2019
DOI: 10.3847/1538-3881/ab2890
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A Pluto–Charon Sonata: Dynamical Limits on the Masses of the Small Satellites

Abstract: During 2005-2012, images from Hubble Space Telescope (HST) revealed four moons orbiting Pluto-Charon (Weaver et al. 2006;Showalter et al. 2011Showalter et al. , 2012. Although their orbits and geometric shapes are well-known, the 2σ uncertainties in the masses of the two largest satellites -Nix and Hydra -are comparable to their HST masses (Brozović et al. 2015;Showalter & Hamilton 2015;Weaver et al. 2016). Remarkably, gravitational n-body computer calculations of the long-term system stability on 0.1-1 Gyr ti… Show more

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Cited by 15 publications
(62 citation statements)
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“…Charon has mass m C = 1.586 × 10 24 g, radius R C = 606 km, and mean density ρ C = 1.702 g cm −3 . Combined with analyses of HST observations (Brozović et al 2015;Showalter & Hamilton 2015), detailed n-body calculations (Kenyon & Bromley 2019b) provide limits on the mass of Nix (m N 4.5 × 10 19 g) and Hydra (m H 4.8 × 10 19 g; see also Youdin, Kratter & Kenyon 2012). Although constraints on the masses of Styx (m S ) and Kerberos (m K ) are more elusive, plausible estimates are m S ≈ 6 × 10 17 g and m K ≈ 10 18 g. Thus, the total mass in satellites is m sat ≈ 10 20 g. These satellites orbit within a 'satellite zone,' a ≈ 33-66 R P , defined as a region that encompasses the orbits of the four satellites (e.g., Kenyon & Bromley 2019a;Bromley & Kenyon 2020).…”
Section: Basic Parametersmentioning
confidence: 99%
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“…Charon has mass m C = 1.586 × 10 24 g, radius R C = 606 km, and mean density ρ C = 1.702 g cm −3 . Combined with analyses of HST observations (Brozović et al 2015;Showalter & Hamilton 2015), detailed n-body calculations (Kenyon & Bromley 2019b) provide limits on the mass of Nix (m N 4.5 × 10 19 g) and Hydra (m H 4.8 × 10 19 g; see also Youdin, Kratter & Kenyon 2012). Although constraints on the masses of Styx (m S ) and Kerberos (m K ) are more elusive, plausible estimates are m S ≈ 6 × 10 17 g and m K ≈ 10 18 g. Thus, the total mass in satellites is m sat ≈ 10 20 g. These satellites orbit within a 'satellite zone,' a ≈ 33-66 R P , defined as a region that encompasses the orbits of the four satellites (e.g., Kenyon & Bromley 2019a;Bromley & Kenyon 2020).…”
Section: Basic Parametersmentioning
confidence: 99%
“…For each combination of a and e of the central binary, we choose two values for the initial inclination, ı 0 = 0.025 and 0.25. The first choice allows for maximum collisional damping throughout the evolution; the second choice provides limits on the ability of collisions to evolve a thick disk into the thin disk required for the growth of satellites (Kenyon & Bromley 2014b;Walsh & Levison 2015).…”
Section: Numerical Codementioning
confidence: 99%
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