Survey
* Your assessment is very important for improving the workof artificial intelligence, which forms the content of this project
* Your assessment is very important for improving the workof artificial intelligence, which forms the content of this project
Magnetohydrodynamics wikipedia , lookup
Corona discharge wikipedia , lookup
Strangeness production wikipedia , lookup
Variable Specific Impulse Magnetoplasma Rocket wikipedia , lookup
Plasma stealth wikipedia , lookup
Van Allen radiation belt wikipedia , lookup
Plasma (physics) wikipedia , lookup
MCANDREWS: RISHBETH PRIZES Saturn’s icy satellites I n July 2004 the Cassini-Huygens spacecraft entered Saturn orbit after a seven-year voyage. This long-awaited event provides the first opportunity since the brief Voyager flybys in 1980 and 1981 to collect data in situ at Saturn. The mission will ultimately provide more than four years of dedicated measurements of the planet and its system of rings and moons. One major area of research is the physics of Saturn’s internally generated magnetic field and the resultant magnetic cavity – the magnetosphere – around the planet. How this is affected by the solar wind is also of great importance. The solar wind is a constant stream of electrons and ions that propagates supersonically from the Sun and carries with it the “frozen-in” heliospheric magnetic field. Planetary bodies or, as is the case at Saturn, a planetary magnetic field, provide obstacles to this flow. The magnetopause is the outer boundary of the magnetic cavity; its nose sits at an average distance of 22 RS from Saturn (where RS = 60 268 km). Saturn rotates with a period of 10 hours, as does the planetary field close to Saturn. This then “tows” the plasma inside the magnetosphere along with it because the field is “frozen in”. The corotating plasma region dominates the magnetosphere to a distance of about 10 RS. Within about 4 RS the trapped high-energy radiation belts are present, as they are at Earth, where they are called the Van Allen radiation belts. However, within around 2 RS of the surface, Saturn’s rings are present and they soak up the radiation-belt particles. Hence the radiation environment at Saturn is much reduced in this region. The effect that the orbiting icy satellites can have on this local magnetospheric environment is the main topic of this brief report. The Electron Spectrometer (ELS) is one of three instruments of the Cassini Plasma Spectrometer (CAPS) (Young et al. 2003). CAPS measures plasma populations in the magnetospheric regions Cassini encounters. It has collected comprehensive electron and ion data with an unprecedented temporal and energy response for the first 11 months of the Saturnian tour. The ELS measures the electron component of the plasma, with energies from 0.58 eV to 28 keV. 4.22 3.4 10000 log10 counts/2s electron energy (eV/q) Hazel J McAndrews – and colleagues including the CAPS Team – presents initial results from the Cassini Plasma Spectrometer, based on the talk which won her a Rishbeth Prize at the UK MIST meeting in April. 1000 100 10 2.3 1.2 0.17 1 03.20 03.30 time (UT) 03.40 1: A time–energy spectrogram for the period when the electron drop-out due to Enceladus occurs. The colour scale indicates the number of counts per two second accumlation period, with red indicating high intensities and blue the lowest. The high count rates at low energy (<10eV) consist of photoelectrons generated on the spacecraft surface and also the low-energy corotation plasma. Greater than 10eV the constant counts at all energies are indicative of the penetrating radiation. The dip in counts at ~03:27UT is striking. average effect of moon to Sun higher energy particles move in a westwards sense corotation Saturn 3.95 RS Enceladus Cassini trajectory orbital wake of thermal particles 2: A cartoon of the geometry of the encounter from the north pole. Saturn is in the centre with Enceladus orbiting at a distance of 3.95Rs. Here the corotation direction is anticlockwise while the high-energy electrons (> MeV) move clockwise. Both the low-energy corotational wake and the average wake over an orbit are indicated. During February and March 2005, the ELS data showed several significant drop-outs in the number of radiation-belt electrons. Although these have energies greater than the dynamic range of the instrument (MeV and above), they can penetrate the instrument housing directly and register counts. The times of these drop-outs were found to coincide with crossings by Cassini of the orbital path of the moon Enceladus, which orbits Saturn at a distance of 3.95 RS. One such drop out was seen on 17 February at 03:27 UT and the electron data observed during this crossing can be seen in figure 1. An energy-versus-time spectrogram is shown with the analyser electron energy (which does not correspond to the energy of the penetrating particles) plotted on the verti- cal axis and time along the horizontal. The severe drop-out in the numbers of these high-energy electrons is due to the sweeping effect that Enceladus has on the radiation-belt electrons. The moon is inert, so any electron that hits it can be assumed to be absorbed (Mead 1972). Therefore the moon leaves a trail of flux tubes of depleted of particles as it orbits the planet. This depleted region will continue to move around the planet with the same velocity and direction as the surrounding non-absorbed particles (Van Allen et al. 1980). Of course, when a discontinuity in the density of the plasma is created, surrounding particles will diffuse into the region such that equilibrium is regained over time. By analysis of the depth of the depletion and knowledge of the time since the “hole” was generated, a value for the highenergy electron diffusion rates at these distances in the magnetosphere can be obtained. Figure 2 shows the geometry, where the corotation direction, shown by the curved arrow, is anticlockwise. The moon also travels anticlockwise, but more slowly. As the plasma drifts past the moon it forms a wake ahead of the moon. Over an orbit, the plasma may not fully recover from the depletion before the moon passes by again, giving a longitudinally averaged effect on the plasma distribution at the moon’s orbit. In this encounter the trajectory of the spacecraft passes behind the moon, “upstream” of the moon with respect to corotation of the plasma. Little to no absorption should be seen in the ambient plasma, since the “hole” carved out by the moon should have had sufficient time (more than a corotation period) to fill in. However, for the penetrating particles a significant drop-out is observed, as in figure 1. This can be explained by considering the motion of electrons at these energies (MeV). They have a drift velocity greater than and in an opposite sense to the corotation velocity. Therefore their net motion is westwards around the planet, clockwise in figure 2. Consequently Cassini lies within the wake of these particles just downstream from the moon, so it can observe almost immediately this newly created “hole”. The physics behind the process of the absorption and consequent filling in of the moon’s plasma wake is an interesting one and will be investigated with further work. It will allow increased understanding of plasma motions in the magnetosphere, and, in particular, calculation of diffusion rates which is of great interest and has not been explored since the times of Voyager. ● Hazel McAndrews, Mullard Space Science Laboratory, University College London, UK. A&G • August 2005 • Vol. 46