arguments such as the dura-tion of the neutrino burst of SN-1987A (ma <5× 10-3 eV)[4] or by direct detection experiments such as ADMX [5]where Galactic halo axions convert to microwave photonsin a magnetic field, excluding ma in the range (1.9-3.53)× 10-6 eV [6–10]. The authors of [11] have used cool-ing simulations, combined with surface temperature mea-surements of 4 thermal X-ray emitting pulsars (PSRs), todetermine ma <(0.06-0.12 eV). In the gamma-ray regime,the authors of [12] have used 5 years of pass 7 Fermi -LAT gamma-ray observations of radiative axion decay in4 nearby PSRs to constrain ma <0.079 eV.

The latest data release of the Fermi -LAT is now pass8, which incorporates improvements to further reducegamma-ray background uncertainty, improve instrumenteffective area and point spread function (PSF) and to per-mit low-energy analysis down to 60 MeV. In this paperwe will seek to refine the work of [12] to take advantageof the improved low-energy analysis in pass 8, coupledwith improved photon statistics (9 years of event data)and a larger sample of 17 gamma-ray dark PSRs. Thisshould allow a more robust determination of UL ma thanwas possible previously.

This paper is structured as follows. In Section II wedescribe the phenomenology of the axion and its pro-duction in neutron stars. In Section III we describe thecriteria used to select pulsars for analysis. In Section

IV we describe our analysis method for the determina-tion of gamma-ray upper limits from the pulsar sample.In Section V we present UL energy and photon flux de-terminations for the pulsar sample and from these derivethe axion mass upper limit ma by two independent meth-ods. In Section VI we discuss the validity of the UL ma

determination with respect to pulsar core temperature.Finally in Section VII we summarise our findings andmake suggestions for future work.

II. PHENOMENOLOGY

In this section we discuss the mechanism for axion pro-duction in degenerate pulsar cores and describe how thisprocess is modelled through a spin structure function.We then restate how the axion emissivity or energy lossrate per volume is expressed in terms of this spin struc-ture function. We use a published astrophysical modelfor the photon flux arising from axion emission and de-cay in pulsars to derive an expression for UL axion mass.Finally we derive an alternative expression for UL axionmass by using the expected energy loss rate per mass dueto axion production to give an expected gamma-ray lu-minosity for a canonical pulsar and then equate this tothe measured gamma-ray upper limits of the pulsars weconsider.

Axions may be produced in pulsar cores through theprocess of nucleon-nucleon Bremsstrahlung as depictedin the Feynman diagram of Fig. 1. The Bremsstrahlungprocess assumes a one pion exchange (OPE) approxima-tion [13] and the nucleons involved are considered to beneutrons. Incoming nucleons N1, N2 and outgoing nucle-

arX

iv:1

908.

0341

3v1

[as

tro-

ph.H

E]

9 A

ug 2

019

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Constraining Axion Mass 2

Fig. 1 Feynman diagram depicting the nucleon-nucleonBremsstrahlung process which produces axions. Incomingnucleons N1,2 undergo a one-pion exchange producing an axion aand outgoing nucleons N3,4 with different energy and momentafrom those of N1,2. The axion undergoes radiative (conservative)decay to two gamma-ray photons.

ons N3, N4 undergo one pion exchange to produce axionsof energy ω via the Bremsstrahlung process. The axionsthen undergo radiative decay to gamma-ray photons.

The axion has a mass ma which is related to the Peccei-Quinn scale fa through a scaling relation (Eqn. 1).

ma ≈ 6µ eV( fa

1012 GeV

)−1(1)

The spin structure function Sσ(ω) (Eqn. 2) is a phasespace integral corresponding to the Bremsstrahlung pro-cess depicted in Fig.1. The phase space integral accountsfor nucleon spin and the balanced energy (E1,2,3,4) andmomenta (p1,2,3,4) transfer between nucleons N1,2,3,4

with conservation of momenta and energy provided byDirac δ functions. The momenta pi have integration lim-its in the range 0 <pi <2pFn where pFn is the neutronFermi momentum. pFn is 300-400 MeV in supernovaecores [14] and typically >100 MeV in neutron stars [15].F in Eqn. 2 is the product of thermodynamic functions asdefined in Eqn. 3. Hij is the hadronic tensor incorporat-ing nucleon spin with value 10/ω2. The rate of axion pro-duction can be determined independently of the OPE ap-proximation using the soft-neutrino radiation rate whichis proportional to the nucleon nucleon on-shell scatter-ing amplitude. This soft-neutrino approximation (SNA)method gives an axion emission rate which is a factor offour smaller than that given by the OPE approximation[15]. It can be shown that a value of Hij = 10/ω2 largelyincludes the reduction in axion emission rate expectedfor the SNA by considering expressions for the scatter-ing kernel of neutrinos produced by Bremsstrahlung insupernovae cores as presented in [16] where the SNA hasnot been applied. We can take the spin structure function

Sσ(ω) (Eqn. 2) to be analogous to the neutrino scatteringkernel Sσ(ω) of [16] and thus equate Hij to the spatialtrace, M , in the neutrino scattering kernel expression of[16]. By combining the expressions presented in [16] for ageneric scattering kernel, the spin fluctuation rate and aneffective degeneracy parameter, we obtain a Hij value of30/ω2. Thus, a value of 10/ω2 for Hij results in a factorof 3 reduction in axion emissivity which is comparablewith the factor of 4 reduction expected from the SNA.The thermodynamic function (Eqn. 4) is the Fermi Diracdistribution in natural units (kB=1) for the nucleons ap-plicable to degenerate matter [17] incorporating energyE, temperature T and neutron star degeneracy µ. Wetake the value of µ/T = 10 as used in the analysis of[12].

Sσ(ω) =1

4

∫ [ ∏i=1..4

d3pi(2π)3

]× (2π)4δ3(p1 + p2 − p3 − p4)

× δ(E1 + E2 − E3 − E4 − ω)FHij

(2)

F = f(E1)f(E2)(1− f(E3)(1− f(E4)) (3)

f(E) = 1/(1 + exp((E − µ)/T )) (4)

The axion emissivity or energy loss rate per volumein natural units (i.e. ~=c=1), εa is defined by Eqn. 5as given in [15] where MN is the nucleon mass of 938MeV and gann is the axion-nucleon coupling with gann=CNMN/fa. CN encapsulates the vacuum expectation val-ues for the Higgs u and d doublets with the doubletsgiving mass to the up and down quarks of the nucleons.The value of CN depends on the coupling model consid-ered with 0 <CN <2.93 [18]; we take CN=0.1 as [12].

εa =g2ann

48π2M2N

∫ω4Sσ(ω) dω (5)

The expected photon flux arising from axion decay fora photon of energy E is given by Eqn. 6 from [12] whered is the distance to the pulsar in parsecs and ∆t is thetimescale for the emission of axions from a neutron starwith a core temperature of 20 MeV (Eqn. 7). We takethe value of Sσ(ω) to be 2.4 × 107 MeV2 and 6.25 × 104

MeV2 for axion energies of 100 MeV and 200 MeV respec-tively from the values of ω4Sσ(ω) in the axion emissivityversus energy plot of [12] for a pulsar of core temperature20 MeV and µ/T = 10. We choose Sσ(ω) at ω=100 MeVand ω=200 MeV in our calculations because these rep-resent reasonable extremes on the emissivity plot, withemissivity peaking and being less sensitive to energy nearω=100 MeV and an emissivity cut-off at ω=230 MeV.

EdΦ

dE= 1.8× 10−2

(ma

eV

)5( ∆ t

23.2 s

)(100 pc

d

)2×( 2E

100 MeV

)4( Sσ(2E)

107 MeV2

)cm−2 s−1

(6)

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Constraining Axion Mass 3

∆t = 23.2 s( eV

ma

)2(7)

By combining Eqn. 6 and Eqn. 7 the UL axion masscan be expressed in terms of the UL gamma-ray photonflux Φ of a pulsar (Eqn. 8).

ULma =[UL Φ cm−2 s−1 × 55.5 ×

( d

100 pc

)2×(100 MeV

2E

)4(107 MeV2

Sσ(2E)

)] 13

(8)

Alternatively, instead of using photon flux methods asdescribed above, axion mass can be constrained using anexpression for the energy lost from the pulsar as a resultof axion production. The energy loss rate εa

D for a givenmass of neutron star material arising from the productionof axions in the pulsar core (Eqn. 9) is as presented in[19] based on [13] and [17] with αa as Eqn. 10. TMeV

is the neutron star core temperature in MeV and ρ15 isthe neutron star mass density in units of 1015 g cm-3 Weinclude a further factor of 0.25 in Eqn. 9 to allow for theSNA reduction in axion emission rate.

εaD = 0.25× αa1.74× 1031erg g−1 s−1 ρ

−2/315 T 6

MeV

(9)

αa ≡(CNMN

fa

)2/4π (10)

The measured UL gamma-ray luminosity, Lγ can beequated to the expected gamma-ray luminosity arisingfrom the axion energy loss rate for the total mass of theneutron star as Lγ=εa

DNSmass Pa→ γ , where NSmass

is the neutron star mass expressed in grams and Pa→ γ

is the axion to photon conversion probability (0-1.0) inthe pulsar B field. In the case of axion radiative decaywhere an axion decays to two gamma-ray photons, with-out conversion in the pulsar B field being required, wetake Pa→ γ to be 1.1 × 10-24 s-1(ma/1 eV) 5[20]. Fromthe above expression for Lγ and by combining Eqns. 1,9 and 10 we obtain an expression for UL ma (Eqn. 11).We assume a canonical pulsar mass of 1.4 M� or 2.786× 1033 g and a density of 0.056 × 1015 g cm-3.

ULma =6.0× 1015

CNMN×

( 4πLγ erg s−1

0.435× 1031erg g−1 s−1 ρ−2/315 T 6

MeVNSmassP a→ γ

) 12

(11)

III. PULSAR SELECTION

We make the simple assumption that axions are emit-ted in a continuous isotropic fashion by the pulsar and

are unaffected by pulsar rotation. In making our pulsarselection we want to maximise the probability of detect-ing isotropic gamma-ray emission arising solely from thedecay of axions to gamma-rays. Thus we wish to excludethe pulsed gamma-ray emission arising from pulsar mag-netospheric emission which would be unrelated to axionproduction and a background to the axion signal that wewish to measure. Therefore, our selection of 17 pulsars(Table I) from version 1.57 of the Australia Telescope Na-tional Facility(ATNF) catalogue[21]22 is based on the fol-lowing criteria to minimise gamma-ray background andto select well-measured pulsars which are most likely toemit detectable gamma-rays solely through axion decay:

• We include pulsars which are located off the Galac-tic plane (|b|>15°) thus reducing the uncertaintyarising from the Galactic gamma-ray backgroundmodel of the Galactic disc

• We include pulsars away from the Galactic centrewith l>30° and l<330°

• We include nearby pulsars with a heliocentric dis-tance of 0.5 kpc or less and possessing an E >0 inthe ATNF catalogue

• We include only pulsars which are not known tohave binary companions in the ATNF catalogueand have not been identified as prior sources ofgamma-ray emission in either the Public List ofLAT-Detected Gamma-Ray Pulsars23 (which listsall publicly-announced gamma-ray pulsar detec-tions, whose significance exceeds 4σ) or in theSecond Fermi Large Area Telescope Catalog ofGamma-Ray Pulsars [24].

IV. ANALYSIS

IV.A. Photon Event Data Selection

The data in this analysis were collected by Fermi -LATbetween 4th Aug 2008 to 18th October 2017 (MissionElapsed Time (MET) 2395574147[s] to 530067438[s]).We consider all pass 8 events which are source classphotons (evclass=128), with Front converting events (ev-type=1), spanning the energy range 60 to 500 MeV. Weuse Front44 converting events because of the improvedpoint spread function (PSF) of this event class with 95per cent containment of 60 MeV photons at a contain-ment angle of 13° as opposed to 20° for both Front andBack converting events. We select a conservative energyrange of 60-500 MeV, as axion decay has previously beenexpected to produce gamma-rays in the range 60-200MeV, with a cut-off by 200 MeV [12]. Throughout ouranalysis, the Fermipy software package45[46] with ver-sion v10r0p5 of the Fermi Science Tools is used, in con-junction with the p8r2 source v6 instrument responsefunctions. We apply the standard pass 8 cuts to thedata, including a zenith angle 90° cut to exclude pho-tons from the Earth limb and good-time-interval cuts of

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Constraining Axion Mass 4

Name l b RA Dec Period (s) Distance B Surface B Light E Spin Downand Ref. (degree) (degree) (degree) (degree) and Ref. (kpc) (1010 Gauss) Cylinder (Gauss) (1030 erg s-1) Age (105 Yr)

J0736-6304 [25] 274.88 -19.15 114.08 -63.07 4.863 [26] 0.10 2750.00 2.24 52.1 5.07J0711-6830 [27] 279.53 -23.28 107.98 -68.51 0.005 [28] 0.11 0.03 16400 3550 58400J0536-7543 [29] 287.16 -30.82 84.13 -75.73 1.246 [30] 0.14 84.90 4.12 11.5 349J0459-0210 [31] 201.44 -25.68 74.97 -2.17 1.133 [32] 0.16 127.00 8.21 37.9 128J0837+0610 [33] 219.72 26.27 129.27 6.17 1.274 [32] 0.19 298.00 13.50 130.0 29.7J0108-1431 [34] 140.93 -76.82 17.03 -14.53 0.808 [32] 0.21 25.20 4.49 5.8 1660J0953+0755 [33] 228.91 43.70 148.29 7.93 0.253 [32] 0.26 24.40 141.00 560.0 175J1116-4122 [29] 284.45 18.07 169.18 -41.38 0.943 [35] 0.28 277.00 31.00 374.0 18.8J0630-2834 [36] 236.95 -16.76 97.71 -28.58 1.244 [32] 0.32 301.00 14.70 146.0 27.7J0826+2637 [37] 196.96 31.74 126.71 26.62 0.531 [32] 0.32 96.40 60.50 452.0 49.2J1136+1551 [33] 241.90 69.20 174.01 15.85 1.188 [32] 0.35 213.00 11.90 87.9 50.4J0656-5449 [38] 264.80 -21.14 104.20 -54.82 0.183 [38] 0.37 7.74 118.00 205.0 909J0709-5923 [38] 270.03 -20.90 107.39 -59.40 0.485 [38] 0.37 25.00 20.50 43.5 610J0636-4549 [39] 254.55 -21.55 99.14 -45.83 1.985 [39] 0.38 254.00 3.05 16.0 99.1J0452-1759 [40] 217.08 -34.09 73.14 -17.99 0.549 [32] 0.40 180.00 102.00 1370.0 15.1J0814+7429 [41] 140.00 31.62 123.75 74.48 1.292 [32] 0.43 47.20 2.05 3.1 1220J2307+2225 [42] 93.57 -34.46 346.92 22.43 0.536 [43] 0.49 6.91 4.21 2.2 9760

Table I Our selection of 17 pulsars from the ATNF catalogue showing their Galactic longitude/latitude, RA and Dec co-ordinates, period,pulsar distance, magnetic field B at surface and light cylinder in Gauss, E and spin down age. Discovery and period are from the referenceslisted.

DATA QUAL >0 and LAT CONFIG = 1. The energybinning used is 4 bins per decade in energy and spatialbinning is 0.1° per image pixel.

IV.B. Determining if Pulsars are Gamma-ray Emitters

We first determine if any of the pulsars in our selectionare significant unpulsed gamma-ray emitters. For eachpulsar we consider a 20° Radius of Interest (ROI) centredon the pulsar co-ordinates. We use an ROI of 20° as ouranalysis is made down to a low energy of 60 MeV andwe wish to be certain to allow for the contribution of lowenergy sources given the PSF of 13° above.

We include known sources using a point sourcepopulation derived from the Fermi -LAT’s third pointsource catalog (3FGL), diffuse gamma-ray emission andextended gamma-ray sources. The diffuse gamma-ray emission consists of two components: the Galac-tic diffuse flux and the isotropic diffuse flux. TheGalactic component is modelled with Fermi -LAT’sgll iem v06.fit spatial map with the normalisation freeto vary. The isotropic diffuse emission is defined byFermi’s iso P8R2 SOURCE V6.txt tabulated spectraldata. The normalisation of the isotropic emission is alsoleft free to vary. In addition, all known sources take theirspectral shape as defined in the 3FGL catalogue.

An energy dispersion correction is applied to the pulsartest source but disabled for all 3FGL sources in line withFermi Science Support Centre recommendations for lowenergy analysis.

We perform an initial binned likelihood analysis usingthe optimize method with the normalisation of all pointsources within 20 ° of the pulsar being left free.

From this initial likelihood fit, all point sources (withthe exception of the target pulsar) with a TS < 4, or witha predicted number of photons, Npred < 4 are removedfrom the model. Thereafter, we free the spectral shape ofall TS > 25 sources in this refined model and undertake

a further secondary likelihood fit using optimize and fitmethods.

The best-fit model from this secondary likelihood fitis then used with the Fermi Science Tool gttsmap,to search for new point sources that were not alreadypresent in the 3FGL. In particular, we run Fermipy’s‘find sources’ method to detect all sources above 3σ sig-nificance. Find sources is a peak detection algorithmwhich analyses the test statistic (TS) map to find newsources over and above those defined in the 3FGL modelby placing a test point source, defined as a power lawwith spectral index 2.0, at each pixel on the TS mapand recomputing likelihood. Lastly, we again run the fitmethod to perform a final likelihood fit, which fits allparameters that are currently free in the model and up-dates the TS and predicted count (Npred) values of allsources.

IV.C. Pulsar Upper Limit Gamma-ray Emission

In order to determine PSR gamma-ray flux upper lim-its we repeat the analysis of Section IV.B with a sourcemodel which includes a pulsar test source for each of the17 pulsars. The differential flux, dN/dE, (photon flux perenergy bin) of the test source for each pulsar is describedas a power law47 as defined in Eqn. 12 where prefactor= N0, index=γ and scale=E0. The test source has indexof 2.0, a scale of 1 GeV and a prefactor = 1 × 10 -11. Weleave the prefactor (normalisation) and index of the testsource free to vary.

dN

dE= N0

( EE0

)γ(12)

We then obtain UL photon and energy fluxes inte-grated over the energy analysis range (at 2 σ signifi-cance, 95 percent confidence level) from the flux ul95 andeflux ul95 attributes respectively of the fermipy sources

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Constraining Axion Mass 5

entry for each pulsar test source. The UL photon and en-ergy fluxes are defined as the values where the likelihoodfunction, 2∆Log(L), which compares the likelihood of amodel with the source and without, has decreased by 2.71from its maximum value across the range of flux valuesarising from the analysis. In addition, we use a com-posite likelihood stacking technique to improve the ULphoton flux determination by considering all test sourcesin the analysis together. We extract a likelihood profile of∆Log(L) vs photon flux for each test source using the fer-mipy profile norm method. Next we determine the func-tional form of this likelihood profile for each test sourceusing numpy polyfit and poly1d and interpolate the like-lihood profile with numpy polyval between the overallminimum and maximum photon flux value obtained byconsidering the UL photon flux of all test sources. Wethen sum the ∆Log(L) values of each interpolated likeli-hood profile to obtain a single stacked ∆Log(L) vs photonflux profile for the test sources as a whole. Finally, wedetermine the maximum photon flux where the stacked∆Log(L) has decreased by 1.35 from its peak value togive the one-sided upper limit photon flux.

V. RESULTS

V.A. Pulsar UL Gamma-ray Fluxes

We list the UL photon, energy fluxes and gamma-rayluminosities (assuming the distances in Table I) for oursample of pulsars in Tables II and III. The UL photon fluxat 95 percent confidence obtained by likelihood stackingof all 17 pulsars is 7.8 × 10-10 cm-2 s-1.

V.B. Upper Limit ma Determination

We list our determination of UL ma in Tables II and IIIfor each pulsar derived from the UL photon flux andEqn. 8 for axions of energy 100 MeV and 200 MeV. Theaverage UL ma considering all 17 pulsars is 9.6 × 10-3

eV and 3.21 × 10-2 eV for axions of energy 100 MeV and200 MeV respectively. We obtain an average UL ma forthe 4 pulsars analysed in [12], J0108-1431, J0953+0755,J0630-2834 and J1136+1551 of 9.8 × 10-3 eV and 3.29× 10-2 eV for axions of energy 100 MeV and 200 MeVrespectively.

Our determination of UL ma = 9.6 × 10-3 eV is a factorof 8 improvement on the result of [12] who determinedan UL ma of 7.9 × 10-2 eV.

Finally, we note that the UL ma obtained by likelihoodstacking is improved two-fold compared to the averagedresult above, with UL ma of 4.8 × 10-3 eV and 1.61 ×10-2 eV for axions of energy 100 MeV and 200 MeV re-spectively.

V.C. Pulsars Near Extended Emission

We note that the UL test sources for 5 pulsars are de-tected with a significance which exceeds 3 σ , namely

J0736-6304 5.7 σ (TS 33), J0630-2834 4.4 σ (TS 19),J2307+2225 3.7 σ (TS 14), J0709-5923 3.5 σ (TS 12) andJ0459-0210 3.2 σ (TS 10). However, the initial analysiswhich searches for point sources (whilst not introducing apulsar test source), detects no point sources at the pulsarco-ordinates and thus we discount these apparent detec-tions as true detections of the pulsars concerned. Thelack of significant point source pulsar detections can alsobe seen on TS maps for the analysis (Fig. 2) where thepulsars are spatially co-incident with regions of extendedgamma-ray emission uncharacteristic of the point sourceemission expected from a pulsar.

We also check for source extension of the pulsars byrunning the GTAnalysis extension method. extensionreplaces the pulsar point source spatial model with anazimuthally symmetric 2D Gaussian model. It then pro-files likelihood with respect to spatial extension in a 1 di-mensional scan to determine the likelihood of extension.Only the J0736-6304 test source has some evidence of ex-tension with an extension TS value of 14 (3.7 σ). Theremaining 4 pulsars with significance <4.4 σ are consis-tent with background and as expected have no significantextension.

We make the assumption that axion emission isisotropic and so the extended emission of J0736-6304which is asymmetric and exhibits its highest significanceoffset from the pulsar would seem to be inconsistent withan axion source. Instead, this emission is more likelyto be consistent with variations in the Galactic diffusegamma-ray background.

These 5 pulsars generally exhibit higher UL fluxes (Ta-ble III) than the other 12 (Table II) and so omittingthese 5 pulsars from the determination of UL ma yieldsan improved average UL ma for the 12 remaining pulsarsof 8.9 × 10-3 eV and 2.97 × 10-2 eV for axions of energy100 MeV and 200 MeV respectively.

VI. DISCUSSION

VI.A. Upper Limit Determination

The authors of [12] analysed 4 pulsars J0108-431,J0953+0755, J0630-2834 and J1136+1551 with an un-binned likelihood analysis using the 2FGL catalogue, 5years of Fermi -LAT pass 7 event data in the energy range60−200 MeV and employing front converting source pho-ton events. They detected no gamma-ray emission anddetermined a 95 percent confidence UL photon flux foreach of the 4 pulsars using the minos method of theFermi Science Tools. In contrast, we analyse 17 pulsars(including the 4 pulsars of [12]) with a binned likelihoodanalysis using the 3FGL catalogue and 9 years of Fermi -LAT pass 8 event data in the energy range 60−500 MeV,again using front converting events. We determine theUL photon flux using the fermipy flux ul95 entry for eachpulsar. Using this analysis we obtain UL photon fluxes(Table V) comparable to [12] for the 4 pulsars they con-sider, which serves as a useful check of our gamma-ray

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Constraining Axion Mass 6

Pulsar TS UL Photon Flux UL Energy Flux UL γ Luminosity UL ma ω=100 MeV UL ma ω=200 MeV(10-8 cm-2 s-1) (10-12 erg cm-2 s-1) (1031 erg s-1) (10-2 eV) (10-2 eV)

J0711-6830 3 0.04 1.51 0.22 0.21 0.70J0536-7543 0 0.22 0.53 0.12 0.43 1.45J0837+0610 0 0.27 0.63 0.27 0.57 1.90J0108-1431 0 0.18 0.41 0.21 0.52 1.75J0953+0755 2 0.47 1.32 1.07 0.84 2.81J1116-4122 1 0.90 1.73 1.62 1.09 3.66J0826+2637 2 0.39 1.18 1.44 0.91 3.04J1136+1551 0 0.50 1.16 1.70 1.04 3.49J0656-5449 0 0.32 0.75 1.23 0.94 3.14J0636-4549 3 1.31 2.08 3.60 1.52 5.08J0452-1759 0 0.31 0.71 1.36 0.97 3.24J0814+7429 0 0.23 0.54 1.19 0.93 3.10

Table II Test statistic, UL photon flux, UL energy flux, UL gamma luminosity and UL ma for axion energies of 100 and 200 MeV for the12 undetected pulsars.

Pulsar TS UL Photon Flux UL Energy Flux UL γ Luminosity UL ma ω=100 MeV UL ma ω=200 MeV(10-8 cm-2 s-1) (10-12 erg cm-2 s-1) (1031 erg s-1) (10-2 eV) (10-2 eV)

J0736-6304 33 2.68 4.87 0.58 0.79 2.65J0459-0210 10 1.72 3.64 1.11 0.93 3.13J0630-2834 19 1.89 3.59 4.40 1.53 5.12J0709-5923 12 1.03 2.55 4.17 1.38 4.62J2307+2225 14 1.12 2.87 8.25 1.71 5.72

Table III Test statistic, UL photon flux, UL energy flux, UL gamma luminosity and UL ma for axion energies of 100 and 200 MeV forthe 5 pulsars which are associated with areas of extended diffuse gamma-ray emission.

analysis method, and do not detect any pulsars in oursample.

Our method to determine UL ma differs from [12] inthat we use UL photon fluxes directly as input to Eqn. 8whilst they fit a model of the spectral energy distribution(SED) of differential flux to a stacked likelihood analysisof the 4 pulsars using the COMPOSITE2 module of theFermi science tools and take the UL normalisation of thismodel to be UL (ma /eV)5 from which they obtain ULma with all flux dependencies on astrophysical factorsbeing accounted for in the SED model.

We can use the UL photon fluxes obtained by [12] toconsider the improvement in UL ma determination whicharises from our UL ma calculation method alone. The av-erage UL ma for the 4 pulsars using the [12] photon fluxes(Table V) and our method (Eqn. 8) is 9.7 × 10-3 eV and3.25 × 10-2 eV for axions of energy 100 MeV and 200MeV, improving on the 7.9 × 10-2 eV determination of[12] by a factor of 2.4−8.1. Despite this improvement,we note that our determination of UL ma is conserva-tive because we assume that the integrated UL photonflux arises solely from a specific axion energy (100 MeVor 200 MeV) rather than the lower UL flux (and hencemore constraining) UL ma determination which would beexpected if we could determine UL photon flux for eachenergy bin in the analysis energy range of 60−500 MeV.

We determine a very similar UL ma in our sample of 17pulsars of 9.6 × 10-3 eV and 3.21 × 10-2 eV for axions ofenergy 100 MeV and 200 MeV respectively. These resultsare also comparable with UL ma values obtained by mod-elling the cooling of Cassiopeia A observed by Chandra.By assuming that the cooling results from both neutrinoand axion emission and that a state of superfluidity ex-

ists in the star, an UL ma of (1.7 − 4.8) × 10-2 eV isobtained for CN = ( 0.14 − -0.05 )[48].

As a final check to test whether the SED differentialflux model used by [12] can be fitted individually to anyof our 17 pulsars, we add a test source with the SEDdifferential flux model from [12] implemented using theFileFunction spectral model (Eqn. 13) with flux valuesas Table IV and re-analyse as Section IV above. All17 pulsars remain undetected with the differential fluxmodel test source exhibiting a consistent normalisationof 10 -5 for all pulsars which is equivalent to ma <0.1 eV.

dN

dE= N0

(dNdE

)∣∣∣∣file

(13)

VI.B. The Effect of Pulsar Core Temperature

The emission rate for axions is strongly dependent onpulsar core temperature, Tc, being proportional to Tc

6

[17]. We therefore re-examine the applicable value of Tc

for modeling axion emission and the effect of loweringTc on that emission. The authors of [12] select Tc=20MeV on the basis of the range temperatures applicable toequation of state (EOS) simulations of pulsar degeneratematter [49–51], slower neutron star cooling due to super-fluidity [52 and 53] and surface temperature observationsof the pulsar J0953+0755 [54].

We now consider to what extent the works cited aboveexplicitly support the choice of Tc=20 MeV. In EOSmodeling both [49] and [50] use Tc as a free model pa-rameter (in the range 0−60 MeV and 0−15 MeV respec-tively) for the construction of phase diagrams but thisdoes not indicate a preferential value for Tc. In [51], a

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Constraining Axion Mass 7

Fig. 2 TS maps for our gamma-ray analysis of the 5 pulsar test sources detected at >3 σ significance (Table III) showing that these sourcesare inconsistent with a point source detection characteristic of pulsars and part of extended diffuse features. The horizontal contour scaleis the TS value, the red diamond is the pulsar position, horizontal axis is RA in decimal degrees, vertical axis is Dec in decimal degrees.

Energy Differential FluxMeV cm-2 s-1 MeV-1

50 2 × 10 -3

60 8 × 10 -4

70 4 × 10 -4

80 1 × 10 -4

90 6 × 10 -5

100 2 × 10 -5

200 1 × 10 -11

Table IV Definition of the FileFunction spectral model with differential flux at a given energy

specific Fermi temperature of TF of 20 MeV per nucleonis supported but no preferred value of Tc is indicated.The cooling of quark hybrid (QH) stars (a special caseof a higher density neutron star where quarks experi-ence deconfinement from nucleons) is considered in [52]

with QH stars in fact cooling more quickly than hadronneutron stars unless a colour flavour locked (CFL) quarkphase with a higher CFL gap parameter of 1 MeV is con-sidered. However, by 105 yr all modelled QH stars againexhibit greater cooling then hadron neutron stars. As

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Constraining Axion Mass 8

all neutron stars in our pulsar sample have age >105 yr(Table I), this QH star slow cooling regime will not re-sult in a higher value for Tc in our sample than mightbe expected from normal cooling processes. The discus-sion of crustal heating arising from super fluidity in neu-tron stars also refutes Tc=20 MeV, with one neutron starJ0953+0755 (PSR 0950+08) analysed in [12] having aninternal temperature of between 0.09 keV and 0.11 keV[53]. Although there is more recent evidence of internalheating of J0953+0755 from far UV HST observations(surface temperature (ST) = (1−3) × 105 K [55] vs 7 ×104 K of [54]), this would still only result in a maximumTc of 1.34 keV assuming Tc=12 × (ST/106 K)1.82 keV[53 and 56].

The authors of [57] have modelled the cooling of neu-tron stars using a fully general relativistic stellar evolu-tion code, without exotic cooling, allowing for inputs forequations of state and uncertainties in superfluidity alongwith a finite time scale of thermal conduction. They de-termine Tc to be initially 3.98 × 109 K (343 keV) whenthe neutron star is 9 hours old, decreasing to 1.99 × 109

K (171 keV) at 1 yr, 6.31 × 108 K (54 keV) at 1000 yrand 1.99 × 108 K (17 keV)) at 105 yr. This cooling trendagrees well with the modelling of pulsar cooling in [58]where the highest pulsar surface temperatures (in all sce-narios) of 3.98 × 106 K at 1 yr and 1.99 × 106 K at 105

yr yield a Tc of 148 keV and 12 keV respectively usingthe ST to Tc conversion above. It should also be notedthat Chandra observations of the very young pulsar CasA (age ≈ 330 yr), yield an ST of 2.04 × 106 K [59] equiv-alent to Tc = 43.9 keV using the ST to Tc conversionabove. Similarly, in their modeling of Cas A cooling us-ing the observations of [59], the author of [48] determinesthe Tc of Cas A to be 7.2 × 108 K, equivalent to 62 keV.

We therefore consider Tc=20 MeV to be a high tem-perature choice more consistent with the neutron starcore just after the supernova event. In [60], EOS andhydrodynamic modeling is performed in the first secondafter the supernova core bounce and proto neutron star(PNS) creation. Here, at 150 ms post bounce, Tc can be14 MeV at the core, falling to 10 MeV at a radius of 10km, before rising to a peak of 32 MeV at radius 12 km.Other modeling work demonstrates that a peak PNS Tc

of 30 to 43 MeV is possible, falling to 5 to 18 MeV within50 s [61] due to efficient cooling by neutrino emission. Avery short time later, at 120 s, the PNS Tc is 2.2 MeV[62]. This suggests that plausible values of Tc are muchless than 20 MeV with Tc=1 MeV being achieved withinseconds [63].

We re-evaluate ω4Sσ(ω), on which the axion emissivitydepends (Eqn. 5), for Tc <20 MeV. We use the analyticsimplification for the phase space integral for Sσ(ω) from[16] and perform a 5 dimensional numeric Monte Carlointegration as described in the Appendix . In order tocheck our method we first reproduce the ω4Sσ(ω) plotfrom [12] using a Tc of 10−50 MeV, µ/Tc = 9−11 andpFn = 300 MeV (Fig. 3).

We reproduce the essential features of the [12] plotboth in magnitude and in the following respects:

• Increasing the value of µ/Tc for fixed Tc=20 MeVdecreases amplitude of ω4Sσ(ω)

• ω4Sσ(ω) for Tc=10 MeV cuts-off at a lower valueof ω=100 MeV than for Tc=20 MeV

• The Tc=50 MeV case has lower values of ω4Sσ(ω)than the Tc=20 MeV case, with ω4Sσ(ω) remainingbroadly flat across higher ω values of 100−300 MeVwith no pronounced cut-off at 200−300 MeV

• The value of ω4Sσ(ω) spans one order of magnitudefor the 20 MeV case and varying µ/Tc = 9−11

We then evaluate ω4Sσ(ω), in a lower temperatureregime, for pFn = 300 MeV, µ/Tc = 10 and considerlower pulsar core temperatures with Tc = 1−20 MeV(Fig. 4). Lowering Tc from 20 MeV to a plausible PNStemperature of 4 MeV reduces axion emissivity and hencegamma-ray emission by a factor of 108 for axions of en-ergy ω=100 MeV. It therefore seems implausible thatthere would be detectable gamma-ray emission to allowthe determination of ma using the astrophysical model ofgamma-ray emission from [12] (Eqn. 6), for realistic pul-sar core temperatures. We note however that this modelis based on a quite conservative assumption that gamma-ray emission arises solely from axion radiative decay asopposed to axion to gamma-ray photon conversion in theB field of the pulsar. It is therefore possible that an alter-native model allowing axion to photon conversion couldproduce detectable gamma-ray emission.

The probable lack of detectable gamma-ray emissionin the lower temperature regime leads us to derive valuesfor UL ma from an alternative model (Eqn. 11) based onthe axion power equation which defines an energy lossrate due to axion production in the pulsar core (Eqn. 9).Using the UL gamma-ray luminosity (Table II) we de-termine UL ma from Eqn. 11 whilst varying Tc and theprobability of axion to photon conversion in the pulsarB field. On Fig. 5 we show the range of UL ma valuesthat we obtain. We see that the conversion of axionsto gamma-ray photons via radiative decay results in thehighest UL ma (67.5 eV at 0.1 MeV, 9.4 eV at 1 MeVand 0.7 eV at 20 MeV, points A, B and C respectively)which is above the classic ma search range of 10-2−10-6

eV. Similarly by varying the axion to photon conversionprobability from 0.001 to 1.0 (total conversion), we onlyobtain an UL ma above the lower search bound of 10-6

eV for Tc <0.1 MeV independent of the degree of axionto photon conversion or Tc <0.4 MeV assuming a prob-ability of ≤ 0.001 for axion to photon conversion (PointsE and F of Fig. 5 respectively). At Tc=1 keV the lowestUL ma obtainable would be 3.0 eV assuming total con-version of axions to photons (Point D of Fig. 5). We donot offer a view on the degree of axion to photon con-version in the pulsar B field but simply present a rangeof conversion alternatives to give indicative values of theUL ma.

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Constraining Axion Mass 9

The determination of a plausible and precise UL ma

from this alternative model thus requires both realisticlower values of Tc and a knowledge of the precise ex-tent of the axion to photon conversion in the pulsar Bfield. We have dealt with the value of Tc in the PNSand old pulsar cases above; however, whilst [12] considerthere to be no axion to photon conversion in the pulsar Bfield (using vacuum bi-refringence arguments) there is noconsensus on the extent of axion to gamma-ray photonconversion in pulsar B fields. More attention has beenpaid to axion to X-ray photon inter-conversion in pulsars[64] and in axion like particle (ALP) to X-ray conversionin the higher B field (20 × 1014 G) of magnetars by [65].[65] finds Pa→ γ=0.225 for ω = 3 keV (the peak emission)and Pa→ γ = 0.025 for ω = 200 keV when Tc=50−250keV. The lower B field of our sample notwithstanding(average B=2.78 × 1012 G) such values of Pa→ γ and Tc

could yield constraints on ma in the classic axion searchrange using the alternative model (Fig. 5).

Finally, the normalized axion energy spectrum dNa/dωpeaks at ω/Tc = 2 [19]. This implies that the pho-ton energy spectrum would peak at energy Tc. There-fore for the values of Tc discussed above, in the 1 MeVrange or below, the determination of an UL for unpulsedgamma-ray emission in our pulsar sample or preferablyyounger pulsars with a potentially higher Tc, by futurelow-energy gamma-ray observatories such as the All-SkyMedium Energy Gamma-ray observatory (AMEGO) ore-ASTROGAM, with greater sensitivity then any currentobservatory in the 0.2−10 MeV band [66, 67] may allowan improved determination on the UL ma presented inthis work.

VII. CONCLUSIONS

We analyze data from 17 nearby pulsars using 9 yearsof Fermi -LAT data and detect none. Using the UL pho-ton flux and the astrophysical model of [12] which as-sumes a pulsar core temperature of 20 MeV we deter-mine an improved UL axion mass (ma) of 0.96 and 3.21× 10-2 eV for axions of energy 100 MeV and 200 MeV re-spectively. However, we show that at realistic pulsar coretemperatures of <4 MeV, axion emissivity is so reducedthat is unlikely a reasonable determination of UL ma canbe made with this method. An alternative axion energyloss rate model yields a plausible range of UL ma valuesassuming low pulsar core temperatures but requires boththe core temperature and the axion to photon conversionprobability to be known to set a useful limit. Observationof the un-pulsed gamma-ray emission of our selected pul-sar sample with future medium energy gamma-ray obser-vatories such as AMEGO and e-ASTROGAM may allowa better determination of UL ma.

ACKNOWLEDGEMENTS

We acknowledge the excellent data and analysis toolsprovided by the Fermi -LAT collaboration. AMB and

PMC acknowledge the financial support of the UKScience and Technology Facilities Council consolidatedgrant ST/P000541/1. This research has made use of theSIMBAD database, operated at CDS, Strasbourg, France(68). Finally we thank the anonymous referee for theirreview and very useful comments which improved thispaper.

Appendix: NUCLEON PHASE SPACEINTEGRATION

The spin structure function of Eqn. 2 has an analyticsimplification as presented by [16] of which we repeat therelevant points here. From the original 12-dimensionalintegral, 7 dimensions may be integrated out analyti-cally so that a 5-dimensional integral remains to be solvedthrough numerical integration (as opposed to numericalintegration of the 4-dimensional integral of [16]).

Firstly the 3-dimensional momentum delta function isused to integrate out d3p4. Then, the non-relativisticnucleons have energy Ei = p2i /2MN and so the energybalance term c

E1 + E2 − E3 − E4 + ω

=−2p23 − 2p1 · p2 + 2p1 · p3 + 2p2 · p3

2MN+ ω (A.1)

Next, a polar co-ordinate system is used with α andβ being the polar and azimuthmal angles of p2 relativeto p1 and θ and Φ those of p3. The medium is isotropicso the p1 momentum can be chosen in the z directionso∫d3p1 = 4π

∫dp1 with p1 = |p1|. The medium iso-

totropy also allows the azimuthmal angle dΦ to be triv-ially integrated to leave three nontrivial angular integra-tions with the remaining angular variables expressed asfollows:

p1 · p2 = p1p2 cos α (A.2)

p1 · p3 = p1p3 cos θ (A.3)

p2 · p3 = p2p3 cos α cos θ + sin α+ sin θ + cos β

(A.4)

The integration over dβ is carried out using the δ func-tion with f(β) ≡ E1 + E2 − E3 − E4 + ω and β1 beingthe root of f(β) = 0 in the interval [0,π] giving:

∫ 2π

0

dβ δ[f(β)] =2

|df(β)/dβ|β=β1

Θ(∣∣∣df(β)

∣∣∣2β=β1

)(A.5)

The derivative can be expressed as

∣∣∣df(β)

∣∣∣β=β1

=√az2 + bz + c (A.6)

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Constraining Axion Mass 10

Fig. 3 The energy dependence of axion emissivity ω4Sσ(ω) on axion energy ω for varying pulsar core temperature Tc and µ/Tc derivedby Monte Carlo numerical integration of an analytic simplification of Sσ(ω).

Fig. 4 The energy dependence of axion emissivity ω4Sσ(ω) on axion energy ω for Tc = 1-20 MeV and µ/Tc =10 derived by Monte Carlonumerical integration of an analytic simplification of Sσ(ω). Reducing Tc from 20 MeV to 4 MeV lowers emissivity by a factor of 108 atω=100 MeV.

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Constraining Axion Mass 11

Fig. 5 Plot of axion mass with respect to Tc using an alternative energy loss rate model and varying axion to photon conversionprobabilities from 0.001 to 1.00. Also shown is the more conservative axion radiative decay case (top). At realistic values of Tc of 0.1 and1 MeV, radiative decay alone yields unrealistic values for UL ma of 67.5 eV and 9.4 eV respectively (labelled A and B). At an unrealistichigh value of 20 MeV for Tc the UL ma is 0.7 eV (Labelled C) . At Tc=1 keV, UL ma is 3.0 eV, assuming total axion to photon conversion(labelled D). To keep UL ma>10-6 eV, which is the classic axion search lower bound, requires Tc <0.1 MeV (labelled E) or Tc <0.4 MeVwith a low axion to photon conversion probability of 0.001 (labelled F).

Pulsar UL Photon Flux (60-200 MeV) UL Photon Flux (60-500 MeV) UL ma ω=100 MeV UL ma ω=200 MeV(From [12]) This analysis (10-2 eV) (10-2 eV)

(10-9 cm-2 s-1) (10-9 cm-2 s-1)J0108-1431 4.03 1.75 0.69 2.31J0953+0755 7.40 4.75 0.97 3.26J0630-2834 4.82 18.90 0.97 3.25J1136+1551 8.52 5.01 1.25 4.17

Table V The UL photon flux for 4 pulsars from [12] (60-200 MeV) compared to our analysis (60-500 MeV) and UL ma which we derivefrom [12] fluxes for axions of energy 100 MeV and 200 MeV using Eqn. 8.

where

z ≡ cos α (A.7)

a = p22(−p21 − p23 + 2p1p3cosθ) (A.8)

b = 2ωMNp1p2 − 2p1p2p23 − 2ωMNp2p3cosθ

+2p21p3cosθ + 2p2p33cosθ − 2p1p2p

23cos

2θ(A.9)

c = ω2M2N + 2ωMNp

23 + p22p

23 − p43 − 2ωMNp1p3cosθ

+2p1p33cosθ − p21p23cos2θ − p22p33cos2θ

(A.10)

Finally the analytic simplification of equation A.5 canbe solved by numerical integration through a MonteCarlo method integrating over dp1dp2dp3d cos θ d cos α.

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Constraining Axion Mass 12

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