1. Introduction
The Fornax dwarf spheroidal galaxy (dSph) has a remarkably high fraction of stellar mass locked in its globular clusters (GCs) system, thus putting at stake some GC formation models. It has been conjectured that an even larger fraction of stellar mass has been lost via tidal stripping.
Aiming at constraining the amount of (stellar) mass lost by Fornax in Di Cintio et al. (Reference Di Cintio, Iorio, Calura, Nipoti and Cantari2024), using high resolution
$N-$
body simulations combined with an a-posteriori mass component (stellar or dark matter) assignment scheme, we evolved the progenitor of the Fornax dSph along two Gaia DR3-based orbits in a static Milky Way (MW) potential. The core result of this work is that, even though, in principle, a broad range of initial stellar mass distributions for Fornax would be consistent with the present observed stellar density profile, the stellar mass loss must have been in all cases rather low (i.e. of the order of
$\lesssim 3\%$
). As a consequence, it appears rather unlikely that the mass loss only could explain the high fraction of stellar mass associated to Fornax’s GCs system. Therefore the relative amount of field and GC stars remains a puzzle (despite the significant uncertainty in the adopted GC mass-to-light ratio) for GC formation channels that assume originally much more massive progenitors.
2. Methods and models
In line with Di Cintio et al. (Reference Di Cintio, Iorio, Calura, Nipoti and Cantari2024) here we assume the Johnston et al. (Reference Johnston, Spergel and Hernquist1995) MW model consisting of three components (disk, bulge and halo) with total gravitational potential
$\Phi_{\rm MW,tot}(R,z)=\Phi_{\text{disk}}+\Phi_{\text{bulge}}+\Phi_{\text{halo}}$
composed of a Miyamoto and Nagai (Reference Miyamoto and Nagai1975) disk
\begin{equation} \Phi_{\text{disk}}(R,z)= -\frac{GM_{\text{disk}}}{\sqrt{R^2 + \big(a+\sqrt{z^2 + b^2}\big)^{2}}} \end{equation}
and a spherical Hernquist (Reference Hernquist1990) bulge
embedded in a spherical Binney (Reference Binney1981) logarithmic halo
In the equations above
$R=\sqrt{x^2+y^2}$
and z are Galactocentric cylindrical coordinates, and
$r_{\rm G}=\sqrt{R^2+z^2}$
is the Galactocentric distance, with
$a=6.5$
kpc,
$b=0.26$
kpc,
$c=0.7$
kpc,
$d=12$
kpc,
$M_{\text{bulge}}=3.4\times 10^{10}\text{ M}_{\odot}$
,
$M_{\text{disk}}=10^{11}\text{ M}_{\odot}$
and
$v_{\text{halo}}=128$
km/s.
To include the effect of Chandrasekhar (Reference Chandrasekhar1943) DF on the orbit of the Fornax dSph, here we perform single particle integrations, where a test mass
$M_{\rm tot}$
orbits in the MW potential according to the equations of motion
augmented by the deceleration produced by DF through
\begin{equation}\mathbf{a}_{\rm DF}=-2\pi G^2 M_{\rm tot}\rho(\mathbf{r})\ln(1+\Lambda^2)\Bigg[{\rm erf}(X)-\frac{2X^2}{\sqrt{\pi}}\exp(-X^2)\Bigg]\frac{\mathbf{v}}{v^3}.\end{equation}
In the equation above
$\rho(\mathbf{r})$
is the total MW mass density at
$\mathbf{r}$
,
$\mathbf{v}=\dot{\mathbf{r}}$
and
$X=v/(\sqrt{2}\sigma)$
, where
$\sigma(\mathbf{r})$
is the velocity dispersion at
${\mathbf{r}}$
(i.e. we assume a local Maxwellian approximation ignoring the MW velocity distribution function) as obtained by solving the Jeans equations for the MW potential and density (e.g. see Dehnen et al. Reference Dehnen, McLaughlin and Sachania2006). In Equation (5), in order to take into account that the satellite is extended (e.g. see Petts et al. Reference Petts, Read and Gualandris2016), we define the ratio
$\Lambda$
entering the Coulomb logarithm as
where
$r_{\rm G}$
and
$r_{\rm sat}$
are the scale radii of the Galaxy and the satellite, which we fix to 12 and 4.3 kpc, respectively.
$N-$
body simulations performed in a static MW potential revealed that the mass loss rate experienced by the Fornax progenitor over 12 Gyr is nearly constant in time for a broad range of putative orbits. In Fig. 1 we show the evolution of the mass within a fixed radius of 3 kpc around the centre of Fornax for the orbits O1 and O2 discussed in Di Cintio et al. (Reference Di Cintio, Iorio, Calura, Nipoti and Cantari2024). The dotted lines mark the best linear fits with the relation
yielding the two mass loss rates
$\dot{M}\approx3.4\times 10^{-3}$
and
$1.1\times 10^{-2}[10^{10}M_{\odot}{\rm Gyr}^{-1}]$
.
Evolution of the mass within a control radius of 3 kpc for two different
$N-$
body simulations of the Fornax dSph in a smooth MW potential (coloured solid lines) and their linear fit (black dotted lines).

3. Numerical simulations and discussion
We integrated backward in time from
$t=12$
Gyr to
$t=0$
via Eq. (4) the orbit of a single particle representing Fornax using a modified leapfrog scheme (Mikkola and Merritt Reference Mikkola and Merritt2006) starting from the same two estimates of the present day phase-space coordinates used in our
$N-$
body simulations, with and without mass loss. In both cases we start by assuming
$M_{\rm tot}=5.7\times 10^9M_{\odot}$
at
$t=12$
Gyr, that is, the present-day total mass of Fornax as estimated in our
$N-$
body simulations. Additionally, we have also propagated from the same sets of coordinates a particle of constant mass
$M_{\rm tot}=1.13\times 10^{10}{\rm M}_\odot$
, corresponding to the heaviest Fornax progenitor used in our
$N-$
body study. Figure 2 shows the Galactocentric distance
$r_{\rm G}$
as a function of time for the two choices of present day coordinates and the different simulation set-ups. It appears evident that allows the mass to vary in time (purple lines, note that in backward integrations
$M_{\rm tot}$
increases), in both simulations partially compensating the effect of DF, in particular with respect to the fixed mass runs with an overestimated present day mass (indicated by the blue dashed lines), thus implying a much lower apogalactic distance for the Fornax progenitor.
Evolution of the Galactocentric distance
$r_G$
of the Fornax dSph for two different models. The blue and cyan dashed lines refer to fixed mass single particle integrations with an artificially overestimated and a realistic present-day Fornax mass, respectively
$1.13\times 10^{10}{\rm M}_\odot$
and
$5.7\times 10^{9}{\rm M}_\odot$
. The purple solid lines refer to backward in time propagation where the mass loss has been accounted for. As a reference, the heavy black line marks the orbits propagated in the frozen MW potential without DF, and the yellow dots correspond to
$N-$
body simulations in the same frozen potential. Here
$t=12$
Gyr is today.

For comparison, we have also reported the evolution of
$r_{\rm G}$
in the
$N-$
body simulations (yellow dotted curves) where MW DF was not implemented. Remarkably, since the interplay between mass loss (nearly 10% for O1 and 40% for O2) and DF results in a much milder orbital decay, we obtained further confirmation that our
$N-$
body simulations neglecting the DF exerted by the Galaxy can be safely taken as a reasonable model of Fornax evolution along a family of Gaia-based reference orbits. We note that, as shown in Miller et al. (Reference Miller, van den Bosch, Green and Ogiya2020), under certain conditions the mass loss can sometimes enhance the orbital decay of a satellite system with respect to the simple point-particle with constant mass approximation. This is the case when extended tidal tails exert an additional torque on the satellite’s orbit inducing the dissipation of orbital kinetic energy. This so-called tidal self-friction is therefore partially compensating the mitigation of the standard DF caused by mass loss. However, for the specific choices of initial conditions used in Di Cintio et al. (Reference Di Cintio, Iorio, Calura, Nipoti and Cantari2024), the tidal self-friction appears to be rather mild as no appreciable decay of the pergalactic distance was detected. In order to disentangle the effect of mass stripping and host galaxy DF one should in principle run
$N-$
body simulations in a galactic model incorporating DF, in a similar fashion to what has been carried out in Giunchi et al. (Reference Giunchi, Marinacci, Nipoti, Claeyssens, Pascale, Calura and Ragagnin2025), where the sinking stellar system suffers the drag exerted by the host system on its center of mass. A numerical study of the strength of the DF force as a function of the satellite size and (possibly time dependent) mass is currently underway.



N−
rG
1.13×1010M⊙
5.7×109M⊙
N−
t=12