1994
DOI: 10.1006/icar.1994.1074
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Comet Shoemaker-Levy 9: Impact on Jupiter and Plume Evolution

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Cited by 61 publications
(52 citation statements)
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“…The alternative to the simplified approach is to use 4) full-scale hydrodynamic models in which the projectile is treated as a strengthless continuous body Takata et al 1994;Crawford et al 1995), as a body with some kind of strength (Ivanov and Melosh 1994), or as a cloud of fragments (Svetsov et al 1995). Since the internal properties of comets and asteroids are poorly known, simplified approaches are competitive with more comprehensive hydrodynamic models because they allow us to investigate systematically a wide range of input parameters over a short period of time.…”
Section: Numerical Models For Atmospheric Entrymentioning
confidence: 99%
See 1 more Smart Citation
“…The alternative to the simplified approach is to use 4) full-scale hydrodynamic models in which the projectile is treated as a strengthless continuous body Takata et al 1994;Crawford et al 1995), as a body with some kind of strength (Ivanov and Melosh 1994), or as a cloud of fragments (Svetsov et al 1995). Since the internal properties of comets and asteroids are poorly known, simplified approaches are competitive with more comprehensive hydrodynamic models because they allow us to investigate systematically a wide range of input parameters over a short period of time.…”
Section: Numerical Models For Atmospheric Entrymentioning
confidence: 99%
“…However, this simplification leads to unrealistically thin and wide projectiles and to extremely low final velocities (essentially, deceleration is inversely proportional to the projectile's thickness). Numerical models (Ivanov et al 1992;Ahrens et al 1994;Takata et al 1994;Crawford et al 1995) carried out around the same time that the pancake model was developed (i.e., the time of the collision of comet Shoemaker-Levy 9 with Jupiter) clearly showed that although flattening ("pancaking") is a typical behavior of disrupted projectiles, it is mostly restricted to a flattening factor of 1.7-2.3. Further, widening is arrested by the growth of Kelvin-Helmholtz (K-H) and Rayleigh-Taylor (R-T) instabilities and the resulting projectile fragmentation into smaller pieces.…”
Section: Separated Fragments (Sf) Model and Pancake Modelmentioning
confidence: 99%
“…Previous 3D impact models were obtained for impacts on Jupiter (see discussion by Mac Low 1996), by Takata et al (1994) using an SPH at an effective resolution of about R4, and by Crawford using an Eulerian code at an effective resolution of about R10. The SPH results show little structure and are clearly underesolved; Crawford's results are intriguing but again unlikely to be adequately resolved.…”
Section: Previous Modelsmentioning
confidence: 99%
“…In other words, the projectile in SIM2 must plow through more envelope to reach the same depth as the projectile in SIM1, and thus kinetic energy deposition as a function of depth is more efficient in off-axis collisions. This kinetic energy is deposited in the form of heat, which gives rise to a growing plume rising toward the surface (see Takata et al 1994, for detailed studies of this subject).…”
Section: Energy Deposition Inside the Envelopementioning
confidence: 99%