2011
DOI: 10.1051/0004-6361/201014194
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New 3D thermal evolution model for icy bodies application to trans-Neptunian objects

Abstract: Context. Thermal evolution models have been developed over the years to investigate the evolution of thermal properties based on the transfer of heat fluxes or transport of gas through a porous matrix, among others. Applications of such models to trans-Neptunian objects (TNOs) and Centaurs has shown that these bodies could be strongly differentiated from the point of view of chemistry (i.e. loss of most volatile ices), as well as from physics (e.g. melting of water ice), resulting in stratified internal struct… Show more

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Cited by 36 publications
(57 citation statements)
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References 48 publications
(55 reference statements)
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“…We used a 3D thermal evolution model by Guilbert-Lepoutre et al (2010) that simulates the temperature of the whole object as a function of its size, density, porosity, orbit, formation delay and radiogenic elements primordial inventory ( 26 Al, 60 Fe, 53 Mn, 40 K, 232 Th, 235 U, 238 U). The bulk assumed composition is dust (77%) plus amorphous water ice (23%), the relative mass fractions being derived from the input 10% porosity.…”
Section: Discussionmentioning
confidence: 99%
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“…We used a 3D thermal evolution model by Guilbert-Lepoutre et al (2010) that simulates the temperature of the whole object as a function of its size, density, porosity, orbit, formation delay and radiogenic elements primordial inventory ( 26 Al, 60 Fe, 53 Mn, 40 K, 232 Th, 235 U, 238 U). The bulk assumed composition is dust (77%) plus amorphous water ice (23%), the relative mass fractions being derived from the input 10% porosity.…”
Section: Discussionmentioning
confidence: 99%
“…In this table, the maximum surface temperature is computed from a thermal balance for the whole surface including different energy inputs such as: the incoming solar energy, (with A the Bond albedo, C the solar constant, d H the heliocentric distance and ξ the local zenith angle), the thermal emission εσT 4 (with ε the thermal emissivity, σ the Stefan-Boltzmann constant and T the temperature), the radial heat flux and lateral heat fluxes, considering a thermal conductivity of about 10 −2 W m −1 K −1 . This thermal balance is computed for about 50 orbits with a full 3D thermal evolution model to get the resulting temperatures (see Appendix B of Guilbert-Lepoutre et al 2010). The insulation per orbit (in J), is computed with the formula (Prialnik et al 2004)…”
Section: (50000) Quaoarmentioning
confidence: 99%
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“…The temperature is determined using a numerical model of three-dimensional heat transport (Guilbert-Lepoutre et al 2011). The model solves the heat equation taking into account conduction via contacts between grains, radiation within pores, insolation, and thermal emission at the surface.…”
Section: Dusty Crust At the Surface Of 67pmentioning
confidence: 99%