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Astron. Astrophys. 324, 357-365 (1997)
3. Definitions and geometric analysis
Here, we use the term ejecta to denote the material ejected by the
explosion after fragment entry. We assume this material is ejected in
a variety of ballistic trajectories. We have generated synthetic
trajectories for ballistic material, for different sets of parameters
(initial velocity, altitude of explosion from the 100-mbar level,
impact longitude from Midnight Meridian and terminator longitude from
Midnight Meridian). The altitude of these trajectories is plotted
versus time in Fig. 4, along with the minimum height that the impact
ejecta should have reached to be observable in sunlight. The
parameters used are those for H and L (Chodas and Yeomans, predictions
as of July 16) with a zero altitude set to the 100-mbar level and
assuming trajectories. Hereafter in the text,
we will cite only the vertical component of the velocity.
![[FIGURE]](img16.gif) |
Fig. 4a and b. a Height above the 100-mbar level as a function of time after impact L for ejecta with several vertical velocities, as indicated in the labels. The continuous lines represent the minimum height above which the ejecta are visible in sunlight. The upper continuous line corresponds to 6 km/s and the lower corresponds to 12 km/s. As can be seen, the 6-km/s ejecta do not intercept the curve of height for the sunlit level corresponding to 6 km/s. That means that the 6-Km/s ejecta cannot be visible in reflected sunlight. Also plotted in continuous lines at the bottom of the graph is the minimum height that the ejecta should have to be visible in emission, as a function of time, for the 12-km/s and 6-km/s ejecta. b The same as a but for H impact. The boxes in a and b represent particularly interesting regions discussed in the text
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The terminator level was also assumed to be at 100 mbar. The jovian
radius at and 100 mbar was obtained by
correcting for oblateness the 100-mbar equatorial radius. The gravity
acceleration was corrected for oblateness in the following way:
23.22+2.85sin2 (latitude) (where 23.22 m/s2 is
the equatorial gravity acceleration, in Jupiter, Anderson, 1976). The
gravitational acceleration has also been corrected for altitude in
each step. Coriolis correction has not been applied (this does not
have an important effect on the vertical component). Refraction
effects would have a minor influence on the very lower parts of the
trajectories and have been ignored (see Hammel et al., 1995). Note
that the horizontal velocity of the plumes plays an important role in
lowering the level where the plumes reach sunlight (see Figs. 4a,
4b).
The moment of first detection of the plumes provides information on
the maximum plume vertical velocity or, at least, on the fastest
ejecta which carry a sufficient amount of material to be visible in
sunlight. From the work by Schleicher et al. (1994), the first
indication of the plume is 220 20 seconds after
the L impact, the begining of the flux increase in their lightcurve.
Fitzsimmons et al. (1996) report their first detection about 210 s
after impact. The 220 20-sec time is consistent
with plume velocity of 9 1 km/s, as can be seen
in Fig. 4a (intersection of vertical trajectory with the curve of sun
illumination level for its corresponding velocity). This is best seen
in Fig. 5, which shows an enlarged version of Fig. 4a along with the
curve for 3.5-km/s ejecta. The first detection of H from the WHT data
is somewhat later (300 s) which would suggest slightly slower ejecta.
On the other hand, the telescope was not observing earlier, so this
value represents a lower limit. For L, we believe most of the material
is ejected at velocities between 9 and 12 km/s, since, for that
velocity range, the material returns to the original level between 780
and 1000 seconds after impact, which is the time of rise and decline
of the second maximum in the lightcurve of Schleicher et al. We
believe this maximum is due to thermal emission. The maximum itself
occurs when the 11 km/s-material returns to the original altitude
( 900 sec after impact). Then, for the L impact,
we conclude that the largest amount of material optically thick in the
visible is ejected at 11 km/s, but there is also material thrown at
other velocities, with a maximum of 12 km/s. We can make comparisons
with the G impact results, as both G and L are in the same class in
the categorization scheme of Hammel et al., releasing similar amounts
of energy and leaving similar scars, etc. This maximum velocity of 12
km/s is in agreement with the velocity derived by Hammel et al. (1995)
for the highest velocity ejecta in G plume by measuring its highest
altitude, a completely different approach to that followed here, which
is based on timings. For the H impact, the time of the second maximum
from Fig. 1 is much more uncertain, but seems to be shorter than what
we would expect for 11 km/s ejecta. This would require slower ejecta,
which would be consistent with the observations of a smaller energy
release in H impact compared to L and a smaller crescent-shaped
scar.
![[FIGURE]](img18.gif) |
Fig. 5. Enlargement of Fig. 4a for short times after impact. Also in this graph has been included the height as a function of time for 3.5-km/s ejecta, which are the slowest ejecta which can reach the limb height and be detectable in emission
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The first maximum is reached when most of the ejected material is
above the sunlit limit and with its maximum vertical spreading. For L,
taking a section in Fig. 4a we observe that the maximum spreading
(while all the 7.5-12 km/s material is still in sunlight) corresponds
to time 500 s. This value is in perfect
agreement with the time of maximum shown in the lightcurve of
Schleicher et al. (1994) and with the time of first maximum brightness
by Fitzsimmons et al. (1996). After that moment, some material starts
to cross below the illumination limit, whereas no other material is
capable of reaching the sunlight level (in Fig. 4a, the 6 km/s curve
does not intercept the 6 km/s sunlit level). Then, the visible flux
starts to decrease. For H, we see the first maximum 430 s after impact
(Fig. 1) which would require slower ejecta, but the time sampling is
not good enough to conclude that. We suggest that the minimum in the
lightcurves occurs when a considerable part of the material (that
ejected at velocities between 7.5-9 km/s) crosses the level
illuminated by sunlight on its descent, after which the amount of
reflected light observed decreases. The minima in the lightcurves for
H and L occur at 720 100 sec and 720
20 sec after impact, respectively, according to
Fig. 1c. This is in agreement with predictions in Figs. 4a, 4b, for
the dissapearance of 9 km/s ejecta.
The following maximum in the CCD lightcurve arises mainly from
thermal emission by the particulates or gas, as well as from reflected
sunlight from the rest of the plume. The thermal emission starts to
decrease as the material cools down and the small fraction of ejecta
which was thrown highest (velocity 12 km/s) reaches the original level
(where there is no longer reflected sunlight contributing to the
thermal emission). Following Figs. 4a, 4b, the 12-km/s velocity
material reaches the initial level 1000 seconds after the
explosion.
© European Southern Observatory (ESO) 1997
Online publication: May 26, 1998
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