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A synchronous moon as a possible cause
of Mars’ initial triaxiality  
 

Michael Efroimsky
US Naval Observatory, Washington DC 20392
michael.efroimsky @ gmail.com
Abstract

The paper addresses the possibility of a young Mars having had a massive moon, which synchronised the rotation of Mars, and gave Mars an initial asymmetric triaxiality to be later boosted by geological processes. It turns out that a moon of less than a third of the lunar mass was capable of producing a sufficient initial triaxiality. The asymmetry of the initial tidal shape of the equator depends on timing: the initial asymmetry is much stronger if the synchronous moon shows up already at the magma-ocean stage. From the moment of synchronisation of Mars’ rotation with the moon’s orbital motion, and until the moon was eliminated (as one possibility, by an impact in the beginning of the LHB), the moon was sustaining an early value of Mars’ rotation rate.

1 Motivation.
The equatorial ellipticity of Mars

Mars’ triaxiality makes itself most evident through the equatorial ellipticity produced by the Tharsis Rise and by a less prominent elevation located almost diametrically opposite to Tharsis and constituted by Syrtis Major Planum and an adjacent part of Terra Sabaea (Smith and Zuber, 1996) .

Terra Sabatea being more ancient, Syrtis Major’s present form is dated by crater counts to the early Hesperian epoch (Hiesinger and Head, 2004), and is a smoothly sloping shield-volcano dome of an average 2.12.1 km height, its peak extending to 2.3 km.

The largest highlands province on Mars and in the solar system, Tharsis is rising, in average, to about 77 km, excluding the much higher volcanoes. Its formation had begun at least in the Noachian period, and continued through the entire Hesperian, the volcanoes staying active into the Amazonian epoch. As was pointed out by Zuber and Smith (1997), this rise may mask or modify gravitational signatures that contain important information on the Martian gravitational field as a whole. For this reason, those authors produced a “Mars without Tharsis” gravitational field, by subtracting the gravitational signature of Tharsis from the full field of the planet. Even then, Mars retained much of its triaxiality.

To explain the origin of this shape, we propose a hypothesis consisting of two items:

  • (a)

    An initial, ‘seed’ triaxiality was created by a massive moon orbiting a young and still plastic Mars on a synchronous orbit. Showing the same face to the moon, Mars assumed a shape close but not identical to a triaxial ellipsoid, its longest axis aligned with the moon. While a symmetrical ellipsoidal part of the shape was created by the quadrupole component of the tide, a weaker, antisymmetrical perturbation was added to the shape by the octupole component, see Figure 1.

  • (b)

    After the moon produced the seed triaxiality and asymmetry of Mars, the tidally elevated provinces became, more than others, prone to convection-generated uplifts and tectonic and volcanic activity. These processes began to gradually add to the equatorial ellipticity. Owing to the degree-3 initial asymmetry of the shape, they were not acting in a symmetrical way; hence the resulting height disparity between Tharsis and Syrtis Major.

In this paper, we address item (a) and demonstrate that a synchronous moon of less than a third of the lunar mass was capable of providing a seed triaxiality. The seed asymmetry of the equator was considerable if the synchronous moon existed already at the magma-ocean epoch, and was weaker if the moon showed up at the solidification stage.

Refer to caption
Figure 1: Mars deformed by its putative moon Nerio. The blue line depicts a spherical Mars. In an exaggerated way, the green line shows a symmetric, quadrupole deformation. The red line shows a combined quadrupole and octupole distortion.

Checking on item (b) requires quite a programme of research, but a qualitative argument in support of this item is available readily for a moon whose orbit is synchronous but not circular. A finite eccentricity causes the tidal deformation to oscillate and produce heat, because an elliptic synchronous orbit makes the moon’s position appear to oscillate E-W in the sky over the same region (or to describe an analemma if the inclination is nonzero). The submoon and antimoon zones might have been warmer than the rest of the surface — though this outcome is very structure-dependent and is not warranted (Segatz et al., 1988). Modeling of a young Kelvin-Voigt Moon has demonstrated that the closer the Moon was to the Earth the higher the ratio of near to farside tidal heat flux, the difference being in the dozens of percent (Quillen et al., 2019, Figure 6). This motivates us to extend this observation to Mars, and to expect that the degree-3 tide made the submoon zone warmer than the antimoon zone, with the possibility of a plume emerging in the submoon zone, as Tharsis’ predecessor. It should be added, though, that the cited model contains also an argument against our hypothesis, an increase of the heat flux toward the polar zones — which poses a question why the volcanic activity near the poles was lower than on Tharsis. To answer this question, accurate modeling based on a more realistic rheology is required.

As per advice from Benoît Noyelles, who kindly reviewed this paper and contributed greatly to its improvement, we christen the hypothetical moon Nerio, after a war goddess who was Mars’ partner in ancient cult practices, later to be supplanted by deities adapted from other religions.

2 Whence had it come, whither gone?

2.1 Origin

Aside from the obvious possibility of in situ formation, the putative moon may as well had been captured in the remnants of the protoplanetary disk (or in a later debris disk, if it existed) and was then slowed down by friction, and eventually synchronised by tides. For example, Hunten (1979) demonstrated that while slowly-rotating condensation in the solar nebula is unlikely to capture a moon, the odds are greatly improved if the atmosphere is rapidly rotating. However, given the relatively short life spans of these disks, more probable option is a megaimpact. Had the impact happened during the magma-ocean stage, it would hardly have influenced the subsequent development of Mars’ global structure. On the other hand, had it happened during the formation of crust, it may have, speculatively, left some signature — whence the question arises whether that impact could be the one responsible for the north-south hemispherical dichotomy, a theme beyond the scope of our study.

As we shall see shortly, a moon of less than a third of the lunar mass was sufficient to produce the required initial triaxiality. Creation of such a moon by a collision of an impactor with an Earth-sized planet would not be a problem. Mars, however, is more than nine times less massive than the Earth, which reduces the probability of generation of the needed moon via impact. This obstacle can be sidestepped. As was shown by Rufu et al. (2017), our Moon could have been created by a succession of smaller collisions. Each such collision resulted in a debris disk accreting to produce a moonlet. The moonlets tidally receded outward and coalesced into the Moon. This mechanism should be applicable to any terrestrial planet, including Mars.

One more mechanism of acquisition of a massive satellite is binary-exchange capture. Originally developed for giant planets (Agnor and Hamilton, 2006), it was recently applied to terrestrial planets. It turned out that smaller planets capture satellites more efficiently because of the slower encounter velocities in their weaker gravity wells (Williams and Zugger, 2024).

Whatever its origin, we assume that the moon Nerio was synchronised sufficiently early, when Mars was not completely rigid — that is to say, either during the magma-ocean stage or during the subsequent period of solidification while the lithosphere was still weak (Daradich et al., 2008). Also, it was not necessary for the moon to have been born or captured exactly at the then synchronous radius. Sufficient would have been its emergence in some vicinity of the synchronous orbit — whereafter the tidal forces would have done the rest. For a molten or semimolten planet, the value of k2/Qk_{2}/Q could have been of order 0.030.03 to 0.60.6. [ See equation (38) in Appendix A, and mind that the QQ of such a planet can reside anywhere between 2\simeq 2 to 10\simeq 10\nobreak\hskip 1.1pt\nobreak. For an extended explanation, see Appendix B. ] So tidal dissipation in the planet was two to three orders of magnitude higher than presently. Had Nerio begun its life slightly above (below) synchronism, it would have quickly synchronised Mars’ rotation while tidally receding (descending). Both options are described by the same equation following from the angular momentum conservation law (Makarov and Efroimsky, 2023).

2.2 Disposal

As one possibility, Nerio could have been destroyed by the Late Heavy Bombardment (LHB) — in which case Phobos and Deimos may be this moon’s remnants or, more likely, the remnants of a larger fragment eliminated by a later event (Bagheri et al., 2021).

A potential restriction on the timing of LHB-caused disposal is that the destruction event ought to have happened early in the LHB, to enable the subsequent LHB to smoothen the latitudinal dependence of the resulting crater distribution. The ancient crater population seen in the southern highlands and in the Quasi-Circular Depressions in the north (buried impact basins) shows no such latitudinal dependence. So the downfall of Nerio’s remnants should have predated those provinces’ formation which coincided in time with the LHB. We are grateful to Andrew Dombard for drawing our attention to this circumstance.

3 Formulae

Consider a static configuration comprising two mutually synchronised bodies: a planet of mass MM and radius RR\nobreak\hskip 1.1pt\nobreak, and a moon of mass MM^{\,\prime}. Aiming at crude estimates, we set the eccentricity zero, so the semimajor axis coincides with the distance rr between the centres of mass of the partners. This enables us to employ a simple formalism developed for static tides with no lag.

Table 1:     Symbol key
Variable        Value Explanation Reference
GG 6.67430×10116.67430\times 10^{-11} m3kg  s2\frac{\mbox{m}^{\nobreak\hskip 0.55pt\nobreak 3}}{\mbox{kg~{}\nobreak\hskip 0.77pt\nobreak s}^{\nobreak\hskip 0.55pt\nobreak 2}} gravitational constant Tiesinga et al. (2021)
MM early Mars’ mass
RR early Mars’ mean radius
M(present)M^{\,(present)} 6.4169×10236.4169\times 10^{23} kg present Mars’ mass Konopliv et al. (2016)
R(present)R^{\,(present)} 3.3895×1063.3895\times 10^{6} m present Mars’ mean radius Seidelmann and Urban (2013)
MM^{\,\prime} Nerio’s mass
RR^{\,\prime} Nerio’s mean radius
k2,h2,k3,h3k_{2},\nobreak\hskip 1.1pt\nobreak h_{2},\nobreak\hskip 1.1pt\nobreak k_{3},\nobreak\hskip 1.1pt\nobreak h_{3} early Mars’ Love numbers
QQ early Mars’ quality factor
K2k2QK_{2}\nobreak\hskip 1.1pt\nobreak\equiv\;\frac{\textstyle k_{2}}{\textstyle Q} early Mars’ quality function
k2k_{2}^{\,\prime} Nerio’s Love number
QQ^{\,\prime} Nerio’s quality factor
K2k2QK_{2}^{\,\prime}\nobreak\hskip 1.1pt\nobreak\equiv\;\frac{\textstyle k_{2}^{\,\prime}}{\textstyle Q^{\,\prime}} Nerio’s quality function
rr early Mars’ synchronous radius Equation (8)
rHr^{\,\prime}_{H} early Mars’ reduced Hill radius Makarov and Efroimsky (2023)
rRr_{R} early Mars’ Roche radius Equation (28)
θ˙\dot{\theta} Mars’ rotation rate
Ω\Omega the synchronous value of θ˙\dot{\theta}
θ˙\dot{\theta}^{\,\prime} Nerio’s rotation rate
aa Nerio’s semimajor axis
nn Nerio’s mean motion
A<B<CA<B<C early Mars’ moments of inertia
J2J_{2} early Mars’ oblateness Equation (10)
J2(present)J_{2}^{(present)} 1.9566×1031.9566\times 10^{-3} present Mars’ oblateness Konopliv et al. (2011)
J22J_{22} early Mars’ triaxiality Equation (17)
J22(present)J_{22}^{(present)} 6.3106×1056.3106\times 10^{-5} present Mars’ triaxiality Konopliv et al. (2020, Tab S4)
H2H_{2} quadrupole tidal elevation
H3H_{3} octupole tidal elevation

Let 𝐫\bf r and 𝐑\bf R be planetocentric vectors pointing, correspondingly, at the moon and at some surface point of the planet. In this surface point, the moon-generated perturbing potential is

W(𝐑,𝐫)=l=2Wl(𝐑,𝐫)=GMrl=2(Rr)lPl(cosγ),\displaystyle W({\bf R},\,{\bf r})\,=\,\sum_{l=2}^{\infty}W_{l}({\bf R},\,{\bf r})\,=\;-\;\frac{G\,M^{\,\prime}}{r}\,\sum_{l=2}^{\infty}\left(\frac{R}{r}\right)^{l}P_{l}(\cos\gamma)\,\;, (1)

γ\gamma being the angular separation between 𝐑\bf R and 𝐫\bf r, and Pl(cosγ)P_{l}(\cos\gamma) being the Legendre polynomials. Specifically,

P2(cosγ)=12(3cos2γ1),P3(cosγ)=12(5cos3γ3cosγ).\displaystyle P_{2}(\cos\gamma)\nobreak\hskip 1.1pt\nobreak=\nobreak\hskip 1.1pt\nobreak\frac{\textstyle 1}{\textstyle 2}\nobreak\hskip 1.1pt\nobreak(3\nobreak\hskip 1.1pt\nobreak\cos^{2}\gamma-1)\,\;,\quad P_{3}(\cos\gamma)\nobreak\hskip 1.1pt\nobreak=\nobreak\hskip 1.1pt\nobreak\frac{\textstyle 1}{\textstyle 2}\nobreak\hskip 1.1pt\nobreak(5\nobreak\hskip 1.1pt\nobreak\cos^{3}\gamma-3\nobreak\hskip 1.1pt\nobreak\cos\gamma)\,\;. (2)

In a static setting, the tidal elevation in the surface point 𝐑\bf R reads:

H(𝐑,𝐫)=l=2Hl(𝐑,𝐫)=1gl=2hlWl(cosγ),\displaystyle H({\bf R},\,{\bf r})\nobreak\hskip 1.1pt\nobreak=\nobreak\hskip 1.1pt\nobreak\sum_{l=2}^{\infty}H_{l}({\bf R},\,{\bf r})\nobreak\hskip 1.1pt\nobreak=\;\;-\;\frac{1}{g}\;\sum_{l=2}^{\infty}h_{l}\;W_{l}(\cos\gamma)\,\;, (3)

where hlh_{l} are static quadrupole Love numbers, while the surface gravity is

g=GMR2.\displaystyle g\,=\,\frac{G\nobreak\hskip 1.1pt\nobreak M}{R^{\nobreak\hskip 0.77pt\nobreak 2}}\;\;. (4)

In the submoon point, we have γ=0\gamma=0 and therefore P2(cosγ)=P3(cosγ)=1P_{2}(\cos\gamma)=P_{3}(\cos\gamma)=1. In the antimoon one, we get γ=π\gamma=\pi, whence P2(cosγ)=1P_{2}(\cos\gamma)=1 and P3(cosγ)=1P_{3}(\cos\gamma)=-1.

Together, equations (1 - 4) entail the following expression for the elevation in the submoon and antimoon points:

H=H2+H3+O((R/r)5),\displaystyle H\,=\,H_{2}\,+\,H_{3}\,+\,O(\nobreak\hskip 1.1pt\nobreak(R/r)^{5}\nobreak\hskip 1.1pt\nobreak)\,\;, (5)

where

H2=h2R2GMGMr(Rr)2=h2MM(Rr)3R,\displaystyle H_{2}\,=\;h_{2}\;\frac{R^{\nobreak\hskip 0.77pt\nobreak 2}}{G\nobreak\hskip 1.1pt\nobreak M}\;\frac{G\,M^{\,\prime}}{r}\,\left(\frac{R}{r}\right)^{2}\,=\;h_{2}\,\frac{M^{\,\prime}}{M\,}\nobreak\hskip 1.1pt\nobreak\left(\frac{R}{r}\right)^{3}\nobreak\hskip 1.1pt\nobreak R\,\;, (6)
H3=±h3R2GMGMr(Rr)3=±h3MM(Rr)4R,\displaystyle H_{3}=\,\pm\,h_{3}\,\frac{R^{\nobreak\hskip 0.77pt\nobreak 2}}{G\nobreak\hskip 1.1pt\nobreak M}\;\frac{G\,M^{\,\prime}}{r}\,\left(\frac{R}{r}\right)^{3}=\,\pm\,h_{3}\,\frac{M^{\,\prime}}{M\,}\nobreak\hskip 1.1pt\nobreak\left(\frac{R}{r}\right)^{4}\nobreak\hskip 1.1pt\nobreak R\,\;, (7)

the “plus” and “minus” signs corresponding to the sub- and antimoon points.

For a moon on a circular synchronous orbit, rr is the synchronous radius:

r=(G(M+M)Ω 2)1/3,\displaystyle r\,=\,\left(\frac{G\,(M+M^{\,\prime})}{\Omega^{\,2}}\right)^{\nobreak\hskip 0.77pt\nobreak 1/3}\,\;, (8)

Ω\Omega being the planet’s ‘initial’ rotation rate. By ‘initial’, we understand the rate established at the time of rotation synchronisation, i.e., equal to the mean motion of the moon at that time. This rotation rate was thereafter sustained by the synchronous moon till its elimination.

Since a part of the centrifugal force mimics the quadrupole component of the tidal force (see Appendix C), a link exists between the then values of the dynamical oblateness J2J_{2}, the Love number k2k_{2}, and the rotation rate Ω\Omega\;:

Ω2=3GMJ2R 3k2,\displaystyle\Omega^{\nobreak\hskip 0.77pt\nobreak 2}\nobreak\hskip 1.1pt\nobreak=\;\frac{3\,G\nobreak\hskip 1.1pt\nobreak M\nobreak\hskip 1.1pt\nobreak J_{2}}{R^{\,3}\,k_{2}}\;\,, (9)

where J2J_{2} is related to the principal moments of inertia A<B<CA<B<C through

J2=C(A+B)/2MR 2.\displaystyle J_{2}\nobreak\hskip 1.1pt\nobreak=\,\frac{C\nobreak\hskip 1.1pt\nobreak-\nobreak\hskip 1.1pt\nobreak(A\nobreak\hskip 1.1pt\nobreak+\nobreak\hskip 1.1pt\nobreak B)/2}{M\;R^{\,2}}\;\;. (10)

Combined, formulae (8) and (9) yield a convenient expression for the synchronous radius’ early value:

r=R(k23J2M+MM) 1/3.\displaystyle r\,=\,R\,\left(\frac{k_{2}}{3\nobreak\hskip 1.1pt\nobreak J_{2}}\;\frac{M+M^{\,\prime}}{M}\right)^{\,1/3}\;\,. (11)

A subsequent insertion of this expression in equations (6 - 7) results in

H2= 3J2h2k2MM+MMMR= 5J2MM+MR,\displaystyle H_{2}\,=\;3\,J_{2}\,\frac{h_{2}}{k_{2}}\;\frac{M}{\nobreak\hskip 1.1pt\nobreak M+M^{\,\prime}\nobreak\hskip 1.1pt\nobreak}\;\frac{\nobreak\hskip 1.1pt\nobreak M^{\,\prime}\nobreak\hskip 1.1pt\nobreak}{M\,}\;R\,=\,5\,J_{2}\;\frac{M^{\,\prime}}{\nobreak\hskip 1.1pt\nobreak M+M^{\,\prime}\nobreak\hskip 1.1pt\nobreak}\,R\;\;, (12)
H3\displaystyle H_{3} =\displaystyle= ±h3(3J2k2MM+M) 4/3MMR\displaystyle\pm\;h_{3}\,\left(\frac{3\nobreak\hskip 1.1pt\nobreak J_{2}}{k_{2}}\;\frac{M}{M+M^{\,\prime}}\right)^{\,4/3}\frac{\nobreak\hskip 1.1pt\nobreak M^{\,\prime}\nobreak\hskip 1.1pt\nobreak}{M\,}\;R~{}
=\displaystyle= ±H273k3k24/3(3J2)1/3(MM+M)1/3,\displaystyle\pm\;H_{2}\;\frac{7}{3}\;\nobreak\hskip 1.1pt\nobreak\frac{k_{3}}{k_{2}^{4/3}}\;\nobreak\hskip 1.1pt\nobreak(3\nobreak\hskip 1.1pt\nobreak J_{2})^{1/3}\nobreak\hskip 1.1pt\nobreak\left(\frac{M}{M+M^{\,\prime}}\right)^{1/3}\,\;,

where we used the hydrodynamic relations h2/k2=5/3h_{2}/k_{2}=5/3 and h3/k3=7/3h_{3}/k_{3}=7/3 acceptable for a hot planet (Appendix A).

We observe that the relative asymmetry H3/H2H_{3}/H_{2} is proportional to the factors (3J2)1/3(3\nobreak\hskip 1.1pt\nobreak J_{2})^{1/3} and k3k24/3\nobreak\hskip 1.1pt\nobreak{k_{3}}\nobreak\hskip 1.1pt\nobreak{k_{2}^{\nobreak\hskip 0.77pt\nobreak-\nobreak\hskip 0.77pt\nobreak 4/3}}\nobreak\hskip 1.1pt\nobreak. As will be explained in Section 4, the former of these factors has undergone a very limited time evolution and may be attributed its present-day value: (3J2)1/3=0.18\nobreak\hskip 1.1pt\nobreak(3\nobreak\hskip 1.1pt\nobreak J_{2})^{1/3}=0.18\,. By distinction, k3k24/3\nobreak\hskip 1.1pt\nobreak{k_{3}}\nobreak\hskip 1.1pt\nobreak{k_{2}^{\nobreak\hskip 0.77pt\nobreak-\nobreak\hskip 0.77pt\nobreak 4/3}} dropped at some point. Thence, very naturally, the earlier the triaxial figure was formed the larger its seed asymmetry was. We shall dwell on this in Section 6 in more detail.

4 Parameters

Provided in Table 1, the present values of the Martian mass and mean radius,

M(present)= 6.4169×1023kg,R(present)= 3.3895×106m,\displaystyle M^{\rm(present)}\nobreak\hskip 1.1pt\nobreak=\,6.4169\times 10^{23}~{}\mbox{kg}~{}~{},\quad R^{\rm(present)}\,=\,3.3895\times 10^{6}~{}\mbox{m}~{}~{}, (14)

include the late veneer carried out mostly by the planetesimals left-over from the terrestrial planet formation period. According to Nesvorný et al. (2023, Fig. 17a) it added 1.6% to Mars’s mass, almost a third of this addition having arrived during the LHB. Hence the estimates for a young Mars:

M=6.31×1023kg,R=3.37×106m.\displaystyle M\nobreak\hskip 1.1pt\nobreak=\nobreak\hskip 1.1pt\nobreak 6.31\times 10^{23}~{}\mbox{kg}~{}~{},\quad R\nobreak\hskip 1.1pt\nobreak=\nobreak\hskip 1.1pt\nobreak 3.37\times 10^{6}~{}\mbox{m}~{}~{}. (15)

Now, the dynamical oblateness and triaxiality, whose current values are given in Table 1. With Tharsis “removed”, J2J_{2} is reduced by approximately 5%5\% for a fully hydrostatic J2J_{2} to approximately 10%10\% for J2J_{2} that is 20%20\% nonhydrostatic (Zuber and Smith, 1997). In our case, however, the reduction of J2J_{2} would have been much less, because we would ignore not the entire Tharsis but only its highest part caused by later uplifts and eruptions, and would leave the tidal contribution. Another change in J2J_{2} might have come from the accretion of exterior material, especially during the LHB. While the arrival rate of deposits may have, in principle, depended on the latitude, any such nonuniformity of mass influx was smeared by the equinoctial precession of Mars and large variations of Mars’ obliquity over its history. This averages out the influence of bombardment on J2J_{2}. These considerations legitimise our use of the present oblateness in calculations pertaining to the figure-formation stage (especially in formulae (LABEL:H3) and (24) for the seed triaxiality, where J2J_{2} is raised to the power of 1/31/3):

J2J2(present)= 1.96×103.\displaystyle J_{2}\nobreak\hskip 1.1pt\nobreak\approx\,J_{2}^{\rm(present)}\nobreak\hskip 1.1pt\nobreak=\,1.96\times 10^{-3}\,\;. (16)

Related to the principal moments A<B<C\nobreak\hskip 1.1pt\nobreak A<B<C\nobreak\hskip 1.1pt\nobreak through

J22=BA4MR 2,\displaystyle J_{22}\nobreak\hskip 1.1pt\nobreak=\,\frac{B\nobreak\hskip 1.1pt\nobreak-\nobreak\hskip 1.1pt\nobreak A}{4\nobreak\hskip 1.1pt\nobreak M\nobreak\hskip 1.1pt\nobreak R^{\,2}}\;\;, (17)

the dynamical triaxiality may have been more sensitive to later uplifts and volcanism, especially at Tharsis and opposite to it. (Recall that within our hypothesis the areas around the frozen tidal bulges are supposed to have been more prone to these processes.) So the relative increase of J22J_{22} may have been more noticeable than that of J2J_{2}. Therefore the present triaxiality J22(present)J_{22}^{\rm(present)} serves as the upper bound for the early value J22J_{22}\,:

J22J22(present)= 6.31×105.\displaystyle J_{22}\nobreak\hskip 1.1pt\nobreak\lesssim\;J_{22}^{\rm(present)}\,=\,6.31\times 10^{-5}\,\;. (18)

5 How massive a moon is needed?

For the purpose of estimate, we assume the seed equatorial asymmetry to be small, |H3|H2\nobreak\hskip 1.1pt\nobreak|\nobreak\hskip 1.1pt\nobreak H_{3}\nobreak\hskip 1.1pt\nobreak|\nobreak\hskip 1.1pt\nobreak\ll\nobreak\hskip 1.1pt\nobreak H_{2}\nobreak\hskip 1.1pt\nobreak, and model the soft young planet with a homogeneous ellipsoid having the principal axes a>b>ca>b>c, whence A=M5(b2+c2)\nobreak\hskip 1.1pt\nobreak A\nobreak\hskip 1.1pt\nobreak=\nobreak\hskip 1.1pt\nobreak\frac{\textstyle M}{\textstyle 5}\nobreak\hskip 1.1pt\nobreak(b^{2}+c^{2})\nobreak\hskip 1.1pt\nobreak and B=M5(c2+a2)\nobreak\hskip 1.1pt\nobreak B\nobreak\hskip 1.1pt\nobreak=\nobreak\hskip 1.1pt\nobreak\frac{\textstyle M}{\textstyle 5}\nobreak\hskip 1.1pt\nobreak(c^{2}+a^{2})\nobreak\hskip 1.1pt\nobreak. Insertion of these formulae in equation (17) produces

J22=15a+b2Rab2R15ab2R.\displaystyle J_{22}\nobreak\hskip 1.1pt\nobreak=\nobreak\hskip 1.1pt\nobreak\frac{1}{5}\;\frac{a+b}{2\,R}\;\frac{a-b}{2\,R}\nobreak\hskip 1.1pt\nobreak\approx\nobreak\hskip 1.1pt\nobreak\frac{1}{5}\;\frac{a-b}{2\,R}\;\,. (19)

Identifying the tidal elevation H2H_{2} with ab2\frac{\textstyle a-b}{\textstyle 2}, we obtain:

H2 5RJ22,\displaystyle H_{2}\approx\,5\,R\,J_{22}\;\,, (20)

which is about 1.11.1 km.

Using formulae (12) and (20), we arrive at a remarkably simple relation:

MJ22J2M.\boxed{\begin{array}[]{rcl}M^{\,\prime}\,\approx\,\frac{\textstyle J_{22}}{\textstyle J_{2}}\,M\,\;.\end{array}} (21)

In this expression, both J2J_{2} and J22J_{22} are parameters of a young Mars. As was explained in Section 4, the present value of the oblateness is still a tolerable estimate for the early oblateness, while the present triaxiality is only an upper bound for the early value. Combined with equality (16) and inequality (18), the above relation becomes:

MJ22(present)J2(present)M.\boxed{\begin{array}[]{rcl}M^{\,\prime}\,\lesssim\,\frac{\;\;\textstyle J_{22}^{\rm(present)}\;}{\;\textstyle J_{2}^{\rm(present)}\;}\;M\,\;.\end{array}} (22)

Insertion of the numerical values of J22(present)J_{22}^{\rm(present)}, J2(present)J_{2}^{\rm(present)},  and MM gives us:

M 3.2×102M 2.0×1022kg,\displaystyle M^{\,\prime}\,\lesssim\;3.2\times 10^{-2}\,M\,\approx\,2.0\times 10^{22}\;\mbox{kg}\;\,, (23)

which is less than one third of the lunar mass. It could have been even less than that, depending on how J22J_{22} has been boosted by the later volcanic activity.

Had we assumed that the elevation H2H_{2} is comparable to the height of Syrtis Major Planum (on average, 2.12.1 km) or of Tharsis (on average, about 77 km above the reference datum), we would have raised the value of H2H_{2} by a factor of 1.9 to 6.4, which would accordingly require, through equation (12), a moon of mass (4.317)×1022(4.3~{}-~{}17)\times 10^{22} kg, which would be between 0.60.6 and 2.32.3 lunar masses. Geophysical evidence, however, is indicating that both Syrtis Major and Tharsis owe much of their elevation to processes subsequent to the initial tidal distortion (Syrtis assumed its present shape in the early Hesperian; Tharsis in the late Hesperian, if not later). So a third of the lunar mass, equation (23), is a trustworthy bound for MM^{\,\prime}.

6 A  tidal  origin  of  Mars’ equatorial asymmetry

Owing to equations (LABEL:H3), (16), and (23), the seed elevations H2+H3H_{2}+H_{3} in the submoon and antimoon points were

H2[1±73k3k24/3(3J2)1/3(MM+M)1/3]=H2[1±0.416k3k24/3],\displaystyle H_{2}\nobreak\hskip 1.1pt\nobreak\left[\nobreak\hskip 1.1pt\nobreak 1\nobreak\hskip 1.1pt\nobreak\pm\,\frac{7}{3}\;\frac{k_{3}}{k_{2}^{4/3}}\;(3\nobreak\hskip 1.1pt\nobreak J_{2})^{1/3}\nobreak\hskip 1.1pt\nobreak\left(\frac{M}{M+M^{\,\prime}}\right)^{1/3}\nobreak\hskip 1.1pt\nobreak\right]\nobreak\hskip 1.1pt\nobreak=\nobreak\hskip 1.1pt\nobreak H_{2}\nobreak\hskip 1.1pt\nobreak\left[\nobreak\hskip 1.1pt\nobreak 1\nobreak\hskip 1.1pt\nobreak\pm\nobreak\hskip 1.1pt\nobreak 0.416\,\frac{k_{3}}{k_{2}^{4/3}}\nobreak\hskip 1.1pt\nobreak\right]\;\,,\;\; (24)

with the “plus” sign for the submoon point, “minus” for antimoon.

While addressing the timing issue would require modeling of the solidification of an early magma ocean, and of the formation and thickening of Mars’ stagnant lid, a simplified analytical approach is nonetheless possible. The insertion of expression (32) for klk_{l} into the second term of equation (24) renders the relative triaxiality, H3/H2H_{3}/H_{2}, as a function of μ\mu. This effectively would be a function of the figure formation time, had we known the history of solidification expressed as μ(t)\mu(t). Establishing of this time-dependence would constitute a separate, heavily numerical project. So for now we are using the evolving μ\mu as a parameter, instead of time. Along these lines, we find in Appendix A that the values of k3k24/3{k_{3}}{k_{2}^{-4/3}} are residing in the interval

7.59×102<k3k24/3< 3.32×101.\displaystyle 7.59\times 10^{-2}\,<\;{k_{3}}\nobreak\hskip 1.1pt\nobreak{k_{2}^{\nobreak\hskip 0.77pt\nobreak-\nobreak\hskip 0.77pt\nobreak 4/3}}\;<\,3.32\times 10^{-1}\,\;. (25)

The upper bound corresponds to a figure that was formed at the magma-ocean stage and sustained by the moon into the solidification epoch. This scenario implies that the moon showed up on the then synchronous orbit when the Martian mean shear modulus was not very different from that of a near-liquid lava, μ0.2×109\nobreak\hskip 1.1pt\nobreak\mu\nobreak\hskip 1.1pt\nobreak\simeq\nobreak\hskip 1.1pt\nobreak 0.2\times 10^{9} Pa. The lower bound in equation (25) pertains to a scenario wherein the moon got synchronised when the solidification was already going on, with the mean viscosity about μ18×109\mu\simeq 18\times 10^{9} Pa.

We observe that an early formation renders a higher seed asymmetry, with an elevation of 1.14H2\simeq 1.14\,H_{2} in the submoon point, and 0.86H2\simeq 0.86\,H_{2} in the antimoon one. A later formation produces a lower asymmetry, with elevations of 1.03H2\simeq 1.03\,H_{2} and 0.97H2\simeq 0.97\,H_{2} in the submoon and antimoon points, correspondingly. This may be regarded as an argument in favour of the moon having emerged and synchronised its mean motion during the magna-ocean period already. On the other hand, if part (b) of our hypothesis in Section 1 is correct, and the tidally elevated areas were most prone to geophysical processes, then even a small initial tidal asymmetry could later entail a larger asymmetry of shape — an issue requiring numerical treatment.

7 Sanity checks

7.1 Nerio was staying outside the Roche sphere

For the synchronicity radius rr of a young Mars, equations (11) and (16) yield:

rR= 5.56k23,\displaystyle\frac{r}{R}\;=\;5.56\;\sqrt[3]{k_{2}}\,\;, (26)

wherefrom

3.88<rR< 6.22.\displaystyle 3.88\,<\,\frac{r}{R}\,<\,6.22\;\,. (27)

Here the upper bound corresponds to a situation where the synchronous moon appeared and formed the figure already at the magma-ocean period, when the planet’s mean rigidity μ\mu was of order 0.20.2 GPa. The lower bound corresponds to a slightly later formation when the solidification was starting, and the mean rigidity was about 1818 GPa. Borrowed from a study of viscoelastic behaviour of basaltic lavas near the softening point (James et al., 2004), these limiting values define an interval for the of values of k2k_{2}, see Appendix A. The uncertainty in our knowledge of the interval for μ\mu, and therefore of the interval for k2k_{2}, is mitigated by k2k_{2} being raised to the power of 1/31/3 in the expression above. Still, the second decimal in the double inequality (27) should be taken with caution, both because of the uncertainty of the limits on μ\mu and because of the approximate nature of the assumption (16) for J2J_{2}.

Even the minimal value of rr in equation (27) is well above the Roche radius, which is

rR= 2.20R(ρpρm)1/3= 2.20R(ρpρM)1/3=2.32R.\displaystyle r_{R}=\,2.20\,R\,\left(\frac{\rho_{p}}{\rho_{m}}\right)^{1/3}\,=\,2.20\,R\,\left(\frac{\rho_{p}}{\rho_{M}}\right)^{1/3}=2.32R\,\;. (28)

In this expression for rRr_{R}, the average density of the planet Mars is ρp=3934\rho_{p}=3934 kg m-3, while the average density ρm\rho_{m} of the moon is approximated with that of our own Moon, ρM=3344\rho_{M}=3344 kg m3{}^{-3}\nobreak\hskip 1.1pt\nobreak. For the overall factor, we employed not Chandrasekhar’s incompressible-fluid factor 2.462.46 but a lower value 2.202.20 appropriate to rubble piles with some shear strength (Leinhardt et al., 2012). The actual factor for solids should be even smaller, which would further ensure the desired inequality r>rR\nobreak\hskip 1.1pt\nobreak r>r_{R}\nobreak\hskip 1.1pt\nobreak.

While Phobos, with its a=2.76R(present)a=2.76\nobreak\hskip 1.1pt\nobreak R^{\rm(present)}, is now entering the Roche sphere whose radius is 2.80R(present)2.80\nobreak\hskip 1.1pt\nobreak R^{\rm(present)}, for Nerio equation (28) gives 2.322.32 instead of 2.802.80 because the density of a large moon is much higher than that of Phobos.

7.2 Nerio’s mass was sufficient
to synchronise Mars’ rotation

7.2.1 Scenario 1. Tidal synchronisation by a receding moon

If the moon is tidally receding, synchronisation may be achieved if several conditions are fulfilled. The synchronous radius rr must be residing between the Roche radius rRr_{R} and the reduced Hill radius rH\nobreak\hskip 1.1pt\nobreak r_{H}^{\,\prime}\nobreak\hskip 1.1pt\nobreak\;:

rR<r<rH.\displaystyle r_{R}\nobreak\hskip 1.1pt\nobreak<\;r\,<\;r_{H}^{\,\prime}\;\,. (29)

For dynamical consequences of these two inequalities, see Makarov and Efroimsky (2023, Appendix A and Section 5, correspondingly). Neither of these inequalities imposes a restriction on the moon-to-planet mass ratio M/MM^{\,\prime}/M\nobreak\hskip 1.1pt\nobreak.

The third condition to be obeyed is this: the synchronism must be attained before the moon leaves the reduced Hill sphere. Most counterintuitively, this condition is not the same as r<rHr\,<\;r_{H}^{\,\prime}\nobreak\hskip 1.1pt\nobreak. What it actually implies is that at some instant of time (not necessarily from the start) the expansion rate of the synchronous radius must exceed the expansion rate of the moon’s orbit — and must keep exceeding it until the synchronisation. This condition does render a restriction on M/MM^{\,\prime}/M. By equation (52) from Ibid, it reads:

MM>(RrH)2,\displaystyle\frac{M^{\,\prime}}{M}\;>\;\left(\nobreak\hskip 1.1pt\nobreak\frac{R}{r_{H}^{\,\prime}}\nobreak\hskip 1.1pt\nobreak\right)^{2}\;\,, (30)

RR being the planet’s radius, and rHr_{H}^{\,\prime} the reduced Hill radius given by equation (2) from Ibid. The insertion of parameters’ values shows that this constraint is mild:

MM> 4.1×105,\displaystyle\frac{M^{\,\prime}}{M}\;>\;4.1\times 10^{-5}\,\;, (31)

and is easily satisfied by the moon we are having in mind.

7.2.2 Scenario 2. Tidal synchronisation by a descending moon

All said above about the two inequalities (29) remains in force for tidal descent. Also, equation (30), again, renders a third condition. As explained in Makarov and Efroimsky (2023, Section 9.2), violation of this inequality leaves the moon no possibility to evade spiralling onto the Roche limit. So we again end up with the mild constraint (31).

7.3 Timescales

7.3.1 Partners’ spin evolution

At the moment of its accretion or capture, the moon’s rotation was likely faster than orbiting; and the timescale τm\tau_{m} of evolution of its rotation may be termed simply “despinning timescale” or “deceleration timescale”. For the planet, however, two options are possible. If the partners were tidally receding from one another, like the Earth and the Moon, the planet’s rotation was slowing down; so the corresponding timescale τp\tau_{p} can be set positive and named “despinning timescale” or “deceleration timescale”. By distinction, were the synchronism being attained via tidal approach, the planet’s rotation was accelerating. While the corresponding timescale τp\tau_{p} still may be termed “despinning timescale” or “deceleration timescale”, its sign should be set negative. As explained in Appendix D, both timescales τm\tau_{m} and τp\tau_{p} were short as compared to Mars’ geological evolution times.

For an impact-created moon, even if we assume the initial separation to be as large as 6R6\nobreak\hskip 1.1pt\nobreak R and both Q/k2Q^{\,\prime}/k_{2}^{\,\prime} and Q/k2Q/k_{2} as large as 10310^{3}, the resulting rotation evolution timescales will be several years for the moon, and about a hundred thousand years for the planet. This is two orders of magnitude shorter than the duration of the magma-ocean era for Mars.

For a captured-moon scenario, choosing again both Q/k2Q^{\,\prime}/k_{2}^{\,\prime} and Q/k2Q/k_{2} to be as high as 10310^{3}, we find that the rotation-evolution timescales are short by the geological measure, assuming the initial separation did not exceed 22R\simeq 22\nobreak\hskip 1.1pt\nobreak R\nobreak\hskip 1.1pt\nobreak. Specifically, for a0=10Ra_{0}=10\nobreak\hskip 1.1pt\nobreak R\nobreak\hskip 1.1pt\nobreak and a0=22Ra_{0}=22\nobreak\hskip 1.1pt\nobreak R\nobreak\hskip 1.1pt\nobreak , the planet’s timescale τp\tau_{p} turns out to be about 10610^{6} yr and 3×1073\times 10^{7} yr, correspondingly. The former value is much shorter than the duration of the magma-ocean stage, the latter one is comparable to that duration.

Our estimates are very conservative. The actual timescales were shorter owing to the partners’ tidal heating leading to lower values of Q/k2Q^{\,\prime}/k_{2}^{\,\prime} and Q/k2Q/k_{2}. Still, a relative proximity of τp\tau_{p} to the duration of the magma-ocean stage may, arguably, be regarded as a limitation on the captured-moon scenario: the capture should not have happened at too remote a distance. Detailed numerical model of a combined orbital and geophysical history is needed to say more on this.

7.3.2 Circularisation

Estimates for the circularisation timescale are derived in Appendix E. Until a mutual synchronism is attained, the tides in the already synchronised moon are working to decrease the eccentricity, while the tides in the still nonsynchronous planet are working to boost the eccentricity value. Therefore, circularisation cannot even begin until full synchronism is reached. Once the synchronism is established, circularisation is taking place over a timescale τe\tau_{e} of about 0.10.1 to 0.30.3 of the tidal deceleration timescale τp\tau_{p} of the planet. Therefore, there is a period of time after the synchronisation, during which the orbit retains its eccentricity. Geologically, this period is short. Whether it is sufficient to produce in the planet an amount of tidal heat sufficient to influence geophysical processes requires a detailed numerical study. As we mentioned above, the pattern of this heat production was surely inhomogeneous, with its maxima around the tips of the figure.

Also, as pointed out in Appendix E, the circularisation was never complete because of two physical factors: the gravitational pull of the Sun and the role of Mars’ triaxiality (recall that circularisation begins after the synchronism is attained — i.e., after a seed triaxiality is acquired by Mars). The Sun’s gravity is especially important if the moon is tidally receding and crossing the 2:1 MMR with the Sun, at a=3.2Ra=3.2\nobreak\hskip 1.1pt\nobreak R. This crossing entails an eccentricity jump of 0.00850.0085. This eccentricity value becomes stable if the synchronous orbit happens to coincide with this MMR. The triaxiality of the planet plays an especially big role if the moon crosses the 2:1 resonance with Mars’ figure, at a=3.8Ra=3.8\nobreak\hskip 1.1pt\nobreak R\nobreak\hskip 1.1pt\nobreak. This crossing gives the eccentricity a jump of 0.0320.032\nobreak\hskip 1.1pt\nobreak — which would become a stable value for ee were the synchronous orbit able to coincide with this resonance. Though in a slight violation of inequality (27), these resonances should not be excluded from consideration, given the uncertainty in our knowledge of the then value of k2k_{2} showing up in equation (26).

7.4 Synchronism as Mars’ spin-orbit end-state

As was pointed out above, circularisation becomes efficient only after synchronisation. In other words, prior to the synchronisation, the binary could have kept its eccentricity high, and could have been even boosting it, depending on the frequency-dependencies of the quality functions k2/Qk_{2}/Q and k2/Qk_{2}^{\prime}/Q^{\,\prime} of the planet and the moon. Therefore, during the spin evolution of the planet, various spin-orbit resonances were crossed by the system. As was explained in detail by Noyelles et al. (2014), such a system can under some circumstances get stuck in one or another higher spin state — like Mercury did in the course of its tidal despinning.

It raises an issue if Mars also could have been captured in a higher spin state in the course of the Mars-Nerio spin-orbit evolution. This is important, because once a partner is caught in a higher spin state, it may stay there for good, or until some event either separates the pair or somehow pushes it out of this spin state. The potential possibility of Mars’ entrapment in a higher spin state may therefore portend a difficulty for our theory. The question then becomes if such a possibility is realistic. An answer to this question hinges on several parameters, including the eccentricity value. E.g. Mercury would have not been trapped into a higher spin state had its high eccentricity not been sustained by other planets’ pull (Noyelles et al., 2014).

Born in situ, or created by impact, or captured in the disk, a moon had a low initial eccentricity, if any. So both partners despan directly to synchronism. Also, a hot semimolten rotator cannot get stuck in a higher spin-orbit state. Moreover, had it somehow been captured in such a state during the short period between the accretion and the formation of a magma ocean, it would definitely have slipped out of that spin state during the magma-ocean stage, as explained in detail in Appendix F.

8 Results and questions

It is proposed in this work that an initial, ‘seed’ triaxiality of Mars was produced by a massive moon that was orbiting a young Mars on a synchronous orbit. Depending on whether the moon’s orbit was circular or not, the tide was static or near-static (slightly librating about the mean direction toward the synchronous moon). After the seed triaxiality was created, the tidally elevated areas on the two opposite tips became, hypothetically, more prone to geophysical processes than the rest of the Martian surface — which led to these tips’ further rise and a resulting triaxiality increase.

8.1 Results

The principal result of our study is that a moon of less than a third of the lunar mass was capable of generating the seed triaxiality. This result is deduced from the following two requirements:

  • (1) 

    The moon must have synchronised its mean motion with Mars’ rotation when Mars was still sufficiently hot, its lithosphere being absent or weak, and its tidal response being predominantly hydrostatic.

  • (2) 

    The present-day triaxiality J22(present)J_{22}^{\rm(present)} is the upper boundary for the value J22J_{22} tidally caused by the putative moon.

The putative moon Nerio failed to survive the LHB. Phobos and Deimos may be remnants of its large fragment, which was destroyed later. Indeed, while the LHB occurred 4.1 to 3.8 Gyr ago, a probable common ancestor of Phobos and Deimos was destroyed by an impact between 1.6 and 2.7 Gyr ago (Bagheri et al., 2021) — which eliminates the possibility of Phobos and Deimos being Nerio’s immediate progeny.

A symmetrical part of the seed triaxiality having originated due to the quadrupole component of the tide, the seed asymmetry was produced by the octupole component. The relative magnitude of this initial asymmetry depended on the time of creation of the initial figure. If the synchronous moon had already existed during the magma-ocean stage of Mars, the seed asymmetry would comprise an additional 14% elevation in the submoon point and a 14% reduction of elevation in the antimoon point, as compared to the symmetrical part of the elevation. If, however, the moon was synchronised somewhat later, when the process of solidification began but a lithosphere was not yet fully formed, then the seed asymmetry would be at a several percent level only. It remains to be studied by numerical modeling if the current asymmetry between Tharsis and its opposite province is due to the initial tidal distortion — or if the initial disparity was later boosted by geological processes in the submoon and antimoon zones (like the emergence of plumes).

8.2 Questions

Our paper serves as a motivation to numerically explore the evolution of a young planet whose shape is neither spherical nor even elliptic. At large, the question is if a limited initial asymmetry of the shape can entail a considerable asymmetry in the process of solidification and in the subsequent geological activity — convection, uplifts, volcanism.

More specifically, is it right to assume that geological processes were more intense in the tidally elevated areas? This question emerges both for a moon on a circular synchronous orbit (with no tidal heating in the planet) and for a moon describing an eccentric synchronous orbit and generating additional heat in the young Mars. A study by Segatz et al. (1988) has demonstrated that in a body (Io) synchronised by its partner (Jupiter) tidal heating is inhomogeneous. Whether the maximally heated areas are in the sub- and anti-Jovian zones is not warranted and depends on the internal structure. Also, that study was carried out for a spherical body and in the quadrupole approximation only. In our case, the nonspherical (and nonellipsoidal) shape of the tidally distorted young Mars will be crucial. Also, due to the proximity of the perturber, the degree-3 inputs into the tidal dissipation rate will have to be included. A study of the kind, carried out by Quillen et al. (2019) for the Moon, offers to our theory both a pro and a contra argument. On the one hand, the degree-3 component of the tide generates a considerable difference in the tidal heat flux between the near and far sides, the near side being predictably warmer and therefore having better chances for subsequent uplift and volcanism. On the other hand, within the considered model the heat flux increases toward the polar zones, thus posing a question on why the volcanic activity near the poles has been weaker than on Tharsis. The model by Quillen et al. (2019) relying on the Kelvin-Voigt rheology, a more accurate study based on a realistic rheology is then required.

Had the moon disintegrated in the early LHB, there should have been an enhanced impactor flux at low latitudes on Mars. Would the subsequent LHB, along with geological processes, be sufficient to wipe out the resulting latitudinal dependence of the most ancient crater population? As of now, the oldest crater populations show no such dependence.

Acknowledgments

The author wishes to acknowledge helpful consultations provided to him by Amirhossein Bagheri, Andrew Dombard, Amir Khan, Alessandro Morbidelli, Anthony L. Piro, Robert Schulmann, Francis Nimmo and Michaela Walterova, none of which colleagues shares responsibility for the hypothesis proposed in this work.

The author was also fortunate in having had the assistance of two reviewers who donated generously of their time, helping to shape and improve the contours of the manuscript. Their advice is greatly appreciated. Particular thanks are owed to Benoît Noyelles for suggesting the name Nerio for the putative moon.

This research has made use of NASA’s Astrophysics Data System.

Open Research

The shear rigidity values used in this paper are borrowed from James et al. (2004). The value of Mars’ present dynamical oblateness J2(present)J_{2}^{(present)} is provided in Konopliv et al. (2011). The value of Mars’ present dynamical triaxiality J22(present)J_{22}^{(present)} is given in Konopliv et al. (2020). The value M(present)M^{(present)} of Mars’ present mass is borrowed from the PDS file for the Mars gravity field MRO120D used in Konopliv et al. (2016).

APPENDIX

Appendix A Love numbers

During the magma-ocean stage and for some time thereafter, while the lithosphere was still weak, the expressions intended for a homogeneous body were applicable:

kl=32(l1)11+lμ,\displaystyle k_{l}\nobreak\hskip 1.1pt\nobreak=\,\frac{3}{2\,(l\nobreak\hskip 1.1pt\nobreak-\nobreak\hskip 1.1pt\nobreak 1)}\;\frac{1}{1\nobreak\hskip 1.1pt\nobreak+\nobreak\hskip 1.1pt\nobreak{\cal B}_{l}\,\mu}\,\;, (32)
hl=2l+12(l1)11+lμ,\displaystyle h_{l}\nobreak\hskip 1.1pt\nobreak=\,\frac{2\,l\nobreak\hskip 1.1pt\nobreak+\nobreak\hskip 1.1pt\nobreak 1}{2\,(l\nobreak\hskip 1.1pt\nobreak-\nobreak\hskip 1.1pt\nobreak 1)}\;\frac{1}{1\nobreak\hskip 1.1pt\nobreak+\nobreak\hskip 1.1pt\nobreak{\cal B}_{l}\,\mu}\,\;, (33)
l=3(2l2+4l+ 3)4lπG(ρR)2.\displaystyle{\cal B}_{l}\,=\,\frac{3\,(2l^{2}+\nobreak\hskip 1.1pt\nobreak 4\,l\,+\,3)}{4\,l\,\pi\,G\,(\rho\,R)^{2}}\;\;. (34)

Derived, historically, for homogeneous elastic spheres, these formulae can be used also for homogeneous viscoelastic spheres under static loading, as can be observed from expressions (19) and (44) in Efroimsky (2015).

From equations (32 - 33), ensue two simple formulae used in Section 3:

h2k2=53,h3k3=73.\displaystyle\frac{h_{2}}{k_{2}}\;=\;\frac{5}{3}\;\;,\qquad\frac{h_{3}}{k_{3}}\;=\;\frac{7}{3}\,\;. (35)

For a young Mars, the dimensional quantities 2{\cal B}_{2} and 3{\cal B}_{3} assume the values

2= 0.193×109kg1ms2,3= 2.24×109kg1ms2.\displaystyle\quad{\cal B}_{2}\,=\,0.193\times 10^{-9}\;\mbox{kg}^{-1}\,\mbox{m}~{}\mbox{s}^{2}\;\,,\,\quad{\cal B}_{3}\,=\,2.24\times 10^{-9}\;\mbox{kg}^{-1}\,\mbox{m}~{}\mbox{s}^{2}\,\;. (36)

Studies of viscoelastic behaviour of basaltic lavas demonstrate that on approach to a sample’s softening point its shear rigidity μ\mu is of order 18×109\simeq 18\times 10^{9} Pa, but goes down to 0.2×109\simeq 0.2\times 10^{9} Pa as sample fluidity begins to rapidly increase at temperatures exceeding 1100o1100^{\,\rm o} C (James et al., 2004):

μ=(0.218)×109Pa.\displaystyle\mu\,=\,(0.2-18)\times 10^{9}\;\nobreak\hskip 1.1pt\nobreak\mbox{Pa}\,\;. (37)

This indicates that the Love numbers at the earliest stages were residing within intervals whose upper bounds were close to the ideal-fluid values:

k2= 0.34 1.4,h2= 0.56 2.4,\displaystyle k_{2}\,=\,0.34\;-\;1.4\;\;,\;\quad h_{2}\,=\,0.56\;-\;2.4\,\;, (38)
k3= 0.018 0.52,h3= 0.042 1.2.\displaystyle k_{3}\,=\,0.018\;-\;0.52\;\;,\quad h_{3}\,=\,0.042\;-\;1.2\,\;. (39)

The value of each of these Love numbers was at the upper bound of the corresponding interval during the magma-ocean stage (with μ=0.2×109\mu=0.2\times 10^{9} Pa), and was descending to the lower bound during the solidification stage, as the rigidity was approaching μ=18×109\mu=18\times 10^{9} Pa.

For comparison, the present-day value of k2k_{2} of the solid Mars is residing between 0.1690.169 and 0.1740.174 (Konopliv et al., 2020).

In section 6, we needed to evaluate the product k3k24/3\nobreak\hskip 1.1pt\nobreak{k_{3}}\nobreak\hskip 1.1pt\nobreak{k_{2}^{\nobreak\hskip 0.77pt\nobreak-\nobreak\hskip 0.77pt\nobreak 4/3}}. Using formulae (32) and (36), we find

7.59×102<k3k24/3< 3.32×101,\displaystyle 7.59\times 10^{-2}\,<\;{k_{3}}\nobreak\hskip 1.1pt\nobreak{k_{2}^{\nobreak\hskip 0.77pt\nobreak-\nobreak\hskip 0.77pt\nobreak 4/3}}\;<\,3.32\times 10^{-1}\,\;, (40)

the maximum corresponding an early figure formation (μ0.2×109\mu\simeq 0.2\times 10^{9} Pa), the minimum to slightly later formation, with solidification already going on (μ18×109\mu\simeq 18\times 10^{9} Pa).

Appendix B Realistic values for the k2/Qk_{2}/Q of a young Mars

Figure S 3 b in the Supplement to Samuel et al (2019) suggests that, when Mars was 0.9 Byr old, its k2/Qk_{2}/Q was already as low as (0.22 - 0.24) ×103\times 10^{-3}\nobreak\hskip 1.1pt\nobreak. We however should be cautious about this result, because it is based on the hypothesis of an early origin of the Martian moons, a hypothesis applicable to Deimos but not necessarily to Phobos. Integration of Phobos’ orbit backwards in time demonstrates a rapid increase in its eccentricity (Bagheri et al., 2021) This means that in the past the tides in Phobos were stronger than those in Mars, and dominated Phobos’ descent. This indicates that the values of k2k_{2} and k2/Qk_{2}/Q provided by Samuel et al (2019) should be used as the low bounds, at best.

Also, the values of k2/Qk_{2}/Q from the said figure in Samuel et al (2019) pertain to a Mars of 0.9 Byr or older. We however are interested in a younger Mars, whose crust was only beginning to mature, but whose interior was still semimolten and not completely differentiated. Modeling this Mars with a homogeneous Maxwell body, we enquire about the magnitudes of and spread between the peaks in the tidal-mode-dependence of k2/Qk_{2}/Q\;, see Figure B1.

Refer to caption
Figure B1: . A typical shape of the quality function kl(ω)sinϵl(ω)\,k_{l}(\omega)\,\sin\epsilon_{l}(\omega)\,,  where ω\,\omega\, is a shortened notation for the tidal Fourier mode ωlmpq\,\omega_{\textstyle{{}_{lmpq}}}\,.  (From Noyelles et al. 2014.)

As shown, e.g. in Walterová et al. (2023, Section 4.4), the peak is residing at

ωpeak=τM11+2μ=μ/η1+2μ\displaystyle{\omega_{\rm{peak}}}\,=\;\;\frac{\tau_{\rm{{}_{M}}}^{-1}}{1\,+\,{\cal{B}}_{2}\,\mu}\,=\,\frac{\mu/\eta}{1\,+\,{\cal{B}}_{2}\,\mu} (41)

and has a viscosity-independent magnitude

(k2Q)(peak)=342μ1+2μ.\displaystyle\left(\frac{k_{2}}{Q}\right)^{\rm{(peak)}}\nobreak\hskip 1.1pt\nobreak=\;\frac{3}{4}\;\frac{{\cal B}_{2}\,\mu}{\nobreak\hskip 1.1pt\nobreak 1+{\cal B}_{2}\,\mu\,}\,\;. (42)

[ Mind a misprint in Bagheri et al. (2022, Eqn 62). ]

The magnitude remains viscosity-independent also when the Burgers and Andrade terms show up as the mantle cools down, because these terms usually become prominent well to the right of the peak (Walterová et al., 2023).

For high Maxwell times (say, months or years, or longer), the peaks are sharp and stay close to zero. So the values of k2/Qk_{2}/Q observed at realistic forcing frequencies are much lower than the peak value, and are defined by how quickly the slope is falling off with the frequency increase. In fact, the slope of the tail does not fall off as quickly as shown in our figure, because at frequencies well above τM1\tau_{M}^{-1} transient processes kick in, and the rheology deviates from Maxwell towards Andrade (to be more exact, towards Sundberg-Cooper), see Figure 3 in Walterová et al. (2023). Most importantly, for a semimolten planet with a Maxwell time of order hours to days, this kink becomes spread widely; and at comparable periods the values of k2/Qk_{2}/Q are not dramatically different from the peak value. So, while the peak value (42) may be by an order or two of magnitude higher than an actual k2/Qk_{2}/Q of a cold planet, it is a tolerable estimate for the k2/Qk_{2}/Q of a hot planet.

Now, numbers. In the extreme case of the magma-ocean stage, we have, from Appendix A: μ=0.2×109\mu=0.2\times 10^{9} Pa, 2μ3.9×102{\cal B}_{2}\mu\approx 3.9\times 10^{-2} and therefore (k2/Q)(peak)0.28×101\,\left({k_{2}}/{Q}\right)^{\rm{(peak)}}\nobreak\hskip 1.1pt\nobreak\approx\nobreak\hskip 1.1pt\nobreak 0.28\times 10^{-1}\,. If however we agree that the moon was giving Mars its shape shortly thereafter, i.e. when solidification began, then the corresponding value μ=18×109\mu=18\times 10^{9} Pa from Appendix A gives us 2μ3.5{\cal B}_{2}\mu\approx 3.5 and therefore (k2/Q)(peak)0.58\,\left({k_{2}}/{Q}\right)^{\rm{(peak)}}\nobreak\hskip 1.1pt\nobreak\approx\nobreak\hskip 1.1pt\nobreak 0.58\nobreak\hskip 1.1pt\nobreak. Thus we see that, for a young Mars, k2/Qk_{2}/Q is taking values, roughly, between 0.030.03 and 0.60.6.

Appendix C Splitting the centrifugal force into a radial and quadrupole components

Using the expression P2(cosγ)=12(3cos2γ1)\nobreak\hskip 1.1pt\nobreak P_{2}(\cos\gamma)=\frac{\textstyle 1}{\textstyle 2}\left(3\nobreak\hskip 1.1pt\nobreak\cos^{2}\gamma-1\right), we split the centrifugal acceleration into a quadrupole and radial parts,

𝛀×(𝛀×𝑹)\displaystyle\boldsymbol{\Omega}\times\left(\boldsymbol{\Omega}\times\mbox{{\boldmath${R}$}}\right) =\displaystyle= [12𝛀 2𝑹 2(cos2γ1)]\displaystyle\nabla\left[\frac{1}{2}\boldsymbol{\Omega}^{\,2}\mbox{{\boldmath${R}$}}^{\,2}\left(\cos^{2}\gamma-1\right)\right]~{}
=\displaystyle= [13𝛀 2𝑹 2[P2(cosγ)1]],\displaystyle\nabla\left[\frac{1}{3}\boldsymbol{\Omega}^{\,2}\mbox{{\boldmath${R}$}}^{\,2}\left[P_{2}\left(\cos\gamma\right)-1\right]\right]\;\,,

the former influencing the geometric shape, the latter not. The quadrupole potential is compensated by the incremental tidal potential:

13𝛀 2𝑹 2P2(cosγ)k2GMRJ2P2(cosγ)=0,\displaystyle\frac{\textstyle 1}{\textstyle 3}\nobreak\hskip 1.1pt\nobreak\boldsymbol{\Omega}^{\,2}\nobreak\hskip 1.1pt\nobreak\mbox{{\boldmath${R}$}}^{\,2}\nobreak\hskip 1.1pt\nobreak P_{2}\left(\cos\gamma\right)\nobreak\hskip 1.1pt\nobreak-\,k_{2}\nobreak\hskip 1.1pt\nobreak\frac{\textstyle GM}{\textstyle R}\,J_{2}\,P_{2}\left(\cos\gamma\right)\nobreak\hskip 1.1pt\nobreak=\nobreak\hskip 1.1pt\nobreak 0\,\;,

whence expression (9).

Appendix D Rotation rate evolution timescales

D.1 Generalities

The tidal deceleration timescales of the moon and planet are, correspondingly,

τm=Qk2MMM+MM1n(aR)3\displaystyle\tau_{m}\nobreak\hskip 1.1pt\nobreak=\;\frac{Q^{\,\prime}}{k_{2}^{\nobreak\hskip 0.77pt\nobreak\prime}}\;\frac{M^{\,\prime}}{M}\;\frac{M\nobreak\hskip 1.1pt\nobreak+\nobreak\hskip 1.1pt\nobreak M^{\,\prime}}{M}\;\frac{1}{n}\nobreak\hskip 1.1pt\nobreak\left(\frac{a}{R^{\,\prime}}\right)^{3} \displaystyle\approx Qk2MM1n(aR)3\displaystyle\frac{Q^{\,\prime}}{k_{2}^{\nobreak\hskip 0.77pt\nobreak\prime}}\;\frac{M^{\,\prime}}{M}\;\frac{1}{n}\nobreak\hskip 1.1pt\nobreak\left(\frac{a}{R^{\,\prime}}\right)^{3} (44)
=\displaystyle= Qk2MMρmρpΠ\displaystyle\frac{Q^{\,\prime}}{k_{2}^{\nobreak\hskip 0.77pt\nobreak\prime}}\;\frac{M^{\,\prime}}{M}\,\frac{\rho_{m}}{\rho_{p}}\;\Pi\qquad

and

τp=±Qk2MMM+MM1n(aR)3±Qk2(MM)2Π,\displaystyle\tau_{p}\nobreak\hskip 1.1pt\nobreak=\;\pm\;\frac{Q}{k_{2}}\;\frac{M}{M^{\,\prime}}\;\frac{M\nobreak\hskip 1.1pt\nobreak+\nobreak\hskip 1.1pt\nobreak M^{\,\prime}}{M^{\,\prime}}\;\frac{1}{n}\nobreak\hskip 1.1pt\nobreak\left(\frac{a}{R}\right)^{3}\nobreak\hskip 1.1pt\nobreak\approx\;\pm\;\frac{Q}{k_{2}}\;\left(\frac{M}{M^{\,\prime}}\right)^{2}\Pi\;\,, (45)

k2/Qk_{2}/Q and k2/Qk_{2}^{\nobreak\hskip 0.77pt\nobreak\prime}/Q^{\,\prime} being the tidal parameters of the planet and moon, ρp\rho_{p} and ρm\rho_{m} being their densities, and a common dimensional factor Π\Pi given by equation (46) below.

The “±\pm” sign in the expression for τp\tau_{p} implies that a positive despinning timescale τp\tau_{p} corresponds to a setting where the synchronism is attained by the recession of the moon (like in the Earth-Moon case, with the Earth’s rotation gradually decelerating). A negative despinning timescale is characteristic of an opposite situation where the synchronism is achieved by tidal descent of the moon and acceleration of the planet’s rotation. On both occasions, one may use the terms “despinning time” or “deceleration time”, keeping in mind that this “despinning” can sometimes be actually a spin-up.

Expressions (44) and (45) follow, e.g. from equation (116) in Efroimsky (2012). An independent check can be performed by combining formulae (123), (132), and (188) from Boué and Efroimsky (2019). Since Goldreich and Soter (1966) were interested in the despinning of the smaller partner, their equation (17) agrees with the r.h.s. of our expression (44), not of (45).

Dividing formulae (44) and (45) by one another, we obseve that τm/τp1\tau_{m}/\tau_{p}\ll 1 in all realistic situations. This is so owing to the smallness of the factor (M/M)3(ρm/ρp)<3×105\left(M^{\,\prime}/M\right)^{3}\left(\rho_{m}/\rho_{p}\right)<3\times 10^{-5}\nobreak\hskip 1.1pt\nobreak emerging in that ratio.

The common factor Π\Pi entering formulae (44) and (45) is given by

Π=n1(aR)3=R3/2G(M+M)(aR)9/2\displaystyle\Pi=n^{-1}\left(\frac{a}{R}\right)^{3}\,=\;\frac{R^{\nobreak\hskip 0.77pt\nobreak 3/2}}{\sqrt{G\nobreak\hskip 1.1pt\nobreak(M+M^{\,\prime})}}\,\left(\frac{a}{R}\right)^{9/2} (46)

and scales as a4.5\nobreak\hskip 1.1pt\nobreak a^{4.5}. E.g. for Phobos, it has the value ΠPhobos=0.88×105\Pi_{\rm\nobreak\hskip 0.77pt\nobreak Phobos}=0.88\times 10^{5} s.

For the hypothetical moon Nerio, the lower bound on Π\Pi pertains to a situation where a0a_{0} (the initial value of aa, one corresponding to a freshly formed or captured moon) equals the Roche radius rR=2.32Rr_{R}=2.32\nobreak\hskip 1.1pt\nobreak R\nobreak\hskip 1.1pt\nobreak. This yields:

minΠ= 0.41×105s.\displaystyle\operatorname{min}\,\Pi\,=\,0.41\times 10^{5}\,\;\mbox{s}\,\;. (47)

In this case, the subsequent synchronisation of the orbit with the planet’s rotation could have been achieved only through tidal recession, because tidal descent would have driven the moon into the Roche zone. Keeping in mind that MMρmρp2.7×102\frac{\textstyle M^{\,\prime}}{\textstyle M}\,\frac{\textstyle\rho_{m}}{\textstyle\rho_{p}}\nobreak\hskip 1.1pt\nobreak\approx 2.7\times 10^{-2}\nobreak\hskip 1.1pt\nobreak, we deduce that within this scenario the synchronisation of both partners is almost instantaneous. E.g. for Q/k2Q^{\,\prime}/k_{2}^{\prime} and Q/k2Q/k_{2} of order 10310^{3}, the timescales come out as low as

minτm 106s,minτp 4×1010s.\displaystyle\operatorname{min}\,\tau_{m}\,\simeq\,10^{6}\,\;\mbox{s}\quad,\qquad\operatorname{min}\,\tau_{p}\,\simeq\,4\times 10^{10}\,\;\mbox{s}\,\;. (48)

To find the maximal values of τm\tau_{m} and τp\tau_{p}, we need to evaluate the upper bound on Π\Pi, one corresponding to the maximal realistic initial value a0a_{0} of the semimajor axis. Two cases have to be addressed separately.

D.2 A moon formed by impact

In numerical simulations, most clumps left orbiting an Earth-sized planet after impact usually stay within several radii from its centre (Ruiz-Bonilla et al., 2020). To be on the safe side, assume that the initial semimajor axis obeyed a/R<6a/R<6\nobreak\hskip 1.1pt\nobreak; thence

maxΠ= 0.30×107s.\displaystyle\operatorname{max}\,\Pi\,=\,0.30\times 10^{7}\;\mbox{s}\;. (49)

For Q/k2Q^{\,\prime}/k_{2}^{\prime} and Q/k2Q/k_{2} of order 10310^{3}, this entails the maximal values of

maxτm108s 3yr,maxτp 3×1012s 105yr,\displaystyle\operatorname{max}\,\tau_{m}\nobreak\hskip 1.1pt\nobreak\simeq\nobreak\hskip 1.1pt\nobreak 10^{8}\;\mbox{s}\;\simeq\,3\nobreak\hskip 1.1pt\nobreak\;\mbox{yr}\;\;\;,\qquad\operatorname{max}\,\tau_{p}\nobreak\hskip 1.1pt\nobreak\simeq\,3\times 10^{12}\;\mbox{s}\;\simeq\,10^{5}\nobreak\hskip 1.1pt\nobreak\;\mbox{yr}\,\;, (50)

i.e., the spin of the moon becomes synchronous within several years; of the planet within a hundred thousand years. Even if we (illegitimately) boost the values of Q/k2Q^{\,\prime}/k_{2}^{\prime} and Q/k2Q/k_{2} by another order of magnitude, we still shall be left with geophysically short times. In reality, the values of Q/k2Q^{\,\prime}/k_{2}^{\prime} and Q/k2Q/k_{2} should sooner be reduced than boosted, because both bodies were experiencing tidal heating. So the actual timescales of deceleration would be shorter than those given by equation (50).

D.3 A captured moon

In the disk, the moon could have been captured, in principle, at an initial separation exceeding that typical for creation of a moon by impact. The factor Π\Pi and, consequently, the spin evolution times τm\tau_{m} and τp\tau_{p} scale as a4.5a^{4.5}. An increase of the initial separation a0a_{0} by a factor of 5/31.675/3\nobreak\hskip 1.1pt\nobreak\approx\nobreak\hskip 1.1pt\nobreak 1.67 would result in a ten-fold increase of the time scales. For example, had we taken in the above calculation the initial separation to be a0=10R\nobreak\hskip 1.1pt\nobreak a_{0}=10\nobreak\hskip 1.1pt\nobreak R\nobreak\hskip 1.1pt\nobreak, we would have obtained, instead of values (50), the values

maxτm109s 30yr,maxτp 3×1013s 106yr,\displaystyle\operatorname{max}\,\tau_{m}\nobreak\hskip 1.1pt\nobreak\simeq\nobreak\hskip 1.1pt\nobreak 10^{9}\;\mbox{s}\;\simeq\,30\nobreak\hskip 1.1pt\nobreak\;\mbox{yr}\;\;\;,\quad\operatorname{max}\,\tau_{p}\nobreak\hskip 1.1pt\nobreak\simeq\,3\times 10^{13}\;\mbox{s}\;\simeq\,10^{6}\nobreak\hskip 1.1pt\nobreak\;\mbox{yr}\;, (51)

while for a0=22R\nobreak\hskip 1.1pt\nobreak a_{0}=22\nobreak\hskip 1.1pt\nobreak R\nobreak\hskip 1.1pt\nobreak it would have been

maxτm3.5×1010s 103yr,maxτp 1015s 3×107yr.\displaystyle\operatorname{max}\,\tau_{m}\nobreak\hskip 1.1pt\nobreak\simeq\nobreak\hskip 1.1pt\nobreak 3.5\times 10^{10}\;\mbox{s}\;\simeq\,10^{3}\nobreak\hskip 1.1pt\nobreak\;\mbox{yr}\;\;\;,\quad\operatorname{max}\,\tau_{p}\nobreak\hskip 1.1pt\nobreak\simeq\,10^{15}\;\mbox{s}\;\simeq\,3\times 10^{7}\nobreak\hskip 1.1pt\nobreak\;\mbox{yr}\,. (52)

Larger initial values a0a_{0} may not fit into our story because of wrong timing. Our scenario requires the planet to synchronise its rotation with the mean motion nn while the planet is still sufficiently deformable and capable of acquiring an asymmetric tidal shape to freeze later. We thus expect the synchronisation to happen well before the planet’s age is 108\sim 10^{8} years. Modeling by Samuel et al. (2019, Fig S3b) suggests that by the age of (28)×108\sim(2-8)\times 10^{8} yr the planet’s k2/Qk_{2}/Q becomes comparable to its present value, indicating that the planet’s shape may have started freezing by that time.

Just like in the case of an impact-made moon, so in the case of a captured moon, tidal heating in the partners was working to increase the values of k2/Qk_{2}/Q and k2/Qk_{2}^{\prime}/Q^{\,\prime} and, consequently, to shorten the actual despinning times.

D.4 Conclusions

No matter how the moon was acquired, for an initial separation not exceeding 22R22\nobreak\hskip 1.1pt\nobreak R and the values of Q/k2Q^{\,\prime}/k_{2}^{\prime} and Q/k2Q/k_{2} not exceeding 10310^{3}, the spin evolution timescales are short by the geological measure. For an initial separation less than 10R10\nobreak\hskip 1.1pt\nobreak R, synchronisation is especially swift.

In reality, both timescales should have been shorter than those obtained above, because tidal heating reduces the values of both Q/k2Q^{\,\prime}/k_{2}^{\prime} and Q/k2Q/k_{2}.

Appendix E Tidal circularisation

When the spin of neither body is synchronised, while both obliquities (inclinations of the equators on the orbit plane) are small, the leading terms in the eccentricity rate are those linear in e\,e\, (Boué and Efroimsky, 2019):

(dedt)l=2=neMM(Ra)5[316K2(n2θ˙)34K2(2n2θ˙)\displaystyle\left(\frac{de}{dt}\right)_{l=2}=\,-\,n\,e\,\frac{\,M^{\,\prime}}{M\,}\,\left(\frac{R}{a}\right)^{\textstyle{{}^{5}}}\,\left[-\,\frac{3}{16}\,K_{2}(n-2\dot{\theta})\,-\,\frac{3}{4}\,K_{2}(2n-2\dot{\theta})\right.
+14716K2(3n2θ˙)+98K2(n)]\displaystyle\left.\,+\,\frac{147}{16}\,\,K_{2}(3n-2\dot{\theta})\,+\,\frac{9}{8}\,\,K_{2}(n)\right]\;\;\;\;
neMM(Ra)5[316K2(n2θ˙)34K2(2n2θ˙)\displaystyle-\,n\,e\,\frac{M\,}{\,M^{\,\prime}}\,\left(\frac{R^{\;\prime}}{a}\right)^{\textstyle{{}^{5}}}\,\left[-\,\frac{3}{16}\,K_{2}^{\,\prime}(n-2\dot{\theta}^{\,\prime})\,-\,\frac{3}{4}\,K_{2}^{\,\prime}(2n-2\dot{\theta}^{\,\prime})\right.
+14716K2(3n2θ˙)+98K2(n)]\displaystyle\left.\,+\,\frac{147}{16}\,K_{2}^{\,\prime}(3n-2\dot{\theta}^{\,\prime})\,+\,\frac{9}{8}\,K_{2}^{\,\prime}(n)\right]
+O(e2)+O(i2)+O(i2).\displaystyle\;+\;O(e^{2})\;+\;O(i^{2})\,+\,O({i^{\,\prime\;}}^{2})~{}~{}_{\textstyle{{}_{\textstyle.}}}\quad (53)

Here, θ˙\dot{\theta} and θ˙\dot{\theta}^{\,\prime} are the planet’s and moon’s rotation rates, while K2K_{2} and K2K_{2}^{\,\prime} are their (odd) tidal quality functions, such that |K2|=k2/Q|K_{2}|=k_{2}/Q and |K2|=k2/Q|K_{2}^{\,\prime}|=k_{2}^{\prime}/Q^{\,\prime}.

When both partners satisfy the Constant Phase Lag (CPL) model (so both K2\,K_{2}\, and K2\,K_{2}^{\,\prime}\, are constants) and both θ˙\,\dot{\theta}\, and θ˙\,\dot{\theta}^{\,\prime}\, exceed  3n/2\,3n/2\,, we have:

K2(n)=K2(n2θ˙)=K2(2n2θ˙)=K2(3n2θ˙)=k2/QK_{2}(n)\,=\,-\,K_{2}(n-2\dot{\theta})\,=\,-\,K_{2}(2n-2\dot{\theta})\,=\,-\,K_{2}(3n-2\dot{\theta})\,=\,k_{2}/Q\,

and

K2(n)=K2(n2θ˙)=K2(2n2θ˙)=K2(3n2θ˙)=k2/Q,K^{\,\prime}_{2}(n)\,=\,-\,K_{2}^{\,\prime}(n-2\dot{\theta}^{\,\prime})\,=\,-\,K_{2}^{\,\prime}(2n-2\dot{\theta}^{\,\prime})\,=\,-\,K_{2}^{\,\prime}(3n-2\dot{\theta}^{\,\prime})\,=\,k_{2}^{\,\prime}/Q^{\,\prime}\,\;,

wherefrom

(dedt)l=2(CPL)=578ne[MM(Ra)5k2Q+MM(Ra)5k2Q]{}^{\textstyle{{}^{(CPL)}}}\left(\frac{de}{dt}\right)_{l=2}=\,\frac{57}{8}\,n\,e\,\left[\frac{\,M^{\,\prime}}{M\,}\,\left(\frac{R}{a}\right)^{\textstyle{{}^{5}}}\,\frac{k_{2}}{Q}\;+\;\frac{M\,}{\,M^{\,\prime}}\,\left(\frac{R^{\;\prime}}{a}\right)^{\textstyle{{}^{5}}}\,\frac{k_{2}^{\,\prime}}{Q^{\,\prime}}\right]~{}
(54)
+O(e2)+O(i2)+O(i2).\displaystyle\;+\;O(e^{2})\;+\;O(i^{2})\,+\,O({i^{\,\prime\;}}^{2})~{}_{\textstyle{{}_{\textstyle.}}}\quad

This is in agreement with Lainey et al. (2012, Eqn (A1)) but differs from the corresponding formulae in some other works.

When both partners satisfy the Constant Time Lag (CTL) model (i.e., when both K2\,K_{2}\, and K2\,K_{2}^{\,\prime}\, are linear in the tidal mode), expression (53) becomes

(dedt)l=2(CTL)=34ne[MM(Ra)511θ˙ 18nθ˙nK2(2n2θ˙){}^{\textstyle{{}^{(CTL)}}}\left(\frac{de}{dt}\right)_{l=2}=\;\frac{3}{4}\,n\,e\,\left[\frac{\,M^{\,\prime}}{M\,}\,\left(\frac{R}{a}\right)^{\textstyle{{}^{5}}}\,\frac{11\;\dot{\theta}\;-\;18\;n}{\dot{\theta}\;-\;n}\;K_{2}(2n-2\dot{\theta})\right.~{}
+MM(Ra)511θ˙ 18nθ˙nK2(2n2θ˙)]\displaystyle\left.\;+\;\frac{M\,}{\,M^{\,\prime}}\,\left(\frac{R^{\;\prime}}{a}\right)^{\textstyle{{}^{5}}}\,\frac{11\;\dot{\theta}^{\,\prime}\;-\;18\;n}{\dot{\theta}^{\,\prime}\;-\;n}\;K_{2}^{\,\prime}(2n-2\dot{\theta}^{\,\prime})\right] (55)
+O(e2)+O(i2)+O(i2).\displaystyle\;+\;O(e^{2})\;+\;O(i^{2})\,+\,O({i^{\,\prime\;}}^{2})~{}~{}_{\textstyle{{}_{\textstyle.}}}\quad

This agrees with Hut (1981, Eqn 10) and Emelyanov (2018, Eqn 19), but not with Kaula (1964, Eqn 46) who neglected a factor of (M+M)/M\,(M+M^{\,\prime})/M\, and lost the factor of 4 in the denominator in the second line of his expression.

We observe that within the CTL model the sign of a partner’s input coincides with Sign(18n11θ˙)\operatorname{Sign}\,(18n-11\dot{\theta}). A body is mitigating the eccentricity ee when spinning swiftly (θ˙/n>18/11\nobreak\hskip 1.1pt\nobreak\dot{\theta}/n>18/11), and is boosting ee when spinning slowly (θ˙/n<18/11\nobreak\hskip 1.1pt\nobreak\dot{\theta}/n<18/11). This is in contrast to the CPL case, equation (54), where each partner, whatever its spin, is always working to increase ee.

The sensitivity of de/dtde/dt to the frequency-dependencies of K2K_{2} and K2K_{2}^{\,\prime} indicates that, even before one of the partners synchronises its spin, the eccentricity rate may have, in principle, been negative. However, for hot semimolten bodies (as well as for near-rubble ones) the rheology is not very different from CTL, because for such bodies interpeak interval in Figure B1 is broad and includes the modes involved. So the tides in such a body, on approach to synchronism (θ˙/n<18/11\nobreak\hskip 1.1pt\nobreak\dot{\theta}/n<18/11), are working to boost the eccentricity.

As we saw in Appendix D, both bodies’ rotation synchronises quickly, whereafter the tides in both bodies start working to reduce the eccentricity.

After both partners are synchronised (θ˙=θ˙=n\dot{\theta}=\dot{\theta}^{\,\prime}=n), the terms with K2(2n2θ˙)\nobreak\hskip 1.1pt\nobreak K_{2}(2n-2\dot{\theta})\nobreak\hskip 1.1pt\nobreak and K2(2n2θ˙)\nobreak\hskip 1.1pt\nobreak K^{\,\prime}_{2}(2n-2\dot{\theta}^{\,\prime})\nobreak\hskip 1.1pt\nobreak in formula (53) vanish, and we end up with

(dedt)l=2=\displaystyle\left(\frac{de}{dt}\right)_{l=2}= \displaystyle- 212neMM(Ra)5K2(n)\displaystyle\frac{21}{2}\,n\,e\,\frac{\,M^{\,\prime}}{M}\,\left(\frac{R}{a}\right)^{\textstyle{{}^{5}}}\,K_{2}(n)~{}
\displaystyle- 212neMM(Ra)5K2(n)+O(e2)+O(i2)+O(i2),\displaystyle\frac{21}{2}\,n\,e\,\frac{M}{\,M^{\,\prime}}\,\left(\frac{R^{\,\prime}}{a}\right)^{\textstyle{{}^{5}}}\,K_{2}^{\,\prime}(n)\;+\;O(e^{2})\;+\,O(i^{2})\;+\,O({i^{\,\prime\;}}^{2})~{}~{}_{\textstyle{{}_{\textstyle,}}}\qquad
where we took into consideration that both K2\nobreak\hskip 1.1pt\nobreak K_{2}\nobreak\hskip 1.1pt\nobreak and K2\nobreak\hskip 1.1pt\nobreak K^{\,\prime}_{2}\nobreak\hskip 1.1pt\nobreak are odd functions.

Here K2(n)=k2(n)/Q(n)\nobreak\hskip 1.1pt\nobreak K_{2}(n)=k_{2}(n)/Q(n)\nobreak\hskip 1.1pt\nobreak and K2=k2(n)/Q(n)\nobreak\hskip 1.1pt\nobreak K^{\,\prime}_{2}=k_{2}^{\prime}(n)/Q^{\,\prime}(n)\nobreak\hskip 1.1pt\nobreak. Therefore,

(dedt)l=2=\displaystyle\left(\frac{de}{dt}\right)_{l=2}= \displaystyle- 212neMM(Ra)5k2Q\displaystyle\frac{21}{2}\,n\,e\,\frac{\,M^{\,\prime}}{M}\,\left(\frac{R}{a}\right)^{\textstyle{{}^{5}}}\,\frac{k_{2}}{Q}~{}
\displaystyle- 212neMM(Ra)5k2Q+O(e2)+O(i2)+O(i2),\displaystyle\frac{21}{2}\,n\,e\,\frac{M}{\,M^{\,\prime}}\,\left(\frac{R^{\,\prime}}{a}\right)^{\textstyle{{}^{5}}}\,\frac{k_{2}^{\prime}}{Q^{\,\prime}}\;+\;O(e^{2})\;+\,O(i^{2})\;+\,O({i^{\,\prime\;}}^{2})~{}~{}_{\textstyle{{}_{\textstyle,}}}\qquad

the tidal parameters’ values taken at the frequency nn.

To evaluate the circularisation timescale τe\tau_{e}, we need to know which term in the above expression is leading. For M/M=0.03M^{\,\prime}/M=0.03, the values of the factors MM(Ra)5\frac{\textstyle M}{\textstyle\,M^{\,\prime}}\,\left(\frac{\textstyle R^{\,\prime}}{\textstyle a}\right)^{\textstyle{{}^{5}}} and MM(Ra)5\frac{\textstyle M^{\,\prime}}{\textstyle\,M}\,\left(\frac{\textstyle R}{\textstyle a}\right)^{\textstyle{{}^{5}}} are comparable. Assuming that the planet is cooling down slower than the moon, i.e., that k2/Q>k2/Qk_{2}/Q\nobreak\hskip 1.1pt\nobreak>\nobreak\hskip 1.1pt\nobreak k_{2}^{\prime}/Q^{\,\prime}, we conclude that the first term in expression (LABEL:57) is dominant. Accordingly,

τe=221Qk2MM1n(aR)5.\displaystyle\tau_{e}\nobreak\hskip 1.1pt\nobreak=\;\frac{2}{21}\;\frac{Q}{k_{2}}\;\frac{M}{M^{\,\prime}}\;\frac{1}{n}\nobreak\hskip 1.1pt\nobreak\left(\frac{a}{R}\right)^{5}\;\,. (57)

Comparing this with the expression (45) for planet despinning timescale τp\tau_{p}, we find that

τeτp=221MM(aR)23×103(aR)2.\displaystyle\frac{\tau_{e}}{\tau_{p}}\,=\,\frac{2}{21}\,\frac{M^{\,\prime}}{M}\left(\frac{a}{R}\right)^{\textstyle{{}^{2}}}\approx 3\times 10^{-3}\left(\frac{a}{R}\right)^{\textstyle{{}^{2}}}\,\;. (58)

Although in realistic situations the right-hand side of this formula assumes values between 0.10.1 and 0.30.3, this in no way implies that the circularisation of orbit is attained before the planet gets despun. Recall that expression (57) becomes valid only after the planet’s synchronisation. Prior to that, a competition had been taking place: while the tides in the already synchronised moon were working to reduce the value of ee, the tides in the still nonsynchronous planet were boosting ee. So the circularisation process cannot even begin before the synchronism is reached.

After the synchronism is attained, the subsequent circularisation never becomes complete, for two reasons. One is the influence of the triaxial figure of Mars on the moon’s orbit. This influence is averaged out if the synchronism is achieved far from such a resonance, but becomes a great booster of the eccentricity if the synchronous orbit is resonant or near-resonant. E.g. for Phobos, the eccentricity jumps Δe\Delta e due to the 2:1 and 3:1 resonances with Mars’ figure, at aPhobos=3.8Ra_{\rm{{}_{Phobos}}}=3.8\nobreak\hskip 1.1pt\nobreak R and aPhobos=2.9Ra_{\rm{{}_{Phobos}}}=2.9\nobreak\hskip 1.1pt\nobreak R\nobreak\hskip 1.1pt\nobreak, were 0.032 and 0.0020.002\nobreak\hskip 1.1pt\nobreak, correspondingly (Bagheri et al., 2021; Yoder, 1982).

The other reason is the Sun’s gravity pull. The role of the Sun would have been especially strong, had the moon been formed or captured below the 2:1 MMR with the Sun at a=3.2Ra=3.2R. The moon’s recession through this MMR would have produced a jump Δe=0.0085\Delta e=0.0085\nobreak\hskip 1.1pt\nobreak (Bagheri et al., 2021; Yoder, 1982).

[ Mind misprints in the upper sentence on page 2 of Bagheri et al. (2021). The words  “…and a 1:1 resonance with the Sun at a=2.6RMarsa=2.6R_{\rm{{}_{Mars}}} when its pericentre rate equals the Martian mean motion”  must be changed to:  “…and a 2:1 resonance with the Sun at a=3.2RMarsa=3.2R_{\rm{{}_{Mars}}} when its pericentre rate equals one half of the Martian mean motion.” Accordingly, in the third sentence from top, Δe1:1Sun=0.0085\Delta e^{\rm{{}^{Sun}}}_{\rm{{}_{1:1}}}=0.0085 must be changed to Δe2:1Sun=0.0085\Delta e^{\rm{{}^{Sun}}}_{\rm{{}_{2:1}}}=0.0085\nobreak\hskip 1.1pt\nobreak. ]

Appendix F Could Mars have ever stayed in a higher spin-orbit resonance with Nerio?

While a comprehensive analysis of Mars’ synchronisation by the moon Nerio would amount to a separate project, we here explain in short why entrapment of a hot Mars into a higher spin-orbit resonance was impossible, even for a high initial eccentricity. Even if a not-yet-molten nascent Mars had somehow been trapped into a higher spin state, it was pushed out of that state towards synchronism after reaching the magma-ocean state.

As mentioned in Section 7.4, a moon formed in situ, or produced by collision, or captured in the disk has a low initial eccentricity, wherefore neither of the partners end up in a higher-than-synchronous rotation state.

Refer to caption
Figure F1: . The angular acceleration of a tidally perturbed rotator, as a function of its spin rate θ˙\dot{\theta} divided by the mean motion nn\,. The smaller term (vanishing in the 3:2 spin-orbit resonance) is superimposed on the main, semidiurnal term. For sufficiently solid planets (i.e., for high mean viscosity values), the peaks are sharp, and the semidiurnal kink is squeezed toward the vertical axis. Its negative-valued right tail is, in the 3:2 resonance, overpowered by the small kink. The upper tip of the kink is residing above the horizontal axis. This creates a tidal trap: the planet is rotating in a stable equilibrium, because small deviations in θ˙/n\dot{\theta}/n render a torque that is always restoring the system back to the 3:2 spin state. For a hot planet (one of low mean viscosity), the peaks of the large kink spread broadly, the small kink “sinks”, and the tidal trap is no more.  (From Noyelles et al. 2014)

Assume that, despite this, the eccentricity somehow acquired a high initial value sufficient for Mars to get stuck in a higher spin state. To understand if this entrapment could happen, we resort to Figure F1. Borrowed from Noyelles et al. (2014), it depicts the dependence of the tidal torque (to be precise, of the angular acceleration) as a function of the spin rate θ˙\dot{\theta} divided by the mean motion nn\nobreak\hskip 1.1pt\nobreak. In the plot, a secondary term (one vanishing in the 3:2 spin-orbit resonance) is superimposed on the main, semidiurnal term. The small kink overpowers the bias and produces a trap near the 3:2 resonance. In this trap, the rotator is spinning in a stable equilibrium, because small deviations in θ˙/n\dot{\theta}/n render a torque that is always restoring, a topic discussed at length in Noyelles et al. (2014).

It is important to spell out the exact reason why the magnitude of small kink can exceed the negative bias produced by the right tail of the semidiurnal kink. In the case of, e.g. Mercury, the reason is that Mercury is a solid planet. Had it been several times closer to the Sun, tidal heating would have put it into a semimolten state, with a much lower value of the mean viscosity of its mantle. The peaks of the semidiurnal torque would then have spread greatly (equation (41) in Appendix B), while the magnitudes of the involved terms would not have changed (equation (42) in that appendix). The so widely spread big kink would have overpowered the small ones, and there would be no traps in higher-order spin-orbit resonances any more. In this situation, Mercury’s capture into the 3:2 resonance would have been temporary; the planet would have been trapped, and would have left the resonance after getting tidally overheated. This issue was later addressed in detail by Makarov (2015).

Now suppose that owing to an unlikely but speculatively possible high value of the initial eccentricity, a nascent and not yet molten Mars went into a higher (say, 3:2) spin-orbit state with Nerio. At this point, the small kink in the plot was having its tip above the horizontal axis. As Mars was warming up and approaching the magma-ocean stage, its mean viscosity value was rapidly decreasing. Consequently, the peaks of the semidiurnal kink were spreading wide, leaving the small kinks no chance to keep the trap functioning. The small kink would lose the competition to the negative-valued tail of the main kink, and the rotator would leave the higher spin state, to continue its spin-down towards synchronism. À propos, tidal overheating is also the reason why close-in planets with appreciable eccentricities easily get caught into higher spin-orbit states — and then leave these states. This is what happened, e.g. with the planets bb, dd, and ee of TRAPPIST-1 (Makarov et al., 2018).

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