Stability of (exo)moons Nagy Imre Research Group for Physical Geodesy and Geodynamics Department of Astronomy, Eötvös University.

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Presentation transcript:

Stability of (exo)moons Nagy Imre Research Group for Physical Geodesy and Geodynamics Department of Astronomy, Eötvös University

Contents ● Exoplanets ● Detectability of exomoons and transit timing effects ● Where can we find exomoons? ● Hill sphere and Roche limit ● The limit of existence of the exomoons ● Layout of the model for stability investigations ● Preliminary results ● Stability of exomoons ● Permissible range ● Further works

Exoplanets ● The first exoplanet (HD b) was discovered in ● Up to date 432 exoplanets are known in 365 systems (45 multiple planet systems). ● One can see, that many exoplanets are giant planet close to the host star, and some of them are Neptune size object.

Detectability of exomoons ● The mass and the diameter of exomoons are commonly supposed relatively small. ● The small mass causes small, almost invisible effects on radial velocity curve. ● The small diameter causes small effects on light curve, moreover these effects are not periodic (except resonant systems), which makes hard to detect an exomoon. ● Planet and its moon orbit around each other, which causes transit timing effects. ● Detecting the transit timing effects seems to be the most hopeful method.

Transit timing effects ● Planets and its moon orbit around their barycentre, which causes variations in the transit of the planet. ● Transit Time Variation (TTV): ● Amplitude is proportional to m moon a moon ● Transit Duration Variation (TDV): ● Amplitude is proportional to m moon (a moon ) -1/2 ● Detecting the TTV and TDV moon's mass and semi-major axis can be separately determined. ● Current ground-based telescopes could detect a 1M ⊕ exomoon in the habitable zone around a Neptune-like exoplanet.

Where can we find exomoons? ● Around giant exoplanets, since giant planets have moons in our Solar System, ● but there are some problem: ● If the planet orbits too close to the star, the temperature is high. However this circumstance restricts just the composition of the moon. ● Close to the star the shape of the planet is elongated, which can cause strong perturbations. ● If the planet rotates too fast, its shape is flattened, which can cause strong perturbations. ● If the planet orbits too close to the star, the Roche limit can extend over the Hill sphere.

Hill sphere and Roche limit ● Hill sphere: An astronomical body's Hill sphere is the region in which it dominates the attraction of satellites. ● Roche limit: It is the distance within which a celestial body (moon), held together only by its own gravity, will disintegrate due to a second celestial body's (planet) tidal forces exceeding the first body's gravitational self- attraction. ● When the Roche limit grows over the Hill sphere, exomoons cannot exist further.

The limit of existence of the exomoons ● When the Roche limit grows over the Hill sphere, exomoons cannot exist further. For example Gliese 581: M = 0.3 M Sun ρ moon := ρ Earth ≈ 6 g/cm 3 R R-H ≈ AU < a Gl581e = AU

Layout of the model a moon =1 a planet = 1 – 400 a moon m Star = 66.6 – 10 5 m planet m planet = 1 a moon = – 1 a planet a planet = 1 m Star = 1 m planet = 0 – m Star a moon = 1 a planet = 1 – 400 a moon m Star = 1 m planet = 0 – m Star Star Planet Moon m moon = e planet = e moon = 0

Stability of exomoons (Preliminary results)

Permissible range (Preliminary results) a p =1 AU a p =1/3 AU a p =1/5 AU a p =1/7 AU a p =1/9 AU Hill sphere

Conclusions ● We can conclude that,...

Further works ● We would like to calculate ● perturbations from the shape of the planet, which are caused by: – fast rotation of the planet (J 2 ); – vicinity of the star (C 22, S 22 ); ● stability of inclined moon orbits; ● more precisely the radius of the Hill sphere. ● We would like to use Pickard iteration calculating the effect of spherical perturbations. It is a Taylor-series method, similar to Lie integration, but more flexible, however very slow. (Renáta's task)

Thank you for you attention!