Long Period Variations in Jupiter's Obliquity and Galilean Satellite Inclinations: Influence
on Tidal Stress and Dissipation
HR: 1330h
AN: P12A-1056 [PDF]
TI: Long Period Variations in Jupiter's Obliquity and Galilean Satellite Inclinations: Influence on Tidal
Stress and Dissipation
AU: * Bills, B G
EM: Bruce.G.Bills@nasa.gov
AF: NASA Goddard Space Flight Center, Laboratory for Terrestrial Physics, Greenbelt, MD 20771 United States
AU: Ray, R D
EM: Richard.D.Ray@nasa.gov
AF: NASA Goddard Space Flight Center, Laboratory for Terrestrial Physics, Greenbelt, MD 20771 United States
AB:
Spatial and temporal patterns of tidal stress and dissipation within the Galilean satellites are important keys to
understanding the dynamics of these bodies. Most past studies have emphasized the role of orbital eccentricity in tidal
forcing. There is an additional component of tidal forcing due to finite obliquities of these bodies.
The present values of satellite orbital inclinations and obliquities are not particularly representative of their respective
longer term variations. As a result, the tidal stress and dissipation regimes at present may not provide adequate explanation
of the sources of surface features seen on the satellites.
On relatively short time scale ($<$ 10$^{4}$ years), the satellite inclinations and obliquities can be approximated by a
model which treats the spin pole of Jupiter as inertially fixed. In that case, each satellite orbit plane responds to torques
from the oblate figure of Jupiter, mutual interaction with the other satellites, and a weak solar torque. The free
oscillation periods of this system are (7.358, 29.63, 139.97, and 547.89) years. The satellite spin pole motions are driven
by torques from Jupiter, acting on the oblate figures of the satellites. The spin pole precession periods are (0.66, 5.16,
31.9, and 320) years.
In order to understand longer term variations in forced obliquities of the Galilean satellites, and the resulting variations
in tidal forcing, we have investigated the response of the system composed of four satellite orbits and the spin of Jupiter
to varying solar torques. The solar torque varies as the orbital inclination of Jupiter varies, on time scales of
10$^{5}$-10$^{6}$ years. The dominant source of orbital variation is exchange of angular momentum between the orbits of
Jupiter, Saturn, Uranus, and Neptune. In the secular variation model of Laskar [1988] there are 50 Fourier terms representing
the orbit pole of Jupiter.
The response of each of the objects (Jupiter's spin and satellite orbits) is a weighted sum of normal mode responses, with
weights proportional to the forcing amplitude but also determined by proximity of the forcing period to the normal mode
period. The free oscillation periods of the 5-body system are (7.365, 29.635, 139.56, 546.16, and 536,500) years. The spin
pole precession period of Jupiter, without satellites, would be 980 kyr, but solar torques on the satellite orbits, coupled
to Jupiter via its
oblateness, shorten that period to 536 kyr. The largest source of uncertainty in this estimate is the polar moment of inertia
of Jupiter, which has a 4% uncertainty.
One of the larger terms in Laskar's secular orbital model is nearly in resonance with the lowest frequency term in the 5-body
system. This allows substantial variations in the obliquity of Jupiter and the satellite orbital inclinations on 10$^{5}$
year time scales. As the satellite orbits evolve under tidal influence, the strength of resonant forcing will vary.
DE: 5450 Orbital and rotational dynamics
DE: 6218 Jovian satellites
DE: 6220 Jupiter
SC: Planetary Sciences [P]
MN: 2003 Fall Meeting