Dynamical Evidence for Phobos and Deimos As Remnants of a Disrupted Common Progenitor
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LETTERS https://doi.org/10.1038/s41550-021-01306-2 Dynamical evidence for Phobos and Deimos as remnants of a disrupted common progenitor Amirhossein Bagheri 1 ✉ , Amir Khan 1,2, Michael Efroimsky 3, Mikhail Kruglyakov 1 and Domenico Giardini1 The origin of the Martian moons, Phobos and Deimos, remains on their dynamical figures, which enhances tidal dissipation16. elusive. While the morphology and their cratered surfaces This effect is more pronounced for Phobos than Deimos, owing to suggest an asteroidal origin1–3, capture has been questioned Phobos’s higher eccentricity and triaxiality. All properties are sum- because of potential dynamical difficulties in achieving the marized in Supplementary Table 1. current near-circular, near-equatorial orbits4,5. To circumvent For a non-librating planet hosting a satellite librating about a this, in situ formation models have been proposed as alterna- 1:1 spin–orbit resonance, the tidal rates of the semi-major axis and tives6–9. Yet, explaining the present location of the moons on eccentricity can be written in terms of the mean motion (n), satellite opposite sides of the synchronous radius, their small sizes and libration amplitude ( ), and planet and satellite quality functions 2 A apparent compositional differences with Mars has proved (K k /Q and K0 k0=I Q0), masses (M and M0), spin rates (θ_ and θ_ 0) l = l l l ¼ l l challenging. Here, we combine geophysical and tidal-evolution and radii (R andI R′): I I modelling of a Mars–satellite system to propose that Phobos and Deimos originated from disintegration of a common 5 da G M M0 M0 R progenitor that was possibly formed in situ. We show that ð þ Þ Kl; θ_; n; e dt ¼ na2 M a ½Fð Þ 1 tidal dissipation within a Mars–satellite system, enhanced ð Þ by the physical libration of the satellite, circularizes the K0; θ_ 0; n; e K0; n; e; ; þFð l Þ þ Gð l AÞ post-disrupted eccentric orbits in <2.7 Gyr and makes Phobos descend to its present orbit from its point of origin close to or above the synchronous orbit. Our estimate for Phobos’s 5 de G M M0 M0 R maximal tidal lifetime is considerably less than the age of ð þ Þ Kl; θ_; n; e dt ¼ na3 M a ½Lð Þ 2 Mars, indicating that it is unlikely to have originated alongside ð Þ _ 0 Mars. Deimos initially moved inwards, but never transcended Kl0; θ ; n; e Kl0; n; e; ; the co-rotation radius because of insufficient eccentricity and þLð Þ þ Hð AÞ therefore insufficient tidal dissipation. Whereas Deimos is where G is the gravitational constant, unprimed and primed vari- very slowly receding from Mars, Phobos will continue to spiral ables refer to those of the planet and the satellite, respectively, and towards and either impact with Mars or become tidally dis- the terms in the square brackets represent the dissipation due to the _ rupted on reaching the Roche limit in ≲39 Myr. main tides on the planet ( Kl; θ; n; e and Kl; θ_; n; e ), the main Fð_ Þ Lð_ Þ Tidal interactions between celestial bodies result in energy dis- tides on the satellite ( K0I; θ; n; e and K0I; θ0; n; e ), and satellite Fð l Þ Lð l Þ sipation and drive systems towards equilibrium states, in part by libration ( K0; n; e; I and K0; n; e; I ). Inclination (i) of a sat- Gð l AÞ Hð l AÞ pushing eccentricity and obliquity to zero and spin rates towards ellite orbit onI Mars’s equator isI governed by synchronization. This evolution is governed by the dissipative prop- 5 erties (including the frequency-scaling laws) of both the planet and di M0 R n sin i Kl; θ_; n; i; e ; 3 the moons10. To determine the orbital history of a Mars–satellite dt ¼ M a ½Ið Þ ð Þ system, we use up-to-date geophysical data for Mars and its satel- lites, including Martian seismic data from the currently operating where the term in square brackets refers to the main tides on the InSight mission11,12, laboratory-based viscoelastic models13 describ- planet. Detailed expressions for the functions , , , and F G L H I ing Mars’s rheology14, and a comprehensive tidal-evolution model are given in Methods. To ensure precision, theI functionsI I were based on the extended Darwin–Kaula theory of tides15, including expanded to order 18 in eccentricity. Equations (1)–(3) were inte- the contribution from a satellite’s physical libration in longitude. grated backwards in time using a Runge–Kutta explicit iterative We consider Mars–Phobos and Mars–Deimos as separate orbital solver. We also track the planetocentric distances (Rp) of the two 2 systems and integrate the semi-major axis (a), eccentricity (e), satellites, given by Rp a 1 e = 1 e cos f ; where f is the true ¼ ðÞ� ð þ Þ Mars’s spin rate (θ_) and inclinations of the satellites (i) backwards anomaly. R assumesI values in the interval a 1 e ≤Rp ≤a 1 e , p ðÞ� ðÞþ in time (t), starting from the current configuration. Our tidal model so a satellite always resides between the twoI circles. We shall com- includes degree-2 and -3 inputs, because of the proximity of the pare the minimal distance of Deimos with the maximal distance of moons to Mars. Although Phobos and Deimos are tidally locked, Phobos, and shall be particularly interested in the case where mini- Deimos Phobos their uniform rotational motion is modified by physical libration mal Rp ≤ maximal Rp (Supplementary Section 2), that is, arising from the time-varying gravitational torque exerted by Mars whereI the orbits of the moonsI intersect. 1Institute of Geophysics, ETH Zürich, Zurich, Switzerland. 2Physik-Institut, University of Zürich, Zurich, Switzerland. 3US Naval Observatory, Washington DC, USA. ✉e-mail: [email protected] NATURE ASTRONOMY | www.nature.com/natureastronomy LETTERS NATURE ASTRONOMY a During the orbital evolution, Phobos undergoes 2:1 and 3:1 spin– 7.5 orbit resonances with Mars’s figure at a = 3.8RMars and a = 2.9RMars, Mars 7.0 R respectively, where RMars is the mean radius of Mars, and a 1:1 reso- 6.5 nance with the Sun at a = 2.6RMars when its pericentre rate equals the 6.0 Martian mean motion. Deimos is affected by a 2:1 mean motion resonance with Phobos. These resonances result in rapid eccentric- 5.5 17 Mars Mars 5.0 ity changes Δe (ref. ). For Phobos, Δe2:1 0:032, Δe3:1 0:002 –4 Sun ¼Phobos ¼ Deimos k2/Q2 = 2.0 × 10 and Δe 0:0085, whereas for Deimos,I Δe I0:002. Finally, 4.5 –4 1:1 2:1 Deimos k2/Q2 = 1.2 × 10 ¼ ¼ –6 in theI course of our integrations, we assumeI that the system has not 4.0 Phobos k2/Q2 = 1.0 × 10 –7 been affected by any other planetary material. 3.5 Phobos k2/Q2 = 6.0 × 10 Synchronous radius To compute the quality functions, models of Mars, Phobos 3.0 and Deimos are required. For Mars, self-consistently computed Max/min planetocentric distance/ 2.5 interior-structure models are obtained by inversion of geophysi- –3,000 –2,500 –2,000 –1,500 –1,000 –500 0 cal data14 (Supplementary Sections 3 and 4 and Supplementary Fig. Time from present (Myr) b 1), which include the degree-2 tidal amplitude in the form of the 0.40 Love number (k2) and the phase response (Q2), mean density and mean moment of inertia (Supplementary Table 1). One of the main 0.35 parameters that controls the orbital history of Phobos is the fre- 0.30 quency dependence of tidal dissipation (through the exponent α)14. Current observations of a few of the largest low-frequency mars- 0.25 quakes are compatible with an effective mantle Martian seismic Q of 0.20 approximately 300 (refs. 11,12). These, together with the observation Eccentricity 0.15 of the Phobos-induced tidal Q around 95 ± 10, suggest an α value in the range of 0.25–0.35, in agreement with previous studies14,18. 0.10 For our nominal cases, we employ 0.27. Densities of Phobos and α= 0.05 Deimos are <2 g cm−3, implying porous and therefore highly dissi- pative, yet weakly bonded, aggregates19,20. This assumption is based 0 –3,000 –2,500 –2,000 –1,500 –1,000 –500 0 on the moons’ ability to sustain sharp features (such as ubiquitous Time from present (Myr) 21 16 grooves and fractures) , their ability to wobble and the presence c of the Stickney crater, an event that would have shattered Phobos 8 completely if it had been a monolith or a complete rubble pile, but would have left a weakly connected Phobos intact22. For Phobos, 7 we use Q2 values based on viscosity estimates and granular friction Mars 23 R 6 studies of loose aggregates, whereas k2 is computed numerically for a two-layer model comprising a consolidated core and a porous 5 0.021 outer layer, each of which is half the satellite radius. Since μ ≫ ρgR Inclination (rad) (where is the shear rigidity modulus, is the mean density and g μ ρ 4 0.019 is the surface gravity) for both satellites, k2 and Q2 of Deimos can be Semi-major axis/ approximated by size-scaling it to Phobos23. 3 The evolution of planetocentric distances, eccentricities, 0.015 –3,000 –2,000 –1,000 0 semi-major axes and inclinations of the two satellites is shown 2 in Fig.