SPEED LIMIT ON NEPTUNE MIGRATION IMPOSED BY SATURN TILTING

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Published 2009 August 11 © 2009. The American Astronomical Society. All rights reserved.
, , Citation Gwenaël Boué et al 2009 ApJ 702 L19 DOI 10.1088/0004-637X/702/1/L19

This article is corrected by 2009 ApJ 705 L99

1538-4357/702/1/L19

ABSTRACT

In this Letter, we give new constraints on planet migration. They were obtained under the assumption that Saturn's current obliquity is due to a capture in resonance with Neptune's ascending node. If planet migration is too fast, then Saturn crosses the resonance without being captured and it keeps a small obliquity. This scenario thus gives a lower limit on the migration timescale τ. We found that this boundary depends strongly on Neptune's initial inclination. For two different migration types, we found that τ should be at least greater than 7 Myr. This limit increases rapidly as Neptune's initial inclination decreases from 10° to 1°. We also give an algorithm to know if Saturn can be tilted for any migration law.

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1. INTRODUCTION

It is now well accepted that the solar system was more compact after the protoplanetary gas disk dissipated. Then planets migrated due to interactions with the primordial planetesimal belt. The Nice model (Gomes et al. 2005; Tsiganis et al. 2005; Morbidelli et al. 2005) gives a unified scenario of this planetary migration, but it is still not fully constrained. For example, the Nice model allowed two possible classes of late evolution (Nesvorný et al. 2007). In the first one, called "class MA," Neptune is scattered to 22–25 AU and reaches its final orbit by slowly migrating over more than 5 AU. In the second class, labeled "DE," Neptune is placed to its current orbital distance with large eccentricity ≈0.3 and then slowly circularizes. Besides, the Nice model does not constrain inclinations, and the timescale of this late evolution is uncertain. Nevertheless, constraints on the migration timescale were obtained from the distribution of the Kuiper belt on the one hand (Murray-Clay & Chiang 2005), and from the distribution of the main asteroid belt on the other (Minton & Malhotra 2009). They both assumed an MA migration type without long-term evolution of eccentricities and inclinations. The former obtained a migration timescale τ between 1 and 10 Myr, and the latter found τ ≲ 0.5 Myr.

In this Letter, we aim at giving new constraints based on Saturn tilting (Ward & Hamilton 2004; Hamilton & Ward 2004). According to Ward and Hamilton, Saturn's large obliquity, epsilon = 26fdg73919 (Helled et al. 2009), is due to a resonance capture between its spin axis and Neptune's orbit. Given the large uncertainties on Saturn's precession rate $-0\farcs 75\pm 0\farcs 21\;{\rm {yr}}^{-1}$ (Ward & Hamilton 2004), the more accurate regression of Neptune's orbit plane s8 = −0farcs692 yr−1 (Laskar et al. 2004) is indeed included in the errorbars. Ward & Hamilton (2004) assume that today the two frequencies are equal. In their scenario, the norm of the frequency of Neptune's ascending node was initially larger, and then it captured Saturn's spin axis as it decreased due to Neptune's migration and/or the dissipation of the planetesimal disk (Ward & Canup 2006). In their numerical model, they took a quasiperiodic model of the solar system and forced an exponential evolution of the frequency s8. Here, we show that Saturn can tilt in both migration classes, and that it gives a lower limit on the migration timescale. This limit depends on Neptune's initial inclination.

A recent paper by Helled et al. (2009) seems to contradict Ward and Hamilton's scenario. It gives a new estimate of Saturn's precession rate −0farcs7542 ± 0farcs0002 yr−1 that is incompatible with a resonance with s8. We show that with this value, Saturn can still evolve to its current state but that it is very unlikely. We discuss this result in our conclusion.

2. SPIN AXIS EVOLUTION

Here we recall the equations of motion of a planet axis and give the current dynamical state of Saturn's spin axis. The evolution of the spin axis w of a planet in a fixed reference frame (i, j, k), where k is the direction of the total orbital angular momentum, is given by

Equation (1)

where n = t(nx, ny, nz) is the normal to the orbit, and α is the precession constant. Without planetary perturbations, n is fixed and the spin axis w precesses uniformly around n with constant obliquity cos epsilon = n · w. However, in a multiplanetary system, n evolves due to secular interactions. The long-term evolution of n can be approximated by a quasiperiodic expression

Equation (2)

where the νk (sorted with increasing amplitudes Ik) are combinations of the fundamental frequencies gj, sj (Laskar 1990). For Saturn, ν2 = s8 = −0farcs692 yr−1 and I2 = 0fdg064. As the other terms have only very weak effects on the behavior of Saturn's spin axis (Hamilton & Ward 2004), one can retain this single term in the orbital precession, which makes the problem integrable (Colombo 1966; Henrard & Murigande 1987). The associated autonomous Hamiltonian, written in a moving reference frame related to the orbital plane, reads

Equation (3)

with now $\mathbf {k}={}^t{(I,0,\sqrt{1-I^2})}$ and n = t(0, 0, 1). The equation of motion, obtained from ${d\mathbf {w}}/{dt}={\boldsymbol{\nabla }}_{\mathbf {w}}{H}\times \mathbf {w}$, is

Equation (4)

This system possesses four relative equilibriums named Cassini states for which the three axes w, n, and k are collinear, and a separatrix delineating three zones in the phase space (see Figure 1). Hereafter, we label the three zones after the Cassini state they contain. Saturn's spin axis coordinates in the orbital frame are

Figure 1.

Figure 1. Projection of the spin axis w (5) in the orbital frame (in abscissae sin epsiloncos ψ, in ordinate sin epsilonsin ψ). (a) Case I with α = 0farcs845 yr−1 (Helled et al. 2009). (b) Case II with α = 0farcs775 yr−1 (Ward & Hamilton 2004). Cassini state 3 corresponds to a retrograde rotation of Saturn and is not represented in these figures. The current position of Saturn's spin axis is represented by a large filled circle. The small filled circles are Cassini states and the curves are energy contours. The bold curve is the separatrix that delineates the libration area in gray.

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Equation (5)

with epsilon = 26fdg73919 (Helled et al. 2009) and ψ = −31° (Hamilton & Ward 2004). As ψ ≠ 0, the system is not in a Cassini state. Given the coordinates of w, if −αcos epsilon ∈ [ − 0.730, − 0.666] ''yr−1 (Ward & Hamilton 2004) then Saturn's spin axis is in resonance around Cassini state 2 with a libration amplitude larger than 31° (see Figure 1(b)), else it is in circulation around either Cassini state 1 (see Figure 1(a)) or Cassini state 3. Literature gives three different values of Saturn's precession rate. Two of them, −0farcs74 ± 0farcs7 yr−1 (French et al. 1993) and −0farcs75 ± 0farcs21 yr−1 (Ward & Hamilton 2004), are compatible with a libration in zone 2, whereas the third one, −0farcs7542 ± 0farcs0002 yr−1 (Helled et al. 2009), constrains Saturn's axis to circulate in zone 1. In the following, we study these two cases. In Case I, we use the precession constant given by Helled et al. (2009), and in Case II we set α such that −αcos epsilon = s8 = −0farcs692 yr−1. In our numerical integrations detailed below, we take into account the dependences of α in Saturn's semimajor axis and eccentricity.

3. ORBITAL EVOLUTION

We integrate the secular equations of motion derived from the Hamiltonian of Laskar & Robutel (1995) written up to degree 4 in inclinations and eccentricities. In order to fit to the present value of s8 (Laskar et al. 2004), a small constant offset δs8 = −0farcs00342 yr−1 is added in the model. This offset was obtained by frequency analysis (Laskar 1990) of our analytical model (Table 1). For the class "MA," we consider only the last 3 AU migration of Neptune. When Neptune was closer to the Sun, the frequency s8 was too large to have any effect on Saturn's axis. Migration is simulated by an additional force leading to the following exponential law,

Table 1. Secular Frequencies Associated with the Precession of the Ascending Nodes

Frequency Laskar et al. (2004) Secular integration
s5 −0.000 −0.000
s6 −26.348 −26.569
s7 −2.993 −2.996
s8 −0.692 −0.689

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Equation (6)

with Δa = +0.1, − 0.3, − 1.3, − 3 AU respectively for Jupiter, Saturn, Uranus, and Neptune. It is scaled from Minton & Malhotra (2009) and it is in agreement with the full integration of Tsiganis et al. (2005). In the same way, for the class "DE" we apply an external force that gives a long-term exponential evolution of Neptune eccentricity starting at e0 = 0.3 and finishing at its current value. For both classes, we did integrations with constant Neptune inclination, and others with an exponential damping with the same τ. For each value of τ, an integration in the past is done to obtain initial conditions for the orbital coordinates. Saturn's initial obliquity is then set to epsilon0 = 1.5°.

We now look at the effect of the dissipation of the remaining primordial planetesimal belt. Following a suggestion of A. Morbidelli (2009, private communication), the mass mK of the planetesimal belt in the class "MA" is estimated by energy conservation as follows. Initially, planetesimals are distributed following Morbidelli et al. (2004, Figure 1) and during Neptune migration, planetesimals move from their initial position to Uranus' orbit. This leads to mK = 1.7 ± 0.1M. During planet migration with a planetesimal disk, we force an exponential decrease of the planetesimal belt mass with the same timescale as the semimajor axis one. To first order, the averaged effect of a planetesimal of mass mi and semimajor axis ai on Neptune's nodal precession rate is

Equation (7)

with nN and aN being, respectively, Neptune mean motion and semimajor axis, and m0 the mass of the Sun. We model the planetesimal belt by a single annulus with semimajor axis aK such that

Equation (8)

Using the mass distribution of Morbidelli et al. (2004), we found ak = 60 ±  5AU. We run numerical integrations with and without a 2 Earth mass primordial planetesimal belt and found that the constraints on the migration timescales were unchanged. In the following, we give only the results of our integrations without a planetesimal disk.

4. RESULTS

In Case I, Saturn's spin axis circulates around Cassini state 1 with a large obliquity (Figure 1(a)). To show whether it is compatible with the Ward & Hamilton (2004) scenario or not, we did several numerical integrations without long-term evolution of Neptune inclination and enumerated those ending in zone 1 with an obliquity larger than or equal to 26.73919°. We first considered the class MA of the Nice model and varied the migration timescale τ from 100 Myr to 600 Myr every 10 Myr. Then, for each value of τ, we searched the range of the initial precession angle ψ for which the final state corresponds to our criterion. We found only three values for τ satisfying the criterion: τ ∈ {170, 180, 190} Myr. In each case, the range of possible values for ψ is extremely small $\Delta _\psi \lesssim 10^{-5}\deg$ (Figure 2, Ia, Ib, Ic). Thus assuming an equiprobable initial phase, the probability to find Saturn in its current state through this mechanism is less than 3 × 10−8 for any of the three selected τ. With a DE migration type, the widths of the initial longitude intervals Δψ are identical. The only changes are in the values of the migration timescale τ leading to the large obliquity circulation state: τ ∈ {150, 260, 290, 310, 320} Myr. We discuss the implications of these results in the conclusion.

Figure 2.

Figure 2. Results for the MA type migration. Projection of Saturn's spin axis on the invariant plane in a frame rotating at Neptune regression frequency (in abscisse sin θcos(ϕ − Ω), in ordinate sin θsin(ϕ − Ω)) (see Equation (9)). The filled circle represents its current position. Subfigures Ia, Ib, and Ic, Case I with τ = 180 Myr and ψ = 108fdg674, 108fdg675 469, 108fdg675 475. Subfigures IIa, IIb, and IIc, Case II with τ = 20, 200, 300 Myr and ψ = 0°.

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In Case II, Saturn's spin axis is presently in resonance with Neptune's ascending node. In that case, planet migration must be slow enough for the capture to occur, but if it is too slow, then the evolution becomes adiabatic and the libration amplitude is too small (less than 31°; Figure 2, IIc). This latter constraint disappears if the precapture obliquity is larger than 4fdg5 (Ward & Hamilton 2004). We performed 2100 integrations for each of the two migration types MA and DE, τ going from 10 to 600 Myr every 10 Myr and ψ between 0° and 350° every 10°. The results are summarized in Figure 3, MA type in gray and DE type in black. Probabilities are now significant and reach 1 for a few timescales. We see clear lower limits, τ ⩾ 90 Myr (resp. τ ⩾ 170 Myr) for the MA (resp. DE) migration type. The difference in the results between the two Nice model classes comes mainly from the different dependence of the semimajor axis and the eccentricity on Neptune's regression frequency. In all these integrations, Neptune's inclination does not undergo long-term evolution. However, the amplitude I2 of Saturn orbital quasiperiodic motion (2) is proportional to Neptune inclination. In Section 5, we show that the higher the inclination amplitude is, the faster a planet can be tilted. We thus studied the minimum timescale, for which Saturn's axis ends in zone 2 with a libration amplitude larger than 31°, as a function of Neptune's initial inclination (Figure 4, bold curves). In both migration classes, τmin decreases rapidly to ≈20 Myr when Neptune's initial inclination increases to 4° and then it decreases slowly down to ≈7 Myr when Neptune's inclination goes to 10°.

Figure 3.

Figure 3. Probability that Saturn librates in zone 2 with an amplitude larger than 31° as a function of the migration timescale τ in Case II. MA migration type in gray and DE migration type in black.

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Figure 4.

Figure 4. Minimal migration timescale as a function of Neptune's initial inclination for both migration types: MA (solid line) and DE (dashed line). Bold curves are results of numerical integrations. Thin curves were obtained by the algorithm described at the end of Section 5.

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5. FASTEST TILTING

In this section, we compute analytically the minimal time required to tilt a planet as a function of its inclination I(t). We give also an algorithm to check whether Saturn can be tilted or not for a given migration.

We call θ the inclination of a planet equator relative to the invariant plane. As Saturn current inclination is small relative to its obliquity epsilon, the two angles θ and epsilon are similar. Let Φ and Ω be the longitude of the ascending node of the equator and of the orbit in the invariant plane. We have

Equation (9)

and

Equation (10)

Thus, from (1),

Equation (11)

where γ = tan θtan I can vary from 0 to infinity depending on the value of the obliquity. We now choose Ω that maximizes this time derivative as a function of I and θ. Doing so, we ensure that it is not possible to have a faster evolution of the equator inclination θ. This leads to

Equation (12)

Substituting this expression in (11) gives the maximal speed Θmax such that dθ/dt ⩽ Θmax

Equation (13)

After some calculus, it can be shown that Θmax is an increasing function of tan I. Thus, if the only constraint on the orbit inclination amplitude is an upper limit Imax < π/2, the fastest evolution is obtained for I = Imax. In two asymptotic cases, the expressions of Θmax are simpler. For I ≪ |π/2 − θ| or θ ≪ |π/2 − I|, we have |γ| ≪ 1 and thus

Equation (14)

In the other case, if |θ − π/2| ≪ I or |I − π/2| ≪ θ, the parameter γ is arbitrarily large and (13) becomes

Equation (15)

Using the approximation for small angles |γ| ≪ 1 (14), the minimum time tmin required to bring θ from 0 to θend at constant inclination amplitude I is

Equation (16)

In Saturn's case, the amplitude of the mode responsible for the tilt is I2. Whenever Neptune's inclination is less than 10°, I2 remains below 0fdg9, γ ⩽ 8 × 10−3 and Expressions (14), (16) are valid. This minimum time tmin decreases with the inclination amplitude I. For example, with I = I2 = 0.064°, Equation (16) gives tmin = 105 Myr in Case I and tmin = 115 Myr in Case 2.

From this study, it is possible to check whether Saturn's axis can be tilted or not for a given migration. Let θ2 be the value of θ at the Cassini state 2. θ2 and its time derivative $\Theta _2=\dot{\theta }_2$ are functions of orbital parameters through I(t), ν(t) = s8(t) and α(t). During a tilt, θ oscillates around the increasing θ2 and $\Theta =\dot{\theta }$ reads

Equation (17)

where A and φ are, respectively, the libration amplitude and a phase, and ωlib is the libration amplitude given by Hamilton & Ward (2004)

Equation (18)

For a given migration, Saturn's axis can tilt if and only if there exist A and ϕ such that Θ ⩽ Θmax (14 and 17) during all the evolution. Replacing θ by θ2 in (14 and 18), one obtains a criterion that depends only on orbital parameters. We applied this criterion on the systems studied in Section 4. For each value of Neptune's initial inclination, we integrated once the system with a given τ. Then, we rescaled the derivatives Θ for different value of τ until the criterion is verified. The resulting values of τmin are displayed in Figure (4, thin curves).

6. CONCLUSIONS

First of all, we see that the Helled et al. (2009) precession constant is incompatible with the Ward & Hamilton (2004) scenario. This is a robust result. Helled et al. (2009) obtained Saturn's precession constant from an empirical model of its internal structure. They used Saturn mass, radius, and gravitational coefficients J2, J4, and J6 to fit a density profile represented by a sixth-degree polynomial. From this density profile they derived the normalized axial moment of inertia γ directly related to the precession constant. Our results suggest, rather, considering γ as an additional independent parameter to better constrain Saturn's interior. If Saturn is actually in libration in zone 2 then 0.2257 < γ < 0.2438 (Ward & Hamilton 2004).

Assuming the Hamilton & Ward (2004) precession constant, Saturn's spin axis is likely to evolve toward a libration in zone 2 whatever the migration class is as long as the timescale τ is sufficiently large. We found a strong dependence between the minimum timescale τmin and Neptune's inclination. Thus, an external constraint on the speed limit of Neptune migration may also constrain its inclination. For instance, the upper boundary obtained by Murray-Clay & Chiang (2005) is τ ⩽ 10 Myr. In that case, our results show that under the hypothesis of Section 3, the initial inclination of Neptune's orbit must have been larger than 7°. On the other side, in all our studied cases, the minimum timescale must be at least greater than 7 Myr, whereas Minton & Malhotra (2009) found τ ≲ 0.5 Myr. This contradiction may be raised if one considers different evolution laws for the semimajor axes, eccentricities, and/or inclinations. In that scope, we have given in Section 5 an algorithm to know if Saturn can be tilted for any migration law.

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10.1088/0004-637X/702/1/L19