Dynamical implantation of objects in the Kuiper Belt
Creators
- 1. Instituto Nacional de Pesquisas Espaciais (INPE), ETE/DMC, Av. dos Astronautas, 1758, São José dos Campos (Brazil)
- 2. Department of Space Studies, Southwest Research Institute, 1050 Walnut Street, Boulder, CO (United States)
Description
Several models have been suggested in the past to describe the dynamical formation of hot Kuiper Belt objects (hereafter Hot Classicals or HCs for short). Here, we discuss a dynamical mechanism that allows orbits to evolve from the primordial planetesimal disk at ≲ 35 AU to reach the orbital region now occupied by HCs. We performed three different sets of numerical simulations to illustrate this mechanism. Two of these simulations were based on modern theories for the early evolution of the solar system (the Nice and jumping-Jupiter models). The third simulation was performed with the purpose of increasing the resolution at 41-46 AU. The common aspect of these simulations is that Neptune scatters planetesimals from ≲ 35 AU to >40 AU and then undergoes a long phase of slow residual migration. Our results show that to reach an HC orbit, a scattered planetesimal needs to be captured in a mean motion resonance (MMR) with Neptune where the perihelion distance rises due to the Kozai resonance (which occurs in MMRs even for moderate inclinations). Finally, while Neptune is still migrating, the planetesimal is released from the MMR on a stable HC orbit. We show that the orbital distribution of HCs expected from this process provides a reasonable match to observations. The capture efficiency and the mass deposited into the HC region appears to be sensitive to the maximum eccentricity reached by Neptune during the planetary instability phase. Additional work will be needed to resolve this dependency in detail.
Availability note (English)
Available from http://dx.doi.org/10.1088/0004-6256/148/3/56Additional details
Identifiers
Publishing Information
- Journal Title
- Astronomical Journal (New York, N.Y. Online)
- Journal Volume
- 148
- Journal Issue
- 3
- Journal Page Range
- [9 p.]
- ISSN
- 1538-3881
INIS
- Country of Publication
- United States
- Country of Input or Organization
- International Atomic Energy Agency (IAEA)
- INIS RN
- 46048579
- Subject category
- S79: ASTROPHYSICS, COSMOLOGY AND ASTRONOMY;
- Descriptors DEI
- AUGMENTATION; CAPTURE; COMPUTERIZED SIMULATION; DISTANCE; DISTRIBUTION; EFFICIENCY; EVOLUTION; INCLINATION; INSTABILITY; JUPITER PLANET; MASS; MIGRATION; NEPTUNE PLANET; ORBITS; RESOLUTION; RESONANCE; SOLAR SYSTEM
- Descriptors DEC
- PLANETS; SIMULATION