Mathematics – Logic
Scientific paper
Dec 2010
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2010agufm.p23b1633n&link_type=abstract
American Geophysical Union, Fall Meeting 2010, abstract #P23B-1633
Mathematics
Logic
[5759] Planetary Sciences: Fluid Planets / Rings And Dust
Scientific paper
As part of the Planetary Science Decadal Survey recently undertaken by the NRC's Space Studies Board for the National Academy of Sciences, studies were commissioned for a number of potential missions to outer planet targets. One of these studies examined the technological feasibility of a mission to carry out in situ studies of Saturn's rings, from a spacecraft placed in a circular orbit above the ring plane: the Saturn Ring Observer. The technical findings and background are discussed in a companion poster by T. R. Spilker et al. Here we outline the science goals of such a mission. Most of the fundamental interactions in planetary rings occur on spatial scales that are unresolved by flyby or orbiter spacecraft. Typical particle sizes in the rings of Saturn are in the 1 cm - 10 m range, and average interparticle spacings are a few meters. Indirect evidence indicates that the vertical thickness of the rings is as little as 5 - 10 m, which implies a velocity dispersion of only a few mm/sec. Theories of ring structure and evolution depend on the unknown characteristics of interparticle collisions and on the size distribution of the ring particles. The SRO could provide direct measurements of both the coefficient of restitution -- by monitoring individual collisions -- and the particles’ velocity dispersion. High-resolution observations of individual ring particles should also permit estimates of their spin states. Numerical simulations of Saturn’s rings incorporating both collisions and self-gravity predict that the ring particles are not uniformly distributed, but are instead clustered into elongated structures referred to as “self-gravity wakes”, which are continually created and destroyed on an orbital timescale. Theory indicates that the average separation between wakes in the A ring is of order 30-100 m. Direct imaging of self-gravity wakes, including their formation and subsequent dissolution, would provide critical validation of these models. Other targets of observation by the SRO will include “propellers” (thought to be the signature of sub-km moonlets embedded in the rings), the “ropy” and “straw” structure seen in images of strong density waves and gap edges, and km-scale radial oscillations which may be signatures of “viscous overstabilities” in high-optical depth regions. Most of the science goals identified above could be accomplished by high-resolution nadir imaging of the rings from a platform that co-orbits with the ring particles, i.e., from a spacecraft in circular orbit a few km above the rings. The vertical displacement of the spacecraft is maintained by a continuous low-thrust ion engine, which can be tilted to provide a slow inward radial drift across the rings. Chemical thrusters permit the craft to `hop' over vertical obstacles in the rings (e.g., bending waves and inclined ringlets). In addition to an imaging system with a resolution of at least 10 cm (with 1 cm a desirable goal), other instrumentat ion might include a laser altimeter/range-finder to measure the effective thickness of the rings, as well as the vertical component of particle motions, aswell as in situ instruments to measure the density and composition of the neutral and ionized ring atmosphere, meteoritic and secondary dust fluxes, and local electric fields (especially in spoke regions).
Nicholson Philip D.
Spilker Linda J.
Tiscareno Matthew S.
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