c European Geosciences Union 2003 Annales Geophysicae (2003) 21: 1419–1441 Annales Geophysicae Magnetosphere-ionosphere coupling currents in Jupiter’s middle magnetosphere: dependence on the effective ionospheric Pedersen conductivity and iogenic plasma mass outflow rate J. D. Nichols1 and S. W. H. Cowley1 1 Department of Physics and Astronomy, University of Leicester, Leicester LE1 7RH, UK Received: 27 August 2002 – Revised: 9 December 2002 – Accepted: 20 February 2003 Abstract. The amplitude and spatial distribution of the coupling currents that flow between Jupiter’s ionosphere and middle magnetosphere, which enforce partial corotation on outward-flowing iogenic plasma, depend on the values of the effective Pedersen conductivity of the jovian ionosphere and the mass outflow rate of iogenic plasma. The values of these parameters are, however, very uncertain. Here we determine how the solutions for the plasma angular velocity and current components depend on these parameters over wide ranges. We consider two models of the poloidal magnetospheric magnetic field, namely the planetary dipole alone, and an empirical current sheet field based on Voyager data. Following work by Hill (2001), we obtain a complete normalized analytic solution for the dipole field, which shows in compact form how the plasma angular velocity and current components scale in space and in amplitude with the system parameters in this case. We then obtain an approximate analytic solution in similar form for a current sheet field in which the equatorial field strength varies with radial distance as a power law. A key feature of the model is that the current sheet field lines map to a narrow latitudinal strip in the ionosphere, at ≈ 15◦ co-latitude. The approximate current sheet solutions are compared with the results of numerical integrations using the full field model, for which a power law applies beyond ≈ 20 RJ , and are found to agree very well within their regime of applicability. A major distinction between the solutions for the dipole field and the current sheet concerns the behaviour of the field-aligned current. In the dipole model the direction of the current reverses at moderate equatorial distances, and the current system wholly closes if the model is extended to infinity in the equatorial plane and to the pole in the ionosphere. In the approximate current sheet model, however, the field-aligned current is unidirectional, flowing consistently from the ionosphere to the current sheet for the sense of the jovian magnetic field. Current closure must then occur at higher latitudes, on field lines outside the region described by the model. The amplitudes Correspondence to: J. D. Nichols: (jdn@ion.le.ac.uk) of the currents in the two models are found to scale with the system parameters in similar ways, though the scaling is with a somewhat higher power of the conductivity for the current sheet model than for the dipole, and with a somewhat lower power of the plasma mass outflow rate. The absolute values of the currents are also higher for the current sheet model than for the dipole for given parameters, by factors of ≈ 4 for the field-perpendicular current intensities, ≈ 10 for the total current flowing in the circuit, and ≈ 25 for the field-aligned current densities, factors which do not vary greatly with the system parameters. These results thus confirm that the conclusions drawn previously from a small number of numerical integrations using spot values of the system parameters are generally valid over wide ranges of the parameter values. Key words. Magnetospheric physics (current systems, magnetosphere-ionosphere interactions, planetary magnetospheres) 1 Introduction The dynamics of Jupiter’s middle magnetosphere are dominated by the processes that couple angular momentum between the planet’s atmosphere and the equatorial plasma that flows outwards from the Io source at ≈ 6 RJ (Jupiter’s radius, RJ , is ≈ 71 373 km) (Hill, 1979; Siscoe and Summers, 1981; Hill et al., 1983; Belcher, 1983; Vasyliunas, 1983; Bagenal, 1994). The field and plasma structures envisaged are sketched in Fig. 1, where the arrowed solid lines indicate magnetic field lines, while the dots indicate the region occupied by dense rotating iogenic plasma. The region of flux tubes threading this plasma disc constitutes Jupiter’s middle magnetosphere, where the field lines are characteristically distended outward by azimuthal plasma currents associated with radial stress balance. In the inner region, the iogenic plasma approximately corotates with the planet, but as it moves outward its angular velocity falls, as the inverse square of the distance if no torques act. However, when the angular 1420 J. D. Nichols and S. W. H. Cowley: Magnetosphere-ionosphere coupling currents in Jupiter’s middle magnetosphere WJ w Bj WJ* Io Bj Fig. 1. Sketch of a meridian cross section through Jupiter’s inner 1 and middle magnetosphere, showing the principal physicalFig features involved. The arrowed solid lines indicate magnetic field lines, the arrowed dashed lines the magnetosphere-ionosphere coupling current system, and the dotted region the rotating disc of out-flowing iogenic plasma. (From Cowley and Bunce, 2001). velocity of the plasma and field lines (ω in Fig. 1) falls below that of the planet (J ), or more specifically, below that of the neutral upper atmosphere (∗J ), a frictional torque is imposed on the feet of the field lines due to ion-neutral collisions in the Pedersen-conducting layer of the ionosphere. This torque acts to spin the flux tubes and equatorial plasma back up towards rigid corotation with the planet, so that in the steady state the plasma angular velocity falls less quickly with distance than as the inverse square. At the same time, the equal and opposite torque on the neutral atmosphere results in atmospheric sub-corotation (“slippage”) in the Pedersen layer, so that ω < ∗J < J (Huang and Hill, 1989). The spin-up torque on the plasma is communicated to the equatorial region by the magnetic field, which becomes bent out of meridian planes into a “lagging” configuration, associated with the azimuthal fields Bϕ shown in the figure. The corresponding magnetosphere-ionosphere coupling current system, of primary interest here, is shown by the arrowed dashed lines in Fig. 1. The current flows radially outward across the field in the equatorial plane, such that the torque associated with the j × B force accelerates the plasma in the sense of Jupiter’s rotation. In the ionosphere the Pedersen current flows equatorward in both hemispheres, producing an equal and opposite torque which balances the torque due to ionneutral collisions. The current circuit is closed by a system of field-aligned currents which flow from the ionosphere to the equator in the inner part of the system, and return in the outer part. The steady-state angular velocity profile of the out-flowing equatorial plasma was first calculated on the above basis by Hill (1979). In this study the poloidal field was taken to be that of the planetary dipole alone, such that the radial distension of the middle magnetosphere field lines shown in Fig. 1 was not taken into account. This restriction was later removed by Pontius (1997), who introduced empirical poloidal field models into the calculations. He found that the solutions for the plasma angular velocity profile are remarkably insensitive to the field model employed. Although consid- ered implicitly, the properties of the coupling currents were not calculated in these studies. Recently, however, attention has focussed directly on the currents, it being suggested by a number of authors that the ring of upward field-aligned current surrounding each magnetic pole is associated with the “main oval” observed in Jupiter’s auroras (Bunce and Cowley, 2001; Cowley and Bunce, 2001; Hill, 2001; Southwood and Kivelson, 2001). Hill (2001) considered the currents in his original dipole problem, while Cowley and Bunce (2001) calculated the currents for both a dipole field and an empirical current sheet field. The latter authors found that the fieldaligned current densities are an order of magnitude larger for the current sheet model than for the dipole. The physical origins of this effect have been discussed further by Cowley et al. (2002, 2003), who show that it relates to the fact that the field lines on which corotation breaks down, while mapping to similar distances in the equatorial plane, map in the ionosphere to a narrower range of latitudes further from the pole for a current sheet field than for the dipole. The solutions for the plasma angular velocity and the current depend on two system parameters, the “effective” value of the height-integrated ionospheric Pedersen conductivity (possibly reduced from the true value by the atmospheric “slippage” mentioned above), and the plasma mass outflow rate from the Io torus. However, neither of these parameters is well determined at present. Estimates of the conductivity have ranged from ≈ 0.1 to ≈ 10 mho (Strobel and Atreya, 1983; Bunce and Cowley, 2001), while estimates of the mass outflow rate have ranged from ≈ 500 to ≈ 2000 kg s−1 (Broadfoot et al., 1981; Hill et al., 1983; Vasyliunas, 1983; Khurana and Kivelson, 1993; Bagenal, 1997). The purpose of the present paper is to examine how the solutions for the plasma angular velocity and coupling currents depend on these two parameters for both dipole and current sheet field models. Some general results for the dipole model have been presented previously by Hill (2001). For the current sheet field model, however, only a few numerical solutions using “reasonable” spot values of the system parameters have been published to date (Cowley and Bunce, 2001; Cowley et al., 2002, 2003). In this paper we first provide a complete solution for the dipole field, before going on to examine related results for a current sheet model in which the equatorial field is taken to vary with distance as a power law. The parameter ranges considered are 0.1–10 mho for the “effective” conductivity, and 100–10 000 kg s−1 for the mass outflow rate. The work presented here thus shows how the coupling current system depends on the system parameters over a wide range of values, here taken as constant quantities in a given solution. This knowledge should provide valuable background for more complex future studies in which the system parameters are taken to vary in time and/or space, as may more generally be the case. J. D. Nichols and S. W. H. Cowley: Magnetosphere-ionosphere coupling currents in Jupiter’s middle magnetosphere 2 Basic equations In this section we first summarise the basic equations governing the magnetosphere-ionosphere coupling current system depicted in Fig. 1, and then discuss the nature of the solutions at small and large distances. Derivations were given earlier by Hill (1979), Vasyliunas (1983) and Pontius (1997), and have most recently been discussed by Hill (2001), Cowley and Bunce (2001), and Cowley et al. (2003). Only the central results will, therefore, be stated here, together with an outline of the assumptions and approximations which have been made. We first assume that the magnetic field is axisymmetric, such that the poloidal components can be specified by a flux function F (ρ, z) related to the field components by B = (1/ρ)∇F × ϕ̂, where ρ is the perpendicular distance from the magnetic axis, z is the distance along this axis from the magnetic equator, and ϕ is the azimuthal angle. In this case F =constant defines a flux shell, such that magnetic mapping between the equatorial plane (subscript “e”) and the ionosphere (subscript “i”), as required here, is simply achieved by writing Fe = Fi . Neglecting non-dipole planetary fields and the small perturbations due to magnetospheric currents, the flux function in the ionosphere is taken to be Fi = BJ ρi2 = BJ RJ2 sin2 θi , (1) where ρi is the perpendicular distance from the magnetic axis, θi the magnetic co-latitude, and BJ the dipole equatorial magnetic field strength (taken to be 4.28 × 105 nT in conformity with the VIP 4 internal field model of Connerney et al., 1998). The absolute value of F has been fixed by taking F = 0 on the magnetic axis. The flux function in the equatorial plane is then obtained by integrating Bze 1 dFe = , ρe dρe (2) where Bze (ρe ) is the north-south field threading the current sheet. Assuming for simplicity that the magnetic and planetary spin axes are co-aligned, the equatorward-directed heightintegrated Pedersen current in the ionosphere is given by ω iP = 26P∗ BJ J ρi 1 − J s Fi ω = 26P∗ BJ J 1− , (3) BJ J where we have taken the polar magnetic field to be nearvertical and equal to 2BJ in strength (an approximation valid to within ≈ 5% in our region of interest). In this expression, 6p∗ is the “effective” height-integrated ionospheric Pedersen conductivity, reduced from the true value 6p = 6p∗ / (1-k) by neutral atmosphere “slippage” as mentioned above, where parameter k (whose value 0 < k < 1 is also uncertain at present) is related to the angular velocities by (J − ∗J ) = 1421 k(J − ω) (Huang and Hill, 1989). The radial current intensity in the equatorial plane iρ , integrated through the full thickness of the sheet, then follows from the current continuity requirement ρe iρ = 2ρi iP (assuming symmetry between the two hemispheres) 46P∗ J Fe ω 1− , (4a) iρ = ρe J so that the total equatorial radial current, integrated in azimuth, is ω Iρ = 2πρe iρ = 8π6P∗ J Fe 1 − , (4b) J equal, of course, to twice the azimuth-integrated total Pedersen current IP = 2 πρi iP flowing in each conjugate ionosphere. The field-aligned current density follows from the divergence of either of these field-perpendicular currents. Differentiating the equatorial current gives j dIρ 1 k = = B 4πρe |Bze | dρe F d ω ω e −26P∗ J + 1− , (5a) ρe |Bze | dρe J J where we have put Bze = −|Bze |, since the jovian field is negative (points south) at the equator, 6P∗ has been taken to be constant, and the sign of jk is appropriate to the Northern Hemisphere (as employed throughout). The quantity (jk /B) is constant along field lines between the equator and the ionosphere in the assumed absence of significant fieldperpendicular currents in the intervening region. The fieldaligned current density just above the ionosphere is then given by j k jki = 2BJ , (5b) B using the same approximation for the polar field as indicated above. The analysis is completed by determining the steady state angular velocity profile of the equatorial plasma. Following Hill (1979, 2001), Pontius (1997), and Cowley et al. (2002), Newton’s second law applied to a steady outflow of plasma from the Io torus gives 2πρe2 iρ |Bze | d (ρe2 ω(ρe )) = , dρe Ṁ (6a) where Ṁ is the plasma mass outflow rate. Expanding and substituting Eq. (4a), we find ω ρe d ω ω 4π 6P∗ Fe |Bze | + = 1− , 2 dρe J J J Ṁ (6b) an equation we refer to as the Hill-Pontius equation (though here slightly simplified, as in Hill (2001), by taking the ionospheric field strength to be equal to 2BJ ). It is a first order linear equation for ω that can be solved with the use of one boundary condition. We note with Hill (2001) that if the angular velocity profile obeys this equation, the derivative may 1422 J. D. Nichols and S. W. H. Cowley: Magnetosphere-ionosphere coupling currents in Jupiter’s middle magnetosphere be substituted directly into Eq. (5a) to yield a form for the field-aligned current which involves (ω/ J ) only. It is an important general property of the physically interesting solutions of the above equations that at small radial distances the currents depend on Ṁ and not on 6P∗ , while at large radial distances they depend on 6P∗ and not on Ṁ. The small-ρe approximations follow from a series solution of Eq. (6b) for the case in which (ω/ J )=1 at ρe = 0 (such that the plasma rigidly corotates at small distances). Taking (Ṁ/6P∗ ) as the formal expansion parameter, we write n ∞ X Ṁ ω = an , J 6P∗ n=0 (7a) and substituting into Eq. (6b) and equating coefficients of powers of (Ṁ/6P∗ ) we find that a0 = 1, and that for n ≥ 1 the an are determined by the recurrence relation an+1 = − 1 d (ρ 2 an ). 8πρe Fe |Bze | dρe e (7b) Thus, the leading term describing the breakdown of rigid corotation in the inner region which we take as our smallρe (‘S’) approximation is Ṁ ω =1− , (8) J S 4π 6P∗ Fe |Bze | as given previously (but not derived in this manner) by Cowley et al. (2003). We note that the departure from rigid corotation is proportional to Ṁ and inversely proportional to 6P∗ . When substituted into Eqs. (3)–(5) to find the corresponding approximations for the currents, we then find that the currents on a given field line depend only on Ṁ and not on 6P∗ iP S = ṀJ , 2πρi |Bze | iρ S = ṀJ , πρe |Bze | j k B =− S Iρ S = ṀJ 2πρe |Bze ṀJ , |Bze | (9a, b) 2ṀJ , |Bze | (9c, d) IP S = |3 d|Bze | , dρe (9e) and jki S = − ṀJ BJ d|Bze | . πρe |Bze |3 dρe (9f) These expressions can also be derived directly by substituting ω = J into the left side of Eq. (6a), i.e. they are just the currents required to maintain near-rigid corotation in the inner region. The large-ρe (‘L’) approximations are simply obtained by putting (ω/J )L = 0 into Eqs. (3)–(5) to find iP L = 26P∗ BJ J ρi , (10a) IP L = 4π 6P∗ BJ J ρi2 , (10b) iρ L = 46P∗ J Fe ρe (10c) Iρ L = 8π 6P∗ J Fe , j k B L = −26P∗ J , (10d) and jki L = −46P∗ BJ J , (10e) (10f) which thus depend only on 6P∗ and not on Ṁ. 3 Plasma angular velocity and coupling current system for a dipole magnetic field model Following the earlier work of Hill (1979, 2001) and Cowley and Bunce (2001, 2003), in this section we provide a complete analytic solution for the case where the poloidal field is taken to be the planetary dipole alone, showing how the solutions for the angular velocity and current components scale in space and in amplitude with the system parameters. These results form a useful introduction to, and point of comparison with, the results for the current sheet field to be presented in the Sect. 4. Using Eq. (2), for the dipole field we have R 3 J Bze dip = −BJ and hence (11a) ρe Fe dip = BJ RJ3 . ρe (11b) Substituting these into Eq. (6b), the Hill-Pontius equation for the dipole field is ω ω RDe 4 ω ρe d + =2 1− , (12) 2 dρe J J ρe J where RDe is the equatorial “Hill distance” for the dipole field (subscript ‘D’), given by 2π6P∗ BJ2 RJ2 1/4 RDe = . (13) RJ Ṁ It can thus be seen that the angular velocity in this case is a function only of (ρe /RDe ), so that the solutions scale with equatorial distance as RDe and hence with the system parameters as (6P∗ /Ṁ)1/4 . The general solution of Eq. (12) can be obtained by the integration factor method (Hill, 1979) !2 " !4 # √ RDe ω RDe = π exp × J ρe ρe " " !2 # # RDe × erfc +K , (14) ρe where erfc(z) is the complementary error function (related to the error function erf(z) by erfc(z) = 1 - erf(z)), and K is a constant of integration. All solutions diverge at the origin except the solution with K = 0. This special solution rigidly corotates (i.e. (ω/ J ) = 1) when (ρe /RDe ) goes to zero, J. D. Nichols and S. W. H. Cowley: Magnetosphere-ionosphere coupling currents in Jupiter’s middle magnetosphere 1423 wêWJ and is the solution derived previously by Hill (1979, 2001). Mapping to the ionosphere is achieved by equating the flux functions given by Eq. (1) and (11b), such that s ρi RJ sin θi = = . (15) RJ ρe 1wêWJ 1 0.8 0.8 0.6 0.6 0.4 Introducing an ionospheric counterpart of the “Hill distance” given by s !1/8 RJ Ṁ RJ , (16) RDi = RJ = RDe 2π 6P∗ BJ2 RJ2 we then find that the angular velocity mapped to the ionosphere is a function only of (ρi /RDi ), where s ρi RDe = , (17) RDi ρe such that the solutions scale with distance from the magnetic pole as (Ṁ/6P∗ )1/8 . With regard to physical units, introduction of the constant quantities given above yields the following values for the equatorial and ionospheric scale lengths !1/4 6P∗ (mho) RDe ≈ 49.21 (18a) RJ Ṁ(103 kg s−1 ) and RDi ≈ 0.1426 RJ Ṁ(103 kg s−1 ) 6P∗ (mho) !1/8 , (18b) such that for system parameters at the centre of the ranges mentioned in the Introduction, i.e. 6P∗ = 1 mho and Ṁ = 1000 kg s−1 , we find RDe ≈ 49.2 RJ and RDi ≈ 0.14 RJ (corresponding to a co-latitude of 8.2◦ ). If we fix Ṁ at this value and allow 6P∗ to increase from 0.1 to 10 mho, we find that RDe increases from 27.7 to 87.5 RJ , while RDi decreases from 0.19 to 0.11 RJ (co-latitudes between 11.0◦ and 6.1◦ ). Similarly, if we fix 6P∗ at 1 mho and allow Ṁ to increase from 100 to 10 000 kg s−1 , we find that RDe and RDi vary over the same ranges but in the reversed sense. Thus because RDe and RDi depend on the system parameters only as the quarter and eighth powers, respectively, they change only by modest factors as the system parameters vary widely. We note that the equatorial scales are comparable to the radial scale of the jovian middle magnetosphere, which extends to distances between ∼40 and ∼100 RJ , depending on local time and the state of the magnetosphere. The solid lines in Figs. 2a and b show the normalised angular velocity solution with K = 0 plotted versus (ρe /RDe ) in the equatorial plane, and versus (ρi /RDi ) in the ionosphere, respectively. Near-rigid corotation is maintained to (ρe /RDe ) ≈ 0.5, beyond which (ω/ J ) decreases rapidly, reaching 0.5 when (ρe /RDe ) ≈ 1.52. We also note that solutions started with non-zero K within (ρe /RDe ) ≤ 0.5 converge very rapidly onto this solution at larger distances, such that the solutions are only weakly dependent on the choice 0.4 0.2 0.2 re êRDe re êRDe 1 2 3 4 5 1 2 3 4 5 0.5 1 1.5 2 0.5 1 1.5 2 ri êRDi 2.5 Fig 2b wêWJ (a) 1wêWJ 1 0.8 0.8 0.6 0.6 0.4 0.4 0.2 0.2 2.5 ri êRDi (b) 2b Fig. 2. Plots of the steady-state plasma angular velocity profileFigfor a dipole magnetic field, shown (a) versus normalised radial distance in the equatorial plane (ρe /RDe ), and (b) versus normalised distance from the magnetic axis in the ionosphere (ρi /RDi ) . The solid line in each case shows the full solution obtained from Eq. (14) with K = 0, such that the plasma rigidly corotates at small radial distances. The long-dashed lines show the small ρe form given by Eq. (19), while the corresponding large ρe form is just (ω/J )L = 0. The downward-pointing tick marks indicate the limits of validity of both these approximations, as defined in the text. The short-dashed lines show the higher-order large ρe form given by Eq. (20), whose limit of validity (as also defined in the text) is indicated by the upward-pointing tick mark. The horizontal dotted lines indicate the condition for rigid corotation, (ω/ J ) = 1. of boundary condition in this case (Cowley et al., 2003). The dashed lines in Fig. 2 show some approximate forms, with the tick marks indicating their regimes of validity. The longdashed lines show the small-ρe (‘S’) approximation given by Eq. (8), which in normalised form becomes ω J ! S 1 ρe =1− 2 RDe !4 1 RDi =1− 2 ρi !8 . (19) (We note that the series generated by Eq. (7) is the same as that obtained by asymptotic expansion of the error function in Eq. (14) for large argument.) The approximate form falls away from rigid corotation more quickly than the full solution, and reaches zero, equal to the large-ρ e (‘L’) approxima√ tion (ω/ J )L = 0 at (ρe /RDe ) = 4 2 ∼ 1.189. We define 1424 J. D. Nichols and S. W. H. Cowley: Magnetosphere-ionosphere coupling currents in Jupiter’s middle magnetosphere Table 1. Principal features of the plasma angular velocity and coupling current system for a dipole field in normalised units ρe RDe Feature Maximum upward field-aligned current density (jk /B)/(jk /B)D = jki /jkiD ≈ 0.6111 max max ρi RDi ω J 1.0203 0.9900 0.7467 Maximum sheet-integrated equatorial radial current iρ /iρD ≈ 0.9809 max Plasma angular velocity falls to ω = 0.5 1.1034 0.9520 0.7014 1.5201 0.8111 0.5 Maximum total current azimuth-integrated Iρ /IρD = 2 IP /IP D ≈ 8.404 1.7409 0.7579 0.4178 2.5674 0.6241 0.2284 ∞ 0 0 J max max Field-aligned current passes through zero Maximum ionospheric Pedersen height-integrated current iP /iP D ≈ 0.9631 max Maximum downward current density field-aligned (jk /B)/(jk /B)D = jki /jkiD = –2 min min the limits of validity of these approximations as being the points where (1 − (ω/ J )S,L ) = 1.1(1 − (ω/ J )), such that the departure from rigid corotation given by the approximate form exceeds that of the full solution by 10% of the latter. These limiting positions are shown by the downwardpointing tick marks in Fig. 2. The short-dashed lines in the figure also show a higher-order large-ρe form (‘L0 ’), in which the plasma angular velocity falls with distance as ρe−2 , due to negligible ionospheric torque. Noting that both the exponential and the error functions go to unity in Eq. (14) as ρe → ∞, we find with Hill (1979) that for K = 0 ! !2 √ ω RDe = π . (20) J 0 ρe L The limit of validity of this approximation is similarly defined as the point where (1−(ω/ J )L0 ) = 0.9(1−(ω/ J )), and is marked by the upward-pointing tick marks in Fig. 2. The normalised solutions for the current components then follow from Eqs. (3)–(5), giving iP ρi ω =2 1− , where iP D RDi J !1/8 !3/4 6P∗ 7 Ṁ iP D = BJ RJ J , (21a) 2π !2 ! IP ω ρi = 4π 1− , where IP D RDi J !1/4 !1/2 6P∗ 3 Ṁ 3 IP D = BJ RJ J , (21b) 2π iρ RDe =4 iρ D ρe 6P∗ Ṁ 2π iρD = !2 where !1/2 6P∗ 3 Ṁ 2π (21c) J , Iρ RDe = 8π IρD ρe IρD = ! ω 1− , J ! ! ω 1− , J !1/4 where !1/2 BJ R J 3 J , (21d) " ! !4 ! !# jk /B ω RDe ω =2 2 − 1+4 1− , J ρe J jk /B D where jk /B D = 6P∗ J , (21e) and " ! !8 ! !# jki ω ρi ω =2 2 − 1+4 1− , jkiD J RDi J where jkiD = 26P∗ BJ J . (21f) We note that Eqs. (21b) and (21d) are equivalent to Hill’s (2001) Eq. (A13), while Eqs. (21e) and (21f) are the same as Hill’s Eq. (A12). These normalised forms are plotted as solid 1 1 0.75 0.75 0.5 0.5 J. D. Nichols and S. W. H. Cowley: Magnetosphere-ionosphere0.25 coupling currents in Jupiter’s middle magnetosphere 0.25 PD IPiPêIêiPD 0.5 1 1.5 2 2.5 riêRDi IPIFig êIPD r êI rD 3a 2 10 1.75 10 20 1.5 8 8 15 1.25 1 1.5 2 2.5 riêRDi Fig 3a 6 61 10 4 0.75 4 0.5 2 0.25 IPiIrêI PD rêiêIrD rD 0.5 0.5 11 1.5 1.5 riêRDi 2.5 riêRDi 2.5 22 25 (a) êi rD3a rêI IirFig rD Figj3b H j3»» êBLêH »» êBLD 3 10 20 2.5 20 2.5 1 8 15 2 0.5 152 6 1.5 10 4 1 0.5 1 i rêi rD H j3»» êBLêH j»» êBLD 0.51 1 12 2 1.53 3 2 4 riêRDi 2.5 re êRDe 5 (c) 0.5 1 2 3 4 5 re êRDe 1 1 1 0.5 1 -0.5 -0.5 riêRDi 2.5 re êRDe (b) 5 2 4 2 3 4 2 2 3 3 1 2 1.5 3 4 4 2 4 5 re êRDe re êRDe 5 re êRDe 5 (d) Fig Fig 3c 3e Fig 3d ri êRDi 2.5 re êRDe 5 -1 -1 0.5 -1.5 j»»i ê j»»iD -2 Fig 3c 3b3d j»»iFig êFig j»»iD H j»» êBLêH j»» êBLD 1 1 0.5 0.5 -0.5 1 -1 -2 1.5 3 1 -1 5 0.5 -1.5 2.5 1 1.5 1 2 Fig Fig3b 3d 1.5 10 -0.5 25 0.5 2 0.5 1425 1 2 3 4 5 re êRDe 1 -1.5 -1.5 (e) -2 -2 Fig Fig3c3e j»»i ê j»»iD (f) Fig 3e Fig 3f 1 Fig. 3. Plots of normalised steady-state current components for a dipole magnetic field, plotted versus normalised equatorial radial distance (ρe /RDe ), or0.5normalised distance from the magnetic axis (ρi /RDi )0.5in the ionosphere, as appropriate. The plots show (a) the heightintegrated ionospheric Pedersen current intensity, (b) the azimuthri êRDi and height-integrated total ionospheric Pedersen current, (c) the current ri êRDi 0.5 1 1.5 2 2.5 sheet-integrated equatorial radial current intensity, (d) the azimuthand current sheet-integrated total1.5equatorial2 radial current, (e) the equa0.5 1 2.5 -0.5 torial field-aligned current density per unit magnetic field strength, and -0.5(f) the field-aligned current density just above the ionosphere. The corresponding-1normalization constants are given by Eq. (21). The solid lines show the full solutions given by Eqs. (14) and (21), while √ the 4 -1 long-dashed lines show the small√ and large ρe forms (the ‘S’ and ‘L’ approximations), shown to their point of intersection at (ρe /RDe ) = 2 -1.5 8 (or equivalently (ρi /RDi ) = 1/ 2), where (ω/J )S = (ω/J )L = 0. The downward-pointing tick marks show the limits of validity of -1.5 these approximate forms, as shown in Fig. 2. The short-dashed lines show the higher-order large ρe form (the ‘L0 ’ approximation) obtained -2 -2 from Eq. (20), whose limit of validity is indicated by the upward-pointing tick mark, as also shown in Fig. 2. Fig 3f Fig 3f lines in Fig. 3 versus either (ρe /RDe ) or (ρi /RDi ) as appropriate. The values and positions of principal features are also tabulated in Table 1 in normalised units, and in Table 2 in physical units. The dashed lines and tick marks in Fig. 3 then show approximate forms in the same format as Fig. 2 for the angular velocity. Specifically, for small ρe the long-dashed lines show the currents obtained by introducing Eq. (19) (the ‘S’ approximation into Eq. (21)). These currents are the same as Eq. (9) for a dipole field, when expressed in normalised form. This ‘S’ approximation is drawn to the point where (ω / J )S falls to zero. Beyond this we draw the currents obtained by introducing (ω/ J )L = 0 into Eq. (21) (the ‘L’ approximation), which are the same as Eq. (10) for the dipole, when expressed in normalised form. The long-dashed lines thus represent the current profiles that would be driven by an angular velocity profile given by the ‘S’ approximation to the point where falls to zero, with zero being taken beyond. The short-dashed lines then show the profiles obtained by introducing Eq. (20) (the ‘L0 ’ approximation) into Eq. (21). The normalised solutions given above show how the form and amplitude of the plasma angular velocity and currents vary with the system parameters for a dipole field. Specifically, Eqs. (13) and (16) show that the solutions scale spatially in the equatorial plane and in the ionosphere as ρe ∝ (6P∗ /Ṁ)1/4 and ρi ∝ (Ṁ/6P∗ )1/8 , respectively, while 1426 J. D. Nichols and S. W. H. Cowley: Magnetosphere-ionosphere coupling currents in Jupiter’s middle magnetosphere Table 2. Principal features of the plasma angular velocity and coupling current system for a dipole field in physical units Feature ρe RJ sin θi = Rρi J Maximum upward field-aligned current density (jk /B)max ≈ 0.10766P∗ (mho) pA m−2 nT−1 6P∗ (mho) Ṁ(103 kg s−1 ) jkimax ≈ 0.092066P∗ (mho)µA m−2 50.21 Maximum sheet-integrated equatorial radial current 1/2 iρmax ≈ 2.178 6P∗ (mho)Ṁ(103 kg s−1 ) mA m−1 6P∗ (mho) 54.30 Ṁ(103 kg s−1 ) Plasma angular velocity falls to ω J = 0.5 !1/4 0.1411 !1/4 74.80 6P∗ (mho) Ṁ(103 kg s−1 ) 85.67 6P∗ (mho) Ṁ(103 kg s−1 ) Ṁ(103 kg s−1 ) 6P∗ (mho) Ṁ(103 kg s−1 ) 0.1357 6P∗ (mho) !1/4 !1/8 !1/8 0.1156 Ṁ(103 kg s−1 ) 6P∗ (mho) 0.1080 Ṁ(103 kg s−1 ) 6P∗ (mho) 0.0890 Ṁ(103 kg s−1 ) 6P∗ (mho) !1/8 Maximum azimuth-integrated total current 1/4 Iρ max = 2 IP max ≈ 65.54 6P∗ 3 (mho)Ṁ(103 kg s−1 ) MA Field-aligned current passes through zero Maximum ionospheric Pedersen current 1/8 ∗ 7 3 −1 iP max ≈ 0.7381 6P (mho)Ṁ(10 kg s ) A m−1 126.34 Maximum downward field-aligned current density (jk /B)min ≈ −0.3526P∗ (mho) pA m−2 nT−1 jki min ≈ −0.30136P∗ (mho)µA m−2 i ∝ 6P∗ (1+γ ) 2 Ṁ (1−γ ) 2 (22) , where γ is equal to zero for the sheet-integrated equatorial radial current, 1/2 for the azimuth-integrated total fieldperpendicular current, 3/4 for the height-integrated ionospheric Pedersen current, and 1 for the field-aligned current density. The fact that these spatial and amplitude scales combine to produce a linear dependence of the current on Ṁ for small ρe , as given by Eq. (9), and a linear dependence on 6P∗ at large ρe , as given by Eq. (10), implies that the currents grow with a specific power of the distance in the inner region, and decline with a specific power of the distance at large distances. It is easy to show that at small distances the currents grow as 2(1+γ ) iS ∝ Ṁρe ∝ Ṁ 4(1+γ ) (23a) , ρi while at large distances they decline as iL ∝ 6P∗ 2(1−γ ) ρe 4(1−γ ) ∝ 6P∗ ρi , 6P∗ (mho) Ṁ(103 kg s−1 ) ∞ Eq. (21) shows that the amplitude of each component of the current system scales as some power of 6P∗ and Ṁ of the form (23b) !1/4 !1/4 !1/8 !1/8 0 as may be readily verified by substituting the appropriate form for the angular velocity (i.e. the ‘S’ or ‘L’ approximations) into Eq. (21). Thus, in summary, the currents grow in the inner region according to Eq. (23a), and depart from this behaviour at an equatorial distance proportional to (6P∗ /Ṁ)1/4 (as shown by the ‘inner’ downward tick marks in Fig. 3), where the current value depends on 6P∗ and Ṁ according to Eq. (22). Similarly, the currents decline in the outer region according to Eq. (23b), starting at an equatorial distance proportional to (6P∗ /Ṁ)1/4 (as shown by the ‘outer’ downward tick marks in Fig. 3), where the current value again depends on 6P∗ and Ṁ according to Eq. (22). 4 Plasma angular velocity and coupling current system for a current sheet magnetic model The solution for the coupling currents for a dipole field represents an important paradigm case. Nevertheless, the model is unrealistic in its application to Jupiter because the middle magnetosphere field lines are not quasi-dipolar, but are significantly distorted outward from the planet by azimuthal currents flowing in the equatorial plasma, as shown in Fig. 1. Thus field lines at a given radial distance in the equatorial plane map to a significantly lower latitude in the ionosphere J. D. Nichols and S. W. H. Cowley: Magnetosphere-ionosphere coupling currents in Jupiter’s middle magnetosphere »Bze »ênT ze»ênT »B 1000 1000 100 100 10 10 11 0.1 0.1 Feeze ênT RJJ 22 »B »ênTR F ênT 20 20 40 40 60 60 80 80 100 100 120 120 êRJJ rreeêR (a) Fig 4a 4a Fig 80000 80000 1000 60000 60000 100 40000 40000 10 20000 20000 1 0.1 êdeg 2 qqFiiêdeg e ênT RJ 25 25 20 20 20 40 40 40 60 60 60 80 80 80 100 100 100 êRJJ rreeêR 120 re êRJ 120 120 (b) 1427 Bze versus equatorial radial distance (the actual values are, of course, all negative), while the dashed line shows the dipole field for comparison. The model field departs from the dipole in the inner part of the middle magnetosphere, and remains significantly lower in magnitude throughout the region of interest, reflecting the outward distension of the current sheet field lines. The model employs the “Voyager-1/Pioneer-10 model” of Connerney et al. (1981) (the “CAN” model) out to a certain radial distance (using the analytic approximations derived by Edwards et al., 2001), and the empirical Voyager-1 outbound model of Khurana and Kivelson (1993) (the “KK” model) beyond. The radial distance at which these models are joined, ρe∗ ∼ 21.78 RJ , indicated by the “kink” in the solid curve in Fig. 4a, is determined from the intersection of the two model curves, such that there is no discontinuity in the field magnitude at this point (only in the first derivative). The expression for the field in the “CAN” region has been given previously by Cowley and Bunce (2001) and Cowley et al. (2002), and will not be repeated here. The expression for the field in the “KK” region, however, is simply a power law given by Fig4b 4a Fig 4b Fig 80000 20 20 Bze = −B0 60000 15 15 40000 10 10 20000 55 qi êdeg 25 2020 20 4040 40 6060 60 8080 80 100 100 100 êR rreerêR e êR JJ J 120 120 120 (c) Fig 4c 4c Fig Fig 4b Fig. 4.20 Plots showing parameters of the current sheet field model employed in Sect. 4 (solid lines), compared with values for the planetary dipole field alone (dashed lines). Plot (a) is a log-linear plot 15 of the modulus of the north-south equatorial magnetic field |Bze | threading the equatorial plane, shown versus jovicentric equatorial 10 radial distance ρe . This field component is actually negative (i.e. points 5south) in both cases. The kink in the curve at ∼21.78 RJ in the current sheet model marks the point where we switch from the re êRJ Plot (b) ‘CAN’ model to the ‘KK’ model, as discussed in the120 text. 20 40 60 80 100 similarly shows the equatorial flux function Fe of the model fields Fig 4c versus jovicentric equatorial radial distance ρe . Plot (c) shows the mapping of the field lines between the equatorial plane and the ionosphere, determined from Eq. (1). The ionospheric dipole co-latitude of the field line is plotted versus jovicentric equatorial radial distance ρe . than for a dipole, thereby increasing the electric field and current for a given departure of the plasma from rigid corotation. In their previous investigations, Cowley and Bunce (2001) and Cowley et al. (2002) employed an empirical model of the equatorial field based on Voyager magnetic data. This model will also be used here, its properties being illustrated in Fig. 4. The solid line in Fig. 4a shows a log-linear plot of the modulus of the equatorial north-south magnetic field RJ ρe m , (24) where B0 = 5.4 × 104 nT and m = 2.71. This function was determined from a fit to outbound Voyager-1 data over the range from ∼20 to ∼100 RJ , corresponding approximately to the range over which we employ it here. The equatorial flux function Fe satisfying Eq. (2) is shown by the solid line in Fig. 4b, where the dashed line again shows the dipole value (Eq. 11b). The value of Fe at ρe∗ is set by the CAN model, equal to ∼3.70×104 nT R2J , while beyond this, in the “KK” region, integration of Eq. (2) using Eq. (24) for Bze yields !m−2 B0 RJ2 RJ Fe (ρe ) = F∞ + , (25) (m − 2) ρe where F∞ , the model value of Fe at infinity, is ∼2.85×104 nT R2J . It can be seen in Fig. 4b that the value of Fe for the current sheet model is much larger than for the dipole at a given equatorial distance, and varies over only a narrow range in the outer middle magnetosphere. Since the value of Fe is directly related to the magnetic co-latitude where the field lines map to the ionosphere through Eq. (1), the implication is that the current sheet field lines map to significantly larger co-latitudes than for the dipole, and also to a very narrow co-latitude range. This is shown explicitly in Fig. 4c, where we plot the co-latitude of the field lines in the ionosphere versus equatorial radial distance. In the current sheet model (solid line), the ionospheric mapping varies from a co-latitude of ∼16.7◦ at 30 RJ to ∼15.6◦ at 120 RJ , a range of only ∼1.1◦ . Even the current sheet field line from infinity, should the model (unrealistically) be taken to extend that far, only maps to ∼15.0◦ . Field lines at smaller co-latitudes then 1428 J. D. Nichols and S. W. H. Cowley: Magnetosphere-ionosphere coupling currents in Jupiter’s middle magnetosphere do not thread the current sheet in this model, but must map instead to the outer magnetosphere and magnetic tail, regions which are not described by the present theory. In the dipole model, by contrast, equatorial field lines in the range 30 to 120 RJ map between ∼10.5◦ and ∼5.2◦ , a range of ∼5.3◦ , and go to the pole, of course, at infinity. Solutions for such a “current sheet” field must generally be computed numerically for specific values of the system parameters, and results have been presented to date by Cowley et al. (2002, 2003) for a few spot values. Here we present an approximate analytic solution which applies to the region beyond ρe∗ ∼21.78 RJ , where the field varies with distance as a power law, which previous work has shown to be the main current-carrying region. However, we must first enquire how solutions in the power law region depend on conditions inside the region, where the dipole field is dominant and the transition to the power law takes place. We commented previously for the dipole problem that solutions of the HillPontius equation which are started at an arbitrary angular velocity well within the “Hill distance” converge rapidly onto the solution which rigidly corotates at small distances, such that the behaviour at larger distances is very insensitive to the choice of initial condition. Numerical investigation shows that the solutions for the current sheet field exhibit the same property (Cowley and Bunce, 2002). The implication for the present problem is that, provided the effective “Hill distance” is larger than ρe∗ ∼20 RJ (i.e. provided the value of (6P∗ /Ṁ) is not too low), the solutions in the “power law” region will be very insensitive to conditions in the interior region. In this case, we can simply take the power law field to be valid over all distances, but apply the results only to the region outside of ρe∗ . The validity of this statement may be judged from Fig. 5, where we show solutions for the plasma angular velocity in the inner part of the system spanning ρe∗ , for three values of (6P∗ /Ṁ) covering our range of interest, i.e. 10−4 , 10−3 and 10−2 mho s kg−1 . The solid lines show numerical solutions using the full current sheet field model shown in Fig. 4, while the dashed lines similarly show numerical solutions using the power law field over the whole range. (The dot-dashed lines show the analytic approximation to be derived below.) Both numerical solutions were initialised by imposing the near-rigid corotation approximation given by Eq. (8) at ρe = 5 RJ . The position of ρe∗ is indicated by the tick mark in each plot, such that both models use the same power law field at larger distances. It can be seen that the two numerical solutions converge rapidly beyond this distance, the convergence becoming increasingly rapid as (6P∗ /Ṁ) increases. Thus, in the parameter range of interest, the solutions in the power law field region can be approximated by taking the power law field to be valid at all distances. We note that the values of the “Hill distance” corresponding to the values of (6P∗ /Ṁ) shown in the figure are 27.7, 49.2, and 87.5 RJ , thus exceeding ρe∗ ∼21.78 RJ in each case, though only just so at the lower limit. Convergence of the two solutions is found to break down for lower values of (6P∗ /Ṁ) ∼ 10−5 mho s kg−1 , corresponding to a “Hill distance” of 15.6 RJ , at the limit of the parameter range considered here. We thus consider solutions for the case in which the equatorial field is taken to be given by Eq. (24) at all distances. To obtain an analytic result we also make the further approximation that the flux function is taken to be a constant in the Hill-Pontius equation. Thus, over the region of interest, the equatorial field is taken to map in the ionosphere to a narrow range of distances from the magnetic axis, an approximation shown to be well satisfied for the empirical current sheet model discussed above. While this approximation will generally be valid for “current sheet” fields, it is clearly not valid for quasi-dipolar fields. We thus note that the solutions obtained here do not reduce to the dipole case in the limit that we choose m = 3 in Eq. (24). With this “current sheet” approximation, then, Eq. (6b) becomes ω ω RCSe m ω ρe d + =2 1− , (26) 2 dρe J J ρe J where RCSe is the equatorial “Hill distance” for the power law current sheet field (subscript ‘CS’) !1/m 2π 6P∗ B0 F0 RCSe = . (27) RJ Ṁ Here we have put Fe = F0 , a constant, into Eq. (6b), such that the field lines are taken to map in the ionosphere to a fixed q distance from the magnetic axis given by (ρi0 /RJ ) = (F0 /BJ RJ2 ) (Eq. 1). The value of F0 could be taken for example, to be equal to F∞ in Eq. (25) (in which case (ρi0 /RJ ) = (ρi∞ /RJ ) where (ρi∞ /RJ ) = √ 2 (F∞ /BJ RJ ) ≈0.258, corresponding to a co-latitude of ◦ ∼14.95 ), or to some nearby (larger) value representative of the field lines in the region of interest. Equation (26) is then of the same form as Eq. (12) for the dipole field (they are identical when m = 4), from which it is clear that the solutions are functions only of ρe /RCSe , and hence scale with distance as RCSe and with the system parameters as (6P∗ /Ṁ)1/m . With m = 2.71, therefore, as used throughout here, the scale length varies somewhat more rapidly with the system parameters than for the dipole, which varies as (6P∗ /Ṁ)1/4 . The general solution of Eq. (26) can again be found by the integration factor method " 2 # ω 4 m RCSe 2 4 RCSe m = exp × J m ρe m ρe " # 2 4 RCSe m × 0 1− , +K , m m ρe where 0(a, z) is the incomplete gamma function Z ∞ 0(a, z) = e−t t a−1 dt. (28a) (28b) z The solutions again diverge at the origin except for the special solution with K = 0, which rigidly corotates for small J. D. Nichols and S. W. H. Cowley: Magnetosphere-ionosphere coupling currents in Jupiter’s middle magnetosphere HwêWJ LL HwêW JJ 11 function only of -4 -1 °° L = 10-4 HSP***êM êM mho ss kg kg-1 -1 HS L = 10 -4 mho PP 0.9 0.9 0.8 0.8 0.7 0.7 0.6 0.6 0.5 0.5 0.4 0.4 HwêWJ LL HwêW JJ 11 10 10 20 20 30 30 40 40 êRJ rreêR 50 ee JJ 50 (a) Fig 5a 5a Fig -1 -3 °° L = 10-3 HSP***êM êM mho ss kg kg-1 -1 HS L = 10 -3 mho PP 0.95 0.95 1ρi RCSi = RCSe ρe m−2 (30) , where 1ρi = (ρi − ρi∞ ), and ρi∞ is the distance from the magnetic axis of the field line from infinity as given above. In deriving Eq. (30) we have assumed that 1ρi is small compared with ρi∞ , in keeping with the “current sheet” approximation introduced above. Numerically, for the above power law field we find ! 1 2.71 6P∗ (mho) RCSe ≈ 56.38 RJ Ṁ 1000kg s−1 and 0.9 0.9 0.85 0.85 Ṁ 1000kg s−1 RCSi ≈ 0.0197 RJ 6P∗ mho 0.8 0.8 HwêWJ LL HwêW JJ 11 1429 10 10 20 20 30 30 40 40 êRJ rreêR 50 ee JJ 50 (b) -2 -1 °° L = 10-2 HSP***êM êM mho ss kg kg-1 -1 HS L = 10 -2 mho PP 0.995 0.995 Fig 5b 5b Fig 0.99 0.99 0.985 0.985 0.98 0.98 0.975 0.975 0.97 0.97 10 10 20 20 30 30 40 40 êRJ rreêR 50 ee JJ 50 (c) Fig 5c 5c Fig Fig. 5. Plots showing plasma angular velocity profiles versus equatorial radial distance for (6P∗ /Ṁ) equal to (a) 10−4 , (b) 10−3 , and (c) 10−2 mho s kg−1 . The solid lines show the solution obtained by numerical integration of Eq. (6b) using the full ‘current sheet’ magnetic model shown in Fig. 4, starting from the near-rigid corotation approximation Eq. (8) at ρe = 5 RJ . The tick marks show the point (ρe∗ ≈21.78 RJ ) where the magnetic field switches from the ‘CAN’ model to the power-law ‘KK’ model. The dashed lines then show the numerical solution obtained by employing the ‘KK’ power law field (given by Eqs. 24 and 25) over the full distance range, the solutions again being initialised using the appropriate form of Eq. (8) at ρe = 5 RJ . The dot-dashed lines show the approximate analytic solution using the ‘KK’ power law field, given by Eq. (28) with K = 0 and m = 2.71. Note that the vertical scale has been tailored to the plot in each case. ρe . To map the solution to the ionosphere we equate Eqs. (1) and (25), and define an ionospheric scaling distance s 1− 2 m BJ RJ2 B0 Ṁ RCSi 1 = ,(29) ∗ RJ F∞ 2π 6P B0 F0 2 m − 2 BJ such that the angular velocity mapped to the ionosphere is a ! 0.71 2.71 , (31) where we have chosen to put F0 = Fe (70 RJ ) ≈ 3.22 × 104 nT RJ2 , a representative value in the middle magnetosphere current sheet. Thus, as (6P∗ /Ṁ) varies over the range of interest from 10−4 to 10−2 mho s kg−1 , we find that RCSe varies between 24.1 and 131.9 RJ (compared with 27.7 to 87.5 RJ for RDe for the dipole), while RCSi varies between 0.046 and 0.0084 RJ (compared with 0.19 to 0.11 RJ for RDi for the dipole). Consequently, since (ρi∞ /RJ ) ≈ 0.258, as indicated above, we will indeed have 1ρi small compared with ρi∞ for values 1ρi ∼ RCSi . The solid lines in Figs. 6a and b show the normalised angular velocity solution given by Eq. (28) with K = 0 and m = 2.71, plotted versus (ρe /RCSe ) in the equatorial plane, and versus (1ρi /RCSi ) in the ionosphere, respectively. The form is similar to that for the dipole, though falling away from rigid corotation more quickly (in normalised units) in the inner region, and less quickly in the outer region. This solution is also shown in un-normalised form (with the above value of F0 ) by the dot-dashed lines in Fig. 5, where it is compared with the results of numerical integration of the full solution (solid and dashed lines as described above). It can be seen that the analytic solution forms a very close approximation to the numerical solutions for ρe > ρe∗ under all conditions of interest here, a result we have confirmed by a wider comparative study not illustrated here. The dashed lines and tick marks in Fig. 6 show normalised approximate forms and their regimes of validity, in the same format as Fig. 2. Specifically, the long-dashed lines show the smallρe (‘S’) approximation given by Eq. (8) m ω 1 RCSi m−2 1 ρe m =1− =1− , (32) J S 2 RCSe 2 1ρi where we again note that the series generated by Eq. (7) (of which Eq. (32) is the leading term) is the same as that obtained by asymptotic expansion of the gamma function in Eq. (28) for large argument. The short-dashed lines 1430 J. D. Nichols and S. W. H. Cowley: Magnetosphere-ionosphere coupling currents in Jupiter’s middle magnetosphere F0 IP CS = 6P∗ BJ RJ2 J , (34b) BJ RJ2 iρ RCSe ω =4 1− , where iρCS ρe J wêWJ wêW 1 J 1 0.8 0.8 0.6 0.6 0.4 iρCS = 0.2 0.2 1 2 3 4 5 6 1 2 3 4 5 6 wêWJ re êRCSe reFig êRCSe 6a (a) Fig 6a 1 J wêW 1 0.8 0.8 0.6 0.6 0.4 0.4 0.2 0.2 0.5 1 1.5 2 2.5 3 3.5 0.5 1 1.5 2 2.5 3 3.5 Dri êRCSi (b) Dri êRCSi Fig 6b Fig. 6. Plots of the approximate analytic plasma angular velocity profile for the current sheet power law magnetic field model, given by Eq. (24) with m = 2.71, shown (a) versus (ρe /RCse ) in the equatorial plane, and (b) versus (1ρi /RCsi ) in the ionosphere. The solid line in each case shows the full solution obtained from Eq. (28) with K = 0, such that the plasma rigidly corotates at small radial distances. The long-dashed lines show the small-ρe (‘S’) form given by Eq. (32), while the large-ρe (‘L’) form is just (ω/J )L = 0. The downward-pointing tick marks indicate the limits of validity of both these approximations as defined for the dipole case shown in Fig. 2. The short-dashed lines show the higher-order large-ρe (‘L0 ’) form given by Eq. (33), whose limit of validity (defined as for the dipole case) is indicated by the upward-pointing tick mark. The horizontal dotted line indicates the condition for rigid corotation, (ω/J ) = 1. then show the higher-order large-ρe (‘L0 ’) approximation, obtained from Eq. (28) as ω J = L0 4 m 2 m 2 RCSe 2 0 1− . m ρe (33) The lower-order large-ρe (‘L’) approximation is again simply (ω/J )L = 0. The normalised approximate solutions for the currents then follow from Eqs. (3)–(5) iP ω =2 1− , where iP CS J s iP CS = IP IP CS F0 6P∗ BJ RJ J , 2 BJ RJ ω = 4π 1 − , J where (jk /B) ρe m−2 =4 × (jk /B)CS RCSe " # ω RCse m ω × −2 1− , J ρe J Fig 6b 1/m F0 Ṁ 6P∗ BJ RJ J , 2π6P∗ B0 F0 BJ RJ2 Iρ ω = 8π 1 − , where IρCS J F0 IρCS = 6P∗ BJ RJ2 J , BJ RJ2 0.4 (34a) (jk /B)CS = × BJ B0 2π6P∗ B0 F0 jki jki CS " × (34d) where F0 × BJ RJ2 1− 2 m 6P∗ J , Ṁ RCSi =4 × 1ρi ω J (34c) 1ρi −2 RCSi m m−2 and ω 1− J # , (34e) where BJ F0 jk iCS = 2 × B0 BJ RJ2 × 2π6P∗ B0 F0 Ṁ 1− 2 m 6P∗ BJ J . (34f) These forms are shown by the solid lines in Fig. 7, plotted versus either (ρe /RCsi ) or (ρi /RCsi ) as appropriate. The dashed lines show approximate forms based on the ‘S’, ‘L’, and ‘L0 ’ approximations for the angular velocity, in the same format as Fig. 3 for the dipole. Comparison with Fig. 3 shows similarities, but also major differences with the currents for the dipole field. The differences arise from the fact that the current sheet field lines reach the ionosphere in a narrow band at a finite co-latitude, rather than continuously approaching the pole with increasing radial distance, as for the dipole. The ionospheric Pedersen current (Eq. 34a), while being proportional q to the displacement of the band from the magnetic axis F0 /BJ RJ2 , then varies with co-latitude only through the variation of the plasma angular velocity. As seen in Fig. 7a, the Pedersen current, therefore, peaks at the poleward edge of the band, where the angular velocity is zero, 0.5 0.5 J. D. Nichols and S. W. H. Cowley: Magnetosphere-ionosphere coupling currents in Jupiter’s middle magnetosphere IiPPêIêiPCS PCS 0.5 1 1.5 2 2.5 3 3.5 Dri êRCSi I rêI rCS IPêIPCS 25 Fig 7a 2 12 1 1.5 2 2.5 3 3.5 1431 Fig 7a 12 20 10 10 1.5 8 15 8 1 6 6 10 4 0.5 4 5 2 2 I rêI rCS IPi rêIêiPCS rCS 253.5 0.5 Dri êRCSi 0.5 0.5 11 1.5 1.5 22 2.5 2.5 33 3.5 3.5 Dr DriiêR êRCSi CSi (a) 12 3 2010 2.5 1 0.5 HIirjrêI j êBL »»êiêBLêH »» CS rCS rCS Fig 4 7a7b 3.5 Fig 25 3.5 3 20 2.5 2 1 3 1.5 2 4 2.5 3 4 44 5 55 4 5 3 5 3.5 re êRCSe Dr 6 i êRCSi (b) Fig 7d Fig 7b 3 2.5 15 82 152 6 1.5 10 4 1 1.5 1.5 10 1 1 5 2 0.5 5 0.5 0.5 i rêi rCS H j »» êBLêH j »» êBLCS 3.5 4 0.5 1 1 122 1.5 3 3 2 44 2.5 553 3.5 66 Dr êRCSe CSi rreeiêR êR CSe 2 Fig 7c »»i ê jFig »»iCS H j »»jêBLêH j 7b êBLCS Fig »» 7d 24 11 (c) 3 3.5 1.75 3.5 2.53 1.5 3 2.5 2 1.25 2.5 2 1.5 12 1.5 1 1 0.5 0.5 1.5 0.75 1 2 22 33 re êRCSe rreeêR êRCSe CSe 66 6 (d) Fig Fig 7c 7e Fig 7d 0.5 1 1 1 j»»i ê j»»iCS 2 2 2 3 3 4 4 5 5 reêRCSe 6 re êRCSe 6 (e) 0.5 0.25 Fig 7c 0.5 j»»i ê j»»iCS Fig 7e 2 1 1 2 1.5 3 2 2.5 3 reDr êRCSe i êRCSi 6 3.5 (f) FigFig 7e 7f Fig. 7. Plots of normalised steady-state current components for a power 1.75law equatorial magnetic field (Eq. (24) with m = 2.71) and ‘current 1.75 sheet’ approximate mapping to the ionosphere, plotted versus (ρe /RCSe ) or (1ρi /RCSi ) as appropriate. As in Fig. 3 for the dipole, the 1.5 1.5 show (a) the height-integrated ionospheric Pedersen current intensity, (b) the azimuth- and height-integrated total ionospheric Pedersen plots 1.25 (d) the azimuth- and current sheet-integrated total equatorial radial current, (c) the current sheet-integrated equatorial radial current intensity, 1.25 current, (e) the equatorial field- aligned current density per unit magnetic1field strength, and (f) the field-aligned current density just above the 1 ionosphere. The normalization constants are given by Eq. (34). The solid lines show the full approximate solutions given by Eqs. (28) and 0.75 0.75 (34), while the long-dashed lines show the small and large-ρ forms derived from (ω/J )S given by Eq. (32) and (ω/ J )L = 0, drawn to e √ m 0.5 their 2 . The downward-pointing tic-marks show the limits of validity of these approximate forms as 0.5 point of intersection at (ρe /RCSe ) = 0.25large-ρe form given by Eq. (33), whose limit of validity is indicated defined for the dipole case. The short-dashed lines show the higher-order by0.25 the upward-pointing tick mark, again defined as for the dipole case. Dr êRCSi 0.5 1 1.5 2 2.5 3 3.5 Dri êRCSi and falls monotonically with distance from the boundary as the angular velocity approaches rigid corotation (Fig. 6b). This implies that the azimuth-integrated total current also varies monotonically with distance, the total equatorial current (Eq. 34d) thus rising with increasing equatorial distance towards 8π F0 6P∗ J (strictly, 8π F∞ 6P∗ J ) at infinity, as seen in Fig. 7d. This behaviour also implies that the radial current intensity (Eq. 34c) rises to a peak value with increas- 0.5 Fig 7f 1 1.5 2 2.5 3 3.5 i ing distance, and then falls as ρe−1 at large distances, as seen in Fig. 7c. The further implication of a monotonically increasing total current is that the field-aligned current is unidirectional, flowing consistently from the ionosphere to the equatorial current sheet, as shown in Figs. 7e and f. Closure of the current system must then occur outside the region described by the model, on field lines mapping between the ionosphere at higher latitudes and the outer magnetosphere Fig 7f 1432 J. D. Nichols and S. W. H. Cowley: Magnetosphere-ionosphere coupling currents in Jupiter’s middle magnetosphere Table 3. Principal features of the plasma angular velocity and coupling current system for the power law current sheet field in normalised units, obtained (with m = 2.71) from the approximate analytic solution of Sect. 4 Feature Maximum sheet-integrated equatorial radial current (iρ /iρCS )max ≈ 1.2109 Plasma angular velocity falls to ω =0.5 J Maximum upward field-aligned current density (jk /B)/(jk /B)CS = jki /jkiCS ≈ 1.5274 max max ρe RCse = 2 IP /IP CS max max 1ρi RCsi ω J 1.6142 0.7118 0.5113 1.6521 0.7002 0.5 2.3777 0.5407 0.3339 ∞ 0 0 Maximum height-integrated ionospheric Pedersen current (iP /iP CS )max = 2 Maximumazimuth-integrated total current Iρ /IρCS = 8π ≈ 25.133 Field-aligned current goes to zero Table 4. Principal features of the plasma angular velocity and coupling current system for the power law current sheet field in physical units, obtained (using B0 = 5.4 × 104 nT, m = 2.71, F∞ ≈ 2.85 × 104 nT R2j and F0 ≈ 3.22 × 104 nT R2j ) from the approximate analytic solution of Sect. 4 Feature Maximum sheet-integrated equatorial radial current 1 2.71 iρ max ≈ 8.690 6P∗ (mho)1.71 Ṁ(103 kg s−1 ) mA m−1 Plasma angular velocity falls to ω J Maximum upward field-aligned current density (jk /B)max ≈ 1 2.71 2.808 6P∗ (mho)3.42 Ṁ(103 kg s−1 )−0.71 pA m−2 nT−1 ∗ 1/2.71 6P (mho) 91.02 −1 3 Ṁ(10 kg s = 0.5 ρe RJ 93.15 6P∗ (mho) Ṁ(103 kg s−1 ) 134.06 ) !1/2.71 6P∗ (mho) Ṁ(103 kg s−1 ) 1ρi RJ 0.71 Ṁ(103 kg s−1 ) 2.71 0.01400 6 ∗ (mho) P 0.71 Ṁ(103 kg s−1 ) 2.71 0.01377 6 ∗ (mho) P 1/4 0.71 Ṁ(103 kg s−1 ) 2.71 0.01063 6 ∗ (mho) P jk i max ≈ 2.404(6P∗ (mho)3.42 Ṁ(103 kg s−1 )−0.71 µA m−2 Maximum height-integrated ionospheric Pedersen current iP max ≈ 2.9506P∗ (mho) A m−1 Maximum azimuth-integrated total current Iρ max = 2IP max ≈ 725.86P∗ (mho) MA Field-aligned current goes to zero and magnetic tail. The values and positions of principal features of the solution are again tabulated in Table 3 in normalised units, and in Table 4 in physical units. The behaviour of these approximate solutions thus reflects the results presented previously by Cowley and Bunce (2001) and Cowley et al. (2002, 2003), using the full current sheet field model shown in Fig. 4. One minor difference is that in the numerical solutions the total equatorial (and ionospheric) current rises with increasing distance to a maximum value slightly above 8πF∞ 6P∗ J before falling with decreasing F ∞ 0 to the latter value at infinity, rather than following the strictly monotonically rising behaviour of the approximation. Correspondingly, the field-aligned current in the numerical solutions reverses to small negative values (given by Eqs. 10e and f) at large radial distances (and hence, close to the poleward boundary in the ionosphere), rather than going to zero as in the approximation (Fig. 7f), though the net current closure is small. However, for the range of system parameters considered here, the maximum in the total current and the concurrent reversal of the field-aligned current typically take J. D. Nichols and S. W. H. Cowley: Magnetosphere-ionosphere coupling currents in Jupiter’s middle magnetosphere place at equatorial distances of several hundred to several thousand RJ , far beyond the limit of physical applicability of the model. Within the region of applicability, the agreement between the numerical and approximate analytic results is found to be very good. In like manner to the dipole results, the normalised solutions given above show how the form and amplitude of the plasma angular velocity and currents vary with the system parameters in the case of a power law current sheet field. Equations (27) and (29) show that the solutions scale spatially in the equatorial plane and in the ionosphere as ρe ∝ (6P∗ /Ṁ)1/m and 1ρi ∝ (6P∗ /Ṁ)1−2/m , respectively, while Eq. (34) shows that the amplitude of each component of the current system scales as some power of 6P∗ and Ṁ of the same form as Eq. (22), but with γ equal to 1–2/m for the equatorial radial current, 1 for the Pedersen current and azimuth-integrated total field-perpendicular current (such that these currents scale linearly with 6P∗ and are independent of Ṁ), and 3–4/m for the field-aligned current density. Since these values of γ are consistently higher for a given current component for the current sheet model than for the dipole (at least for m > 2, as investigated here), the implication is that the currents scale as a somewhat higher power of the conductivity for the current sheet model than for the dipole, and as a somewhat lower power of the mass outflow rate. The corresponding behaviours at small and large distances, such that the solutions obey Eqs. (9) and (10), are m iS ∝ Ṁρe2 (1+γ ) ∝ Ṁ (m(1+γ )/2(m−2)) 1ρi (35a) and 6P∗ (m(1−γ )/2(m−2)) ∝ 6P∗ 1ρi , (35b) m(1−γ )/2 ρe as can be verified by substituting the appropriate approximations (‘S’ and ‘L’) for the angular velocity into Eq. (34). Thus, for example, with γ = 1–2/m, the equatorial radial current increases as ρem−1 in the inner region and falls as ρe−1 at large distances, while the field-aligned current with γ = 3–4/m grows as ρe2(m−1) in the equatorial plane in the inner region and approaches zero in this approximation at large distances, as indicated above (Figs. 7e, f). The spatial variation of the field-aligned current in the large-distance limit may then be obtained from the higher-order large-distance approximation (Eq. 33), from which it is found that the current varies as ρe−(4−m) in the equatorial plane, and as (4−m)/(m−2) 1ρi in the ionosphere. iL ∝ 5 Comparison of system behaviour for the dipole and current sheet field models In this section we finally provide a summary and comparison of how the major features of the plasma flow and coupling current system vary with 6P∗ and Ṁ for the dipole and current sheet field models. Specifically, we consider the location of corotation breakdown, the magnitudes and locations 1433 of the peak values of the various current components, and the latitudinal width in the ionosphere of the region of upwarddirected field-aligned current. With the exception of the latter parameter, in effect we here provide plots showing how the quantities in Tables 2 (for the dipole) and 4 (for the power law field approximation) vary with 6P∗ and Ṁ. We also compare the approximate results for the current sheet field with spot values obtained by numerical integration using the full current sheet field. Figure 8 shows how the spatial scale on which plasma corotation breaks down depends on 6P∗ and Ṁ for the two models. Specifically, we show the position where (ω/J ) = 0.5, as previously given in Tables 1–4. In Fig. 8a the equatorial distance is plotted versus 6P∗ in log-log format for Ṁ = 100, 1000 and 10 000 kg s−1 , while in Fig. 8b it is plotted versus Ṁ in similar format for 6P∗ = 0.1, 1 and 10 mho. Solid lines give results for the dipole field obtained from Eqs. (13) and (14), showing that the distance in∗1/4 creases with the conductivity as 6P , and decreases with the mass outflow rate as Ṁ −1/4 . The dashed lines show corresponding results obtained from the power law field approximate solutions Eqs. (27) and (28) (with m = 2.71 and F0 ≈3.22×104 nT R2J as above), which, of course, are not applicable to the full field model at distances smaller than ρe∗ ≈21.78 RJ . These increase more rapidly with 6P∗ and ∗1/2.71 decrease more rapidly with Ṁ, as 6P and Ṁ −1/2.71 , respectively. Overall, however, the equatorial distances of corotation breakdown are similar for the dipole and current sheet fields as noted above, but are generally somewhat larger for the current sheet model than for the dipole, particularly for larger values of 6P∗ and smaller values of Ṁ. The solid dots in the figures provide spot values obtained by numerical integration of the full current sheet solution, their close association with the dashed lines clearly indicating the values of Ṁ (in Fig. 8a) and 6P∗ (in Fig. 8b) employed. This close association also confirms that the analytic solutions provide good approximations to the numerical results in the power law regime over essentially the whole parameter range considered here. The only notable deviations occur at small 6P∗ and large Ṁ, where corotation breakdown occurs at equatorial distances approaching the radial limit of the power law field region at ρe∗ ≈21.78 RJ . In this case the numerical results give somewhat larger distances than the analytic approximation, as also seen in Fig. 5. Corresponding results projected to the ionosphere are shown in Figs. 8c and 8d, in a similar format. The horizontal dotted line at θi ≈14.95◦ shows the co-latitude of the current sheet field line from infinity (the corresponding limit for the dipole being, of course, the pole at θi = 0◦ ). These plots again emphasise the significantly larger distance from the magnetic axis at which plasma corotation breaks down in the ionosphere for the current sheet field than for dipole, despite the similarity of the equatorial results. They also display the relative lack of response of this distance to the system parameters in the current sheet model, this forming the basis of the “current sheet” approximation Fe ≈ F0 employed to obtain the analytic results ° ° -1 -1 J. D. Nichols and S. W. H. Cowley: Magnetosphere-ionosphere coupling currents in Jupiter’s middle magnetosphere MHkg s sL L MHkg re HwêW êR êR re HwêW J = 0.5L J = 0.5LJ J 500 500 1434 ° 10 ° 10 MHkg s-1sL-1 L MHkg 2 2 re HwêW êRJêRJ re HwêW J = 0.5L J = 0.5L 500500 10221022 1010 103103 200 200 re HwêW êRJêRJ re HwêW J = J0.5L = 0.5L 500500 re HwêW êRJêRJ re HwêW J = 0.5L J = 0.5L 500500 200200 10231032 10310 3 10 10 104104 10341043 104104 104104 200200 100 100 100100 5050 50 50 2020 2020 0.10.1 0.20.2 0.10.1 0.20.2 qi HwêW êdeg qi HwêW êdeg J = J0.5L = 0.5L 0.50.5 1 1 2 2 5 5 * * S PS HmhoL P HmhoL 1010 1010 1.0 101.0 10 1.01.0 20 20 200200 8a8a * Fig Fig SP SHmhoL P HmhoL 200200 10 10 (a) êdeg ° ° -1 -1Figqi8a HwêW qi HwêW êdeg J = J0.5L = 0.5L MHkg s sL L Fig 8a MHkg 500500 1000 1000 2000 2000 0.50.5 1 1 2 2 5 5 104104 3 ° 10 ° 310-1 -1 MHkg 2s 2 sL L M 10Hkg 10 104104 103103 2 2 15 15 1010 10 10 107 10 7 104104 10 7 10 7 75 57 103 34 10410 10 57 57 10 10 102102 0.50.5 1 1 2 2 5 5 * * S PS HmhoL P HmhoL 1010 (c) M 8b Hkg s sL-1 L FigFig 8b M Hkg 5000 500010000 10000 (b) . -1 * * SPFig HmhoL Fig S8b HmhoL P 8b 0.10.1 1.01.0 * 10 * SP10 SHmhoL P HmhoL 0.1 15 15 1010 5 5 3 3 500500 1000 1000 2000 2000 qi HwêW = 0.5L êdeg qi HwêW êdeg 15J 15J = 0.5L 10321023 1.00.1 0.1 1.0 1.01.0 0.10.1 0.10.1 . . M Hkg s-1sL-1 L M Hkg 0.1 0.1 5000 500010000 10000 . * qi HwêW êdeg qi HwêW êdeg J = 0.5L = 0.5L 15 15J 32 3 2 0.10.1 0.20.2 10 10 * * SP10 SHmhoL HmhoL P10 100100 5050 50 50 20 20 * SP *SHmhoL P HmhoL 200200 100100 0.1 0.1 1.00.1 1.0 10 10 1.0 0.11.0 0.1 10 10 1.0 1.0 1010 5 5 3 3 23 23 M Hkg s-1sL-1 L M Hkg 5000 500010000 10000 (d) . 200200 500500 1000 1000 2000 2000 . . . Fig 8c8c 2 2 * Fig FigFig M8d Hkg s-1sL-1 L 2 2 SP *SHmhoL M8d Hkg P HmhoL ° ° 200 500 1000 2000 5000 10000 -1 -1 200 500 1000 2000 5000 10000 0.10.1 0.2 0.5 1 2 5 10 0.2 0.5 1 2 5 10 Hkg s sL L MHkg * on the system -1 SP *SHmhoL Fig.iP8.max showing the location of plasma corotationMbreakdown, specifically êAêA m-1 iP max êAêA m-1 iPPlots m . . P HmhoL iP max m-1 where (ω/ J ) = 0.5, and its dependence max Fig 8c ∗ ∗ Fig 8c All M Fig 8d parameters 6P and Ṁ. Plot (a) shows the equatorial distance = 100, 1000 and Fig AllatMwhich (ω/J ) = 0.5 versus 6P in log-log format for Ṁ 10 108d ° ° -1 -1 ∗ −1-1, while MHkg s versus MHkg sL L Ṁ for 6 * * for the dipole -1 -1 -1= 0.1, 1 and 10 mho. Solid lines give results 10 000 s (b) shows this distance similarly plotted S HmhoL iP max êA m S HmhoL iPkg êA m P P iP max êA êA mm P iP max max . . field obtained from Eqs. (13) and (14), while the dashedAll lines field M Mshow corresponding results derived from the power law10 All 10 approximate 1010 10 10 solutions for the current sheet model Eqs. (27) and (28). The dots provide spot values obtained from numerical integration of the full 4 10 10 104310solid ∗ (in (b)) values 10103are obvious from their close association with the corresponding dashed lines. current 5sheet solution, whose Ṁ (in (a)) and 6 5 5 5 P 102102 ∗ 10 10 10 10 Corresponding plots of the ionospheric co-latitude at which10(ω/ horizontal dotted 4 4 J ) = 0.5 are shown versus 6P and Ṁ in (c) and (d). The 1.0 101.0 10 10 3 3 line shows the latitude of the field line from infinity in the current sheet field model. 10 10 5 5 5 5 2 2 10 10 1.01.0 1.0 1.0 1 1 1 1 in Sect. 4. ing F0 = Fe (ρe = 70 RJ ) in the approximation, as above. 0.50.5 1.01.0 if we had Very close agreement would have been obtained 1 1 0.10.1 instead taken F = F . These plots also show that for given ∞ 0 the behaviour of the peak Pedersen current, plotted in a 0.50.5 0.50.5 system parameters the peak Pedersen current for 0.10.1 the current similar format to Fig. 8. The magnitude of the peak cur0.10.1 0.1 sheet model exceeds that for the dipole by relatively constant 0.10.1 0.1 rent, plotted versus 6P∗ and Ṁ in Figs. 9a and 9b, respecfactors of ∼3 to ∼5 (typically ∼4). This difference ° ° s-1 L-1 arises * * tively, shows that for the dipole (solid lines) the peakSPPederM0.1 Hkg 0.1 M Hkg s L SHmhoL P HmhoL from the different ionospheric mappings of corotation break200 500 1000 2000 5000 10000 0.20.2 0.50.5 1 1 2 2 5 5 ∗7/8 0.10.10.1 increases 200 500 1000 2000 5000 10000 sen current with the conductivity as 6P1010, while 0.10.1 down, as shown in Figs. 8c and 8d. Figures 9c and 9d ° ° -1 -1 show *Ṁ*1/8 also increasing weakly with the mass outflow rate as M Hkg s sL L M Hkg SFig HmhoL PS P9aHmhoL Fig 9a the co-latitude of the peak Pedersen current, which Fig 9b9b for the Fig 200200 500500 1000 1000 2000 2000 5000 500010000 10000 0.10.1 0.20.2 0.50.5 1 1 2 2 5 5 10 10 0.50.5 1 1 now to the current components, in Fig. 9 we show Turning (Eq. (21a)), while for the current sheet (dashed line) approximations the peak current varies linearly with 6P∗ but is indeFigFig 9a 9a pendent of Ṁ (Eq. (34a)). The modestly lower numericallydetermined spot values in the latter case result from our tak- dipole field lies typically at ∼5◦ and is such that the distance from the magnetic axis varies with the system parameters as FigFig 9b9b ∗−1/8 1/8 6P and Ṁ (Eq. 16), while for the current sheet ap- 3 3 3 3 * SP *SHmhoL P HmhoL 2 2 M Hkg s-1sL-1 L M Hkg . 2 2 . 1000 200 500in 500Jupiter’s 10002000 2000 5000 500010000 10000 0.10.1 and 0.20.2 1 1 Magnetosphere-ionosphere 2 2 5 5 10 10 J. D. Nichols S. W.0.5 H.0.5Cowley: coupling200 currents middle magnetosphere FigFig 8c 8c ° ° -1 -1 MHkg s sL L MHkg iP max êA êA m-1m-1 iP max . . AllAll MM iP max êA êA m iP max m-1 -1 10 10 5 5 FigFig 8d 8d * SP *SHmhoL P HmhoL 10 10 10 10 1043104 10 103 102102 1435 10 10 5 5 1.01.0 1 1 1 1 0.50.5 0.50.5 1.01.0 0.10.1 0.10.1 0.10.1 0.10.1 0.10.1 0.20.2 qi HiPqmaxL êdeg i HiP maxL êdeg 0.50.5 1 1 2 2 5 5 * SP *SHmhoL P HmhoL 200200 10 10 (a) qi HiPqimaxL êdeg HiP maxL êdeg FigFig 9a 9a 500500 1000 1000 2000 2000 ° ° -1 -1 M Hkg s sL L M Hkg 5000 500010000 10000 (b) FigFig 9b 9b 15 15 15 15 10 10 10 10 0.10.1 ° ° -1 -1 MHkg s sL L MHkg 7 7 1.01.0 104104 5 5 10 10 7 7 5 5 * SP *SHmhoL P HmhoL 103103 3 3 3 3 102102 2 2 0.10.1 0.20.2 0.50.5 1 1 2 2 5 5 * 2 2 SP *SHmhoL P HmhoL 10 10 (c) 200200 FigFig 9c 9c ° ° -1 -1 M Hkg s sL L M Hkg 500500 1000 10002000 2000 5000 500010000 10000 (d) FigFig 9d 9d * êmA êmAêmA m Pedersen current intensity in the ionosphere, SP *SHmhoL êmAshowing m Fig.i rmax 9.i rmax Plots the magnitude and location of M the i r max Hkg s-1 sL -1height-integrated P HmhoL and their Mpeak Hkg L i r max ∗ ∗ 100 4 100 100 on 6 and Ṁ. Plot (a) shows the magnitude10 4 peak 100 dependence of the Pedersen current plotted versus 6 in log-log format 10 10 10 for Ṁ = 100, P P −1 , while plot (c) show the ionospheric location of the peak. Plots (b) and (d) similarly show the magnitude and 1000 and 10 000 kg s 50 50 50 50 3 ∗3 106 10P = 0.1, 1 and 10 mho. Solid lines give results for the dipole field obtained location of the peak Pedersen current plotted versus Ṁ for 10 10 from Eq. (21a), while the dashed lines show corresponding derived from the approximate solutions for the power law current sheet 104results 104 2 2 field given by Eq. (34a). The solid dots show spot values 10 obtained from numerical integration using the full current sheet solution. For the 1.01.0 10 case of10the current sheet approximation the peak current depends only10on106P∗ and not on Ṁ, so that only one dashed line is shown in plot 10 (a), valid for all Ṁ. The peak current in this case always occurs as1.0 indicated by the 103103 at the poleward boundary of the current sheet field lines,1.0 5 5dotted lines at ∼14.95◦ in plots (c) and (d). 5 5 horizontal 0.10.1 m-1 -1 . . m-1 -1 0.10.1 102102 proximation it is located consistently at the poleward boundmagnitude of the azimuthal magnetic field outside of the cur1 1 1 1 rent sheet (Fig. 1) (Bϕ (nT) ≈0.63iρ (mA m−1 )). Figures 10a ary of the current sheet field lines at ∼14.95◦ , (dotted line) where0.5 the and b show that for the dipole field the peak current varies 0.5plasma angular velocity falls to zero. The numeri- 0.50.5 ∗1/2 cally computed positions are located at a slightly higher coas 6P and Ṁ 1/2 (Eq. (21c)), while for the current sheet . . latitude, typically by ∼0.1◦ , like the total field-perpendicular * approximation it varies more strongly with Mthe conductivity Hkg s-1sL-1 L SP *SHmhoL M Hkg P HmhoL 200200 500500 1000 ∗1.71/2.71 10002000 2000 5000 500010000 10000 0.50.5In1practical 5 5 10the 0.1 0.20.2 above. 1 2 2 application 10 peak current 0.1 mentioned as 6P , and less strongly with the mass outflow rate 10a 10a current will thus be limited instead by the radial extentFigofFig the 1/2.71 Fignumerical 10b10b Fig as Ṁ (Eq. 34c). The values given by the in. . -1 -1 region to which the model is taken to apply, with the peak M Hkg s L M Hkg s L tegrations are in close agreement with the latter. The current re HirremaxL êRJêRJ r êR r êR e Hir maxL J Hir maxL e Hir maxL J value500 occurring at its outer (poleward) boundary. 104104 500500 500 sheet values are again higher than the dipole values by factors Figure 10 similarly provides results for the peak equatorial radial current, a parameter which relates directly to the 200200 100 103103 104104 3 10 10 3 of ∼3 to ∼5 (typically ∼4), for reasons given above. Fig200200 100 * SP *SHmhoL P HmhoL 3 3 2 2 0.1 0.20.2 0.50.5 1 1 2 2 5 2 20.1 0.20.2 0.50.5 1 W. 5 1436 0.10.1J. D. Nichols and S. 1 H.2 Cowley: 2 i rmax êmA m-1m-1 i rmax êmA 100êmA 100 m-1 -1 i rmax i rmax êmA m 100100 50 50 5050 10 10 1010 5 5 5 5 1 1 1 1 0.50.5 0.50.5 0.10.1 0.20.2 0.50.5 1 1 2 2 5 0.10.1 0.20.2 0.50.5 1 1 2 2 5 re Hir êRJêRJ remaxL Hir maxL 500 500 re Hir êR re maxL Hir maxLJêRJ 500500 3 3 2 2 1010 ° ° -1 * * 2 2 M Hkg s sL-1 L SP S HmhoL M Hkg P HmhoL 200 500 1000 2000 5000 10000 ° ° -1 10 200 500 1000 2000 5000 10000 5 10 * 2 M Hkg s sL-1 L * SPSHmhoL 2 M Hkg P HmhoL 200 500 1000 200 500 1000in2000 2000 5000 500010000 10000 9c 9c Magnetosphere-ionosphere coupling currents Jupiter’s middle magnetosphere 5 1010FigFig FigFig 9d9d . . Fig 9c * * 9d -1 -1 Fig -1 Fig 9c i êmA m S HmhoL 9d PSPFig MHkg s sL-1 L r max i r max êmA m HmhoL MHkg . * -1 100100 . 4 -1 4 10 10 * -1 êmA m S HmhoL P 10 10 -1 i r max MHkg s L SP HmhoL MHkg s L i r max êmA m 4 100 4 1010 1010 100 50 50 3 3 10 10 1010 5050 34 34 10 1010 1010 10421042 1.01.0 10 10 2 2 1010 1010 1.01.0 103103 1.01.0 1010 5 5 3 0.1 3 1010 1.00.1 1.0 5 5 0.10.1 2 2 0.1 10 10 0.1 2 2 0.10.1 1010 1 1 1 1 0.50.5 0.50.5 . . * * M Hkg s-1sL-1 L SP S HmhoL M Hkg P HmhoL . . 200 500 1000 2000 5000 10000 10 200 500 1000 2000 5000 10000 5 10 * MM HkgHkg s-1sL-1 L * SPSHmhoL HmhoL P10a FigFig 200 500 1000 2000 5000 10000 10a 10 Fig 10b 200 500 1000 2000 5000 10000 (a) Fig 10b (b) 5 10 -1 10a MHkg sFig MFig Hkg sL-110a L r êRJêRJ e Hir remaxL . . 4 4 Hir maxL -1 -1 10 10 MHkg s sL L 500500 MHkg re r êR Hire maxL 4 4 Hir maxL JêRJ 1010 500 500 . . 103103 10341034 1010 4 4 1010 103103 1032102 3 1010 2 2 1010 2 2 10 10 200200 200200 100100 100100 50 50 200200 * * SPS HmhoL P HmhoL 200 200 * SPS* HmhoL 10P10HmhoL 100100 100 100 2 2 1010 5050 FigFig 10b 10b 1010 1010 5050 101.0 1.0 10 1.01.0 1.01.0 1.00.1 1.0 0.1 5050 2020 20 20 2020 * SP SHmhoL P HmhoL 2020 * 0.10.1 0.20.2 0.10.1 0.20.2 0.50.5 0.50.5 1 1 1 1 2 2 2 2 5 5 5 5 10 10 * (c) * SPSHmhoL P HmhoL 1010 FigFig 10c10c 200200 500 500 1000 1000 2000 2000 200 200 500 500 1000 1000 2000 2000 0.10.1 0.1 . . 0.1 M0.1 Hkg s-1sL-1 L M Hkg 5000 . . 500010000 10000 (d) MM HkgHkg s-1sL-1 L 5000 10000 5000 10000 FigFig 10d 10d Fig. 10. Plots showing the magnitude and location of the peak sheet-integrated equatorial radial current intensity, and their dependence on FigFig 10c 10c Fig 10d 6P∗ and Ṁ. Plot (a) shows the magnitude of the peak current versus 6P∗ in log-log format for Ṁ = 100, 1000 and 10 000 kgFig s−110d , while plot (c) shows the corresponding equatorial location of the peak in a similar format. Plots (b) and (d) similarly show the magnitude and location of the peak current versus Ṁ for 6P∗ = 0.1, 1 and 10 mho. Solid lines give results for the dipole field obtained from Eq. (21c), while the dashed lines show corresponding results derived from the approximate solutions for the power law current sheet model given by Eq. (34c). The solid dots show spot values obtained from numerical integration of the full current sheet solution. ures 10c and d show that the equatorial distance of the peak is typically located at ∼50 RJ for the dipole model, vary∗1/4 ing with the system parameters as 6P and Ṁ −1/4 , while for the current sheet approximation it is generally located at somewhat larger distances ∼90 RJ , and varies more strongly ∗1/2.71 as 6P and Ṁ −1/2.71 . The positions given by the numerical integrations are again in close agreement with the latter, except for small 6P∗ and large Ṁ, where the position of the peak approaches ρe∗ ≈ 21.78 RJ . In fact for small 6P∗ and large Ṁ, the peak current in the numerical solutions lies consistently at ρe∗ , where the field models are joined. Such points are omitted from the plots. At large distances the ra- dial regime of applicability is again limited, such that the peak radial currents will actually occur at the outer boundary of the region for sufficiently large 6P∗ and/or sufficiently small Ṁ, as can be determined from the position of the peak in Figs. 10c and d. Results for the magnitude and location of the peak azimuth-integrated total equatorial radial current, equal, of course, to twice the peak azimuth-integrated total Pedersen current in each conjugate ionosphere, are shown in Fig. 11. Figures 11a and b show that the magnitude of the peak current for the dipole field increases with the conductivity as ∗3/4 6P , and less strongly with the mass outflow rate as Ṁ 1/4 Ir max Ir êMA max êMA I êMA 10000 . Ir êMA . Ir max max êMA AllAll M M 10000 10000 . Ir max . IrêMA . max êMA . M-1 MAll Hkg s M MAll Hkg sL -1 L10000 10000 4 4 1000 1000 10 . 10 . 3s-13Ls-1 L M MHkg 10Hkg 10 1000 4104 1000 . 10 . 2 -12 10 103Ls-1 L MHkg s10 3Hkg M 10 1000 1000 104 1024 100100 103210 3 10 10 100100 102 102 SP SHmhoL . r max Ir max êMA P HmhoL AllAll M M 10000 J. D. Nichols and S. W. H. Cowley: Magnetosphere-ionosphere coupling currents in Jupiter’s middle magnetosphere . Ir max êMA Ir max êMA Ir max IrêMA max êMA 1000 1000 1000 1000 1000 1000 100100 100100 100100 10 10 100100 10 10 10 10 10 10 10 0.1 100.1 0.20.2 0.50.5 1 1 0.10.1 0.20.2 0.50.5 1 1 re HIr êRJêRJ remaxL HIr maxL 0.1 0.1 0.2 0.2 0.5 0.5 1 1 1000 1000 re HIr êRJêRJ . . 3 remaxL HIr maxL -1 -1 M= kg3 skg M10 = 10 s 1000 1000 re HIrremaxL êR J êRJ . . HIr maxL 500500 3 3 -1 -1 M= kg kg s s M10 = 10 1000 1000 500500 . . 3 kg3 s-1 -1 M =M10= 10 kg s 500500 200200 200200 100100 200200 100100 50 50 100100 50 50 * SP *SHmhoL P HmhoL 10 10 200200 2 2 5 5 10 10 * SP *SHmhoL HmhoL P FigFig 11a11a 200200 2 2 5 5 10 10 * r êR SP * S HmhoL e HIr maxL J J P HmhoL 11a11are HIr maxL êR 200 200 2 2 5 5 10 10 FigFig (a) 1000 1000 r11a êRJ êRJ remaxL e HIr HIr maxL FigFig 11a 1000 1000 104104 re500 êRJ êRJ HIr remaxL HIr maxL 500 4 4 1000 1000 10 10 500500 102102 104 104 500500 200200 102102 103103 2 2 200200 10 10 103103 100100 4 4 10 10 200200 3 10 103 100100 104104 50 50 100100 104 104 50 50 * 0.50.5 1 1 2 2 0.10.1 0.20.2 qHIP qmaxL êdegêdeg HIP maxL 0.1 0.1 0.2 0.2 qHIPqmaxL êdeg êdeg HIP maxL 15 15 qHIP maxL êdegêdeg qHIP maxL 15 15 10 10 15 15 10 10 7 7 10 10 7 7 5 5 7 7 5 5 0.50.5 1 1 2 0.5 0.5 1 1 2 3 3 2 2 3 0.130.1 0.20.2 0.50.5 1 1 2 2 2 0.10.1 0.20.2 0.50.5 1 1 2 2 2 Plots0.1 showing 0.5 0.5 1 1 and 2 0.1 0.2 0.2the magnitude * 5 5 1437 * 10 SP10 HmhoL SP * HmhoL 10 10 1.01.0 10 10 1.0 1.0 10 10 1.01.0 1.0 1.0 10 0.110 0.1 1.0 1.0 0.1 0.10.1 0.1 1.0 1.0 0.1 0.1 0.1 0.1 0.1.0.1. M Hkg s-1sL-1 L M Hkg 500500 1000 10002000 2000 5000 500010000 10000 . . M Hkg s-1 Ls-1 L M Hkg FigFig 11b11b 5005001000 10000 10002000 2000 5000 5000 10000 . . -1 M Hkg s Ls-1 L M Hkg 5005001000 10000 Fig 11b11b Fig 10002000 2000 5000 5000 10000 (b) Fig* HmhoL 11b Fig * 11b S P SP HmhoL SP *1.0 HmhoL SP * HmhoL 1.0 * SP * HmhoL SP1.0 HmhoL 1.0 1.0 1.0 0.10.1 10 10 0.1 0.1 10 10 0.1 1.00.1 1.0 10 10 1.0 0.11.0 0.1 ° ° -1 -1 M Hkg s sL L M Hkg 0.1 1.0 0.1 500500 1000 1.0 10002000 2000 5000 500010000 10000 ° ° -1 -1 M Hkg s Ls L M Hkg 0.1 500500 1000 0.1 10002000 2000 5000 500010000 (d) Fig10000 11d Fig ° 11d ° s-1 L -1 M Hkg M Hkg s L 5005001000 * 11d 10002000 2000 5000 500010000 FigS10000 11d * Fig HmhoL PS P HmhoL * SP SHmhoL P HmhoL50 200200 50 10 10 * SP *SHmhoL P HmhoL 200200 11c 5 5 10 10 FigFig 11c (c) 2 * q HIP maxL êdeg SP * S HmhoL êdeg P HmhoLHIPqmaxL 200200 11c11c 5 5 10° 10 Fig ° Fig 2 MHkg s-1sL -1 L MHkg qHIP qmaxL êdegêdeg HIP maxL ° ° Fig 11c *11d* Fig SPFig HmhoL -1 11c MHkg s-1 LsFig SP 11d HmhoL MHkg L 15 15 qHIP maxL êdegêdeg qHIP maxL ° ° -1 -1 15 * * S HmhoL P 0.1 MHkg s Ls L SP0.1 HmhoL 15 MHkg 10 10 15 15 0.1 0.1 1.01.0 10 10 7 7 0.1 0.1 1.0 1.0 10 10 10 10 104104 7 7 1.0 5 5 4 4 10 1.0 10 10 10310 103 7 7 5 5 43 4 10 10 3 10 10 10210 102 5 3 53 10 10321023 3 3 . . 2 102 10 * 2 2 M Hkg s-1sL-1 L SP *SHmhoL M Hkg P HmhoL 3 10002000 2000 5000 500010000 10000 5 5 10 10 (e) 3 200200 500500 1000 (f) 2 . . -1 2 2 M Hkg s Ls-1 L * SP *SHmhoL M Hkg P HmhoL 200 500 1000 2000 5000 10000 5 10 200 500 1000 2000 5000 10000 11e11e 2 5 10 FigFig Fig 11f . Fig . 11f * 2 2 M Hkg s-1 Ls-1 L SP * S HmhoL M Hkg P HmhoL the10Fig peak azimuth-integrated equatorial ionospheric currents, 200200 500total 5000 10000 11e11e 5 5of 10 500 1000 10002000 2000 and 5000 10000 Fig 11f 2location Fig Fig 11f 50 0.1 500.1 0.20.2 53 53 * 10 *10 SP HmhoL SP * HmhoL Fig. 11. and their dependence on 6P∗ and Ṁ. Plot (a) shows the magnitude of the peak total equatorial radial current (equal to twice the peak total ionospheric Fig 11e11e FigFig 11f11f Pedersen current) versus 6P∗ in log-log format for Ṁ = 100,Fig1000 and 10 000 kg s−1 , while plots (c) and (e) show the corresponding equatorial and ionospheric locations of the peak in a similar format. Plots (b), (d) and (f) similarly show the magnitude and location of the azimuth-integrated peak total current versus Ṁ for 6P∗ = 0.1, 1 and 10 mho. Solid lines give results for the dipole field obtained from Eqs. (21b, d), while the dashed lines show corresponding results derived from the approximate solutions for the power law current sheet model given by Eqs. (34b, d). The peak total current in the latter model is independent of Ṁ, so that only one dashed line is shown in (a). It occurs at infinity in the equatorial plane so that no dashed lines are shown in (c) and (d), or equivalently at the poleward boundary of current sheet field lines in the ionosphere at ∼14.95◦ as shown in (e) and (f) (dotted line). The solid dots show spot values obtained from numerical integration of the full current sheet solution. In this case the peak values occur at large but finite distances such that only the closest of them are included in (c) and (d). 1438 J. D. Nichols and S. W. H. Cowley: Magnetosphere-ionosphere coupling currents in Jupiter’s middle magnetosphere -1 -2 -1 j»»max êBL ê pA m nT H jmax ê-2 pA m nT-1 j»»HêBL ê pA nT H jH»»êBL ê»»êBL pA mm-2 max max -2nT-2 H j»»êBL ê pA m nT-1nT-1 H 100 jmax êBL ê pA m »»100 max 100 100 -2 -2 -2-2 j»»i jmax êmA m j»»i êmA êmA mm-2-2 max êmA »»ij»»i max max -2 -2 -1 -2 -1 -2 m -1 êmax pA nT jêBL êpA pA m-2 j»»i maxj»»iêmA êmA m H j»»êBL H jH»»Hmax êm m »»jêBL max maxm ê pA mnT nT-1 -2 »»êêBL max H j»»êBL pA m nT H jmax êBL ê pA m-2-1nT-1 »»100 max 100 100 100 100 100 * * * = SP =S mho SPP10 10 mho mho * S= *10 10 mho P10=mho SP * =SP10 =mho 10 10 10 10 10 1010 10 10 10 10 10 1.0 1.0 1.0 1.0 1.0 1.0 -1 100 100 M . Hkg . s-1 M HkgL s L M Hkg -1 L -1 LL s L HkgMs2ss-1 Hkg 10 10MMHkg 102 102 10 10 1010 10 223 102 10 10 103 103 3 10 33 10 10 104 10 104 10444 104 .. 1 1 1 11 1 . . -1 -1 10 1 . . 0.01 0.01 0.01 0.1 0.010.10.2 0.2 0.01 0.1 0.10.2 0.2 0.5 0.5 SP * HmhoL 1SP * HmhoL 1 2 2 0.2 0.5 SP * HmhoL 1* 2 0.01 0.1 * SP HmhoL 0.1 0.2 0.5 SP HmhoL 1 2 0.5 0.5 1 re H H j»»êBL re H HmaxL J êRJ j»»êBLêR maxL re1000 re1000 H H j»»êBL J êRJ H HmaxL j»»êBLêR maxL 1 2 2 SP * HmhoL re H1000 H j»»êBL1000 maxL êRJ re H 1000 H j»»êBL maxL êRJ 500 500 1000500 500 500 500200 200 200 200 200 100 100 200100 100 10050 50 50 50 50 20 20 50 20 20 20 0.1 0.1 0.2 0.2 0.1 0.1 0.2 0.2 q20 i H j»»i maxL êdeg qi H j»»i maxL êdeg qi H j»»iqmaxL 0.1 0.2 i H j»»iêdeg maxL êdeg qi H j»»i0.1 maxL êdeg 0.2 15 15 15 15 qi H j»»i maxL êdeg 0.5 0.5 1 0.5 0.5 1 1 2 1 2 2 2 0.5 1 2 0.5 1 2 75 1.0 1.0 1.0 0.1 0.1 0.1 0.1 0.1 10 10 1 1 1 1 0.1 0.1 0.1 0.10.1 0.1 1.0 0.1 0.01 0.01 0.01 0.01 0.01 0.1 (a) (b) (c) (d) 10 qi H j »» i maxL êdeg °103 -1 MHkg s L 10 15 10 102 4 10 10 10 43 104 10 10 15 104 1042 10 7 7 15 10 5 0.1 0.1 0.1 1 1 0.01 0.01 0.01 2000200050005000 10000 ° 1000 1000 10000 0.01200 200 500 500 ° -1 L s-12000 HkgM L 50005000 Hkg 0.0110 200 200 500 M 2000 10000 0.01 500 1000 10000 ° 1000 ° s-1 5 10 0.01 200 M500 5000 10000 ° 1000 L s-1-1 HkgMsHkg L 2000 5 10 10 L M Hkg s Fig 12b Fig 12b 5 Fig 12a 10 0.01 200 500 ° 1000-1 2000 5000 10000 Fig 12a Fig 12b M Hkg s L Fig 12b Fig10 12a r 5Fig. 12a Fig 12b . -1 re HHmaxL e HH j»»êBL J êRJ j»»êBLêR maxL Fig .12a M sHkgL s-1rLe1000 . HkgM re1000 J êRJ HHmaxL j»»êBLêR maxL -1 -1 HH j»»êBL Fig 12b MHkg sHkgL s L 1000 .M re1000 Fig HH j»»êBL maxL êRJ 2 12a 2 10Hkg 10s-1 M L 1000 10.2 102 -1 re HH j»»êBL maxL êRJ 2 s L 500 500 M10 Hkg 1000 500 500 103 10 10332 500 3 10 10 SP * HmhoL SP * HmhoL 200 200 500 103 102 102 SP * HmhoL SP * HmhoL 200 200 1024 10 10 10243 10 10 4 104 S * HmhoL 200 10 10 2 10 10 P 100 100 3 1031010 4 * 100 100 103101032 10 SP HmhoL 200 1.0 1.0 10 3 44 1041010 50100 1.0 10 10 1.0 50 10 4 4 10 10 10 50 50 10 10 100 1.0 1.01.0 4 3 1010 50 1.0 0.1 1.0 0.1 10 20 20 0.1 0.1 1.0 20 2050 0.1 0.11.0 10 104 0.1° 0.1 0.1 ° -1 * -1 * M° HkgM SP HmhoL HkgL s L SP HmhoL 20 ° s-1 * 200 200 500 50010001000 20002000 50005000 10000 5 5 10SP10 M HkgMs0.1 10000 HkgL s-11.0 L HmhoL SP * HmhoL 200 200 500 50010001000 20002000 50005000 10000 10000 5 5 10 10 0.1 ° Fig 12c 20 Fig 12d * M Hkg s-1 L êdeg Fig S12c êdeg P HmhoL Fig 12cqi H j »» qi maxL i H j »» i maxL Fig 12d Fig10000 12d 0.1 500 1000 2000 5000 5 ° 10 ° -1 -1qi H j »» qi maxL i H j »» êdeg i maxL êdeg 200 SP * HmhoL SP * HmhoL M HkgL s L ° HkgM * °4s-1 ° * -1 S HmhoL S HmhoL * P0.1 P0.1 4s HmhoL MHkg sHkg L 10MFig M Hkg s-1 L SLP12c 10 Fig 1.0 43 4 1.0 12d qi H j »» i maxL êdeg 200 0.1 0.1 500 1000 2000 5000 10000 10 1010 10 5 103 10 10 15 15 1.0 32 1.0 3 °10 * 0.1 10 2 0.1 10 10 10Hkg SP HmhoL 10s-1 M L 15 15 Fig 2 12c 0.1 0.1 Fig 12d 102 10 4 10 10 10 10 7 0.01 0.01 0.010.01 0.01 0.1 0.1 1.0 1.0 10 10 10 10 10 5 5 15 10 7 1 0.1 0.1 0.1 1 1 0.1 0.1 0.1 0.1 0.1 All M .All . . M AllAll M All . MM 0.1 0.1 All M 0.10.1 0.1 0.1 0.1 0.1 0.1 0.1 100 1 1 1 1 1 11 10 10 10 10 10 -2 -2 -2 j»»i maxjêmA m êmA m-2 »»i jmax mêmA m-2 »»i max -2jêmA »»immax j»»i maxj»»i êmA êmA maxm 7 7 7 103 103 43 1031010 5 5 0.1 1.0 1.01.0 * 10 1.0 1.0 0.1 SP HmhoL 10 10 10 10 10 1.0 0.1 1.0 10 0.1 10 1.0 7 5 510 5 75 2 10 102 102 3 2 1010 104 0.1 0.1 0.2 0.2 0.1 0.1 0.2 0.2 DqH+ Dq j»»iL êdeg H+ j»»iL êdeg 10 10 5 0.1 5 5 0.2 0.1 2 2 0.2 1 10 5 7 M s-1 L -1 SP * HmhoL . HkgM . Hkg s L S * HmhoL -1 200 200 500 50010001000 20002000 50005000 10000 * 2 P* 5 5 10SP10 M HkgMsHkg L s-1 L 10000 HmhoL 10 SP3HmhoL 200 200 500 50010001000 20002000 50005000 10000 10000 5 5 10 10 10 DqH+ jDq êdeg »» iLH+ j »» iL êdeg Fig 12e * 12f * 12f Fig 12e 10 10 5 SFig SFig P HmhoL P HmhoL Fig 12e Fig 12f Fig 12e Fig 12f . -1 *2 S10 0.1 0.1 M Hkg s L P HmhoL 200 500 1000 2000 5000 10000 5 M° Hkg 10° s-1 L -1 MHkg s L 5 5 1.0 1.0 104 104 10 10 Fig 12e Fig 12f . 0.1 0.1 103 10 M Hkg s-1 L S3 * HmhoL . 75 0.5 0.5 1 0.5 0.5 1 1 2 1 2 2 2 0.5 1 2 0.5 1 2 (e) 5 (f) P 2 1010 102 Fig 12e 1 104 104 0.5 0.5 103 103 2 10 10 2 2 1 1 200 500 1000 2000 5000 10000 1.0 1.0 10 10 Fig 12f 0.5 0.5 2 0.2 0.2 0.2 0.2 0.1 0.1 0.1 0.1 0.2 0.2 . 0.5 0.5 1 1 2 2 5 0.1 0.1 SP * HmhoL SP * HmhoL 5 10 10 (g) Fig 12g Fig 12g M HkgMs-1 HkgL s-1 L 200 200 500 50010001000 20002000 50005000 10000 10000 . . (h) Fig 12h Fig 12h Fig. 12. Plots showing the magnitude, location and half-width of the peak upward-directed field-aligned current density, and their dependence on 6P∗ and Ṁ. Plot (a) shows the magnitude of the peak total current density versus 6P∗ in log-log format for Ṁ = 100, 1000 and 10 000 kg s−1 , where the left-hand scale shows the peak current density in the ionosphere, while the right-hand scale shows the peak (jk /B) value, simply related to the latter via Eq. (5b). Solid lines give results for the dipole field obtained from Eqs. (21e ,f), while the dashed lines show corresponding results derived from the approximate solutions for the power law current sheet model given by Eqs. (34e, f). The solid dots show spot values obtained from numerical integration of the full current sheet solution. Plot (c) shows the corresponding location of the peak (jk /B) in the equatorial plane in a similar format, while plot (e) shows the conjugate location of the peak field-aligned current in the ionosphere. Plots (b), (d), and (f) similarly show the magnitude and equatorial and ionospheric locations of the peak current density versus Ṁ for 6P∗ = 0.1, 1 and 10 mho. Plots (g) and (h) show the latitudinal width of the upward field-aligned current region in the ionosphere in a similar format, defined as the full width at half maximum. J. D. Nichols and S. W. H. Cowley: Magnetosphere-ionosphere coupling currents in Jupiter’s middle magnetosphere (Eqs. 21b, d), while for the current sheet approximation it is linearly proportional to 6P∗ and independent of Ṁ (Eqs. 34b, d). The numerical values shown by the dots in the latter case are a little lower than the dashed line approximation for reasons given above for the Pedersen current. The value of the peak current is a factor of ∼5 to ∼20 (typically ∼10) larger for the current sheet than for the dipole. The location of the peak in the equatorial plane (where the field-aligned current passes through zero), is shown in Figs. 11c and d. It is located ∗1/4 typically at ∼90 RJ for the dipole field, scaling as 6P and Ṁ −1/4 , but occurs at infinity for the current sheet approximation (such that no dashed lines are shown in Figs. 11c and d), or, in other words, at the outer boundary of the relevant region in practical application. The peak value in the numerical curves, shown by the dots, occurs at large but finite radial distance, as mentioned above, typically well beyond the region of physical applicability (∼500 to ∼5000 RJ ). Only the closest of them (for small 6P∗ and large Ṁ) are included in Figs. 11c and d. The corresponding location of the peak azimuth-integrated Pedersen current in the conjugate ionosphere is shown in Figs. 11e and f. It is located typically ∗−1/8 at ∼6◦ for the dipole field, scaling as 6P and Ṁ 1/8 as before, but for the current sheet it is located consistently at (for the approximation) or near (for the numerical values) the poleward boundary of the current sheet field lines at ∼14.95◦ (dotted line). Figure 12 shows results for the upward-directed fieldaligned current density, a parameter of relevance to the origins of the jovian auroras. The magnitude of the peak upward current is shown in Figs. 12a and 12b in a similar format to the above, where, since jki and (jk /B) are simply related through the constant factor 2 BJ in the approximation for the ionospheric magnetic field employed here (Eq. 5b), one plot serves the purpose of both parameters according to the leftand right-hand scales. These plots show that for the dipole field the peak upward current density depends linearly on 6P∗ and is independent of Ṁ (Eqs. 21e, f), while for the current sheet approximation it increases somewhat more rapidly with ∗3.42/2.71 the conductivity as 6P (i.e. as ∼ 6P∗1.26 ), while decreasing slowly with the mass outflow rate as Ṁ −0.71/2.71 (Eqs. 34e, f). The latter values agree well with those obtained from numerical integration, and exceed those obtained for the dipole field by factors of ∼10 to ∼50 (typically by ∼25). The position of the peak value of (jk /B) in the equatorial plane is shown in Figs. 12c and d. It lies typically at ∗1/4 distances of ∼50 RJ for the dipole field and varies as 6P −1/4 and Ṁ , while lying at larger typical distances beyond ∗1/2.71 ∼100 RJ for the current sheet model and varies as 6P and Ṁ −1/2.71 . The position of the peak field-aligned current density in the ionosphere is shown in Figs. 12e and f. For the dipole it lies typically at a co-latitude of ∼8◦ and scales in ∗−1/8 distance from the magnetic axis as 6P and Ṁ 1/8 , while for the current sheet model it lies just equatorward of the boundary of current sheet field lines, with variations which are in the same sense as for the dipole, but with amplitudes 1439 which are much smaller. In Figs. 12g and h we finally show a measure of the latitudinal width of the region of upward fieldaligned current, potentially related to the latitudinal width of associated jovian auroras, plotted versus 6P∗ and Ṁ, respectively. The width of the upward current given here is the full width at half maximum. The solid and dashed lines show results for the dipole and power law current sheet approximation, respectively. The results were derived from the fact that in the equatorial plane the value of (jk /B) reaches half its peak positive value for the dipole field at normalised radial distances (ρe /RDe ) of ∼0.629 and ∼1.470 (see Fig. 3e), while for the power law current sheet approximation the corresponding values of (ρe /RCSe ) are ∼0.940 and ∼8.337 (see Fig. 7e). The dots again show spot values obtained numerically using the full current sheet field. It can be seen that the width for the dipole field is typically ∼3◦ –5◦ , decreasing modestly with increasing 6P∗ and increasing modestly with ∗−1/8 increasing Ṁ (as 6P and Ṁ 1/8 , respectively). For the current sheet model the thickness is reduced to ∼0.5◦ –1.5◦ (less if the system is limited in radial distance), varying in the above manner more strongly with the system parameters (as ∼ 6P∗−0.26 and ∼ Ṁ 0.26 ). 6 Summary In this paper we have considered the steady-state properties of the magnetosphere-ionosphere coupling current system that flows in Jupiter’s middle magnetosphere, associated with the enforcement of partial corotation on outwardflowing plasma from the Io torus. The solutions depend on the values of two parameters, the effective Pedersen conductivity of the jovian ionosphere 6P∗ , and the mass outflow rate of iogenic plasma Ṁ, these being taken to be constants. However, their values remain uncertain at present, thus prompting the study presented here of how the solutions depend on these parameters over wide ranges of the latter. We have also focussed on two models of the magnetospheric poloidal field, taken for simplicity to be axisymmetric. The first is the planetary dipole alone, which constitutes an instructive paradigm. Some general results for this case have previously been given by Hill (1979, 2001). Here we have provided a complete analytic solution for this case, showing how the plasma angular velocity and current components scale in space and in amplitude with 6P∗ and Ṁ. We find that the plasma angular velocity and current components scale in equatorial radial distance as (6P∗ /Ṁ)1/4 , as found previously by Hill (and correspondingly as (6P∗ /Ṁ)1/8 ) in the ionosphere), while each current component scales in ampli∗(1+γ )/2 (1−γ )/2 tude as (6P Ṁ , where γ has a particular value for each component. The scales in space and amplitude then combine to produce current values which depend only on Ṁ at a fixed position at small radial distances, and only on 6P∗ at a fixed position at large radial distances, these dependencies then requiring current variations at small and large distances 1440 J. D. Nichols and S. W. H. Cowley: Magnetosphere-ionosphere coupling currents in Jupiter’s middle magnetosphere 2(1+γ ) with particular powers of the distance, as ρe at small −2(1−γ ) distances, and as ρe at large distances. These results provide useful background for the second, more realistic field model, based on Voyager data, in which the equatorial field strength is significantly less than for the dipole field due to the radial distension of the middle magnetosphere field lines, and is taken to vary with distance as a power law ρe−m . Solutions for a few spot values of 6P∗ and Ṁ have previously been presented by Cowley et al. (2002, 2003), obtained by numerical integration of the corresponding Hill-Pontius equation. Here we have derived an analytic approximation, applicable to the power law regime, which shows how the plasma angular velocity and current components scale with 6P∗ and Ṁ in this case. We find that these solutions provide accurate approximations to the full numerical results within the power law regime (roughly ρe > 20 RJ ) over very wide ranges of the system parameters, provided (6P∗ /Ṁ) is not too small (∼10−4 mho s kg−1 or larger). The results show that the conclusions concerning the nature of the current sheet solutions, and their relation to the dipole solutions, which were drawn previously on the basis of a limited number of numerical investigations are generally valid over wide ranges of the parameters. In particular, it has been shown that in the current sheet model the field-aligned current flows unidirectionally outward from the ionosphere into the current sheet over the whole current sheet, in all cases of interest. The closure of this current must then occur on field lines at higher latitudes which map to the outer magnetosphere and tail, which are not described by the present theory. This situation contrasts with the dipole model, in which (at least in principle) all the flux in the system is described by the theory, such that complete current closure occurs between the equator and the pole. The results for the power law current sheet show that the plasma angular veloc1/m ity and currents now scale in radial distance as (6P∗ /Ṁ) , while each current component again scales in amplitude as ∗(1+γ )/2 (1−γ )/2 Ṁ , where the values of γ for each compo6P nent exceed those of the corresponding component for the dipole field (at least for m > 2 as considered here). The current components thus scale as a somewhat higher power of 6P∗ for the current sheet than for the dipole, and as a somewhat lower power of Ṁ. These scales in space and amplitude again combine to produce current values which depend only on Ṁ at a fixed position at small radial distances, and only on at a fixed position at large radial distances (both being general properties of the solutions), these dependencies then m(1+γ )/2 requiring current variations as ρe at small distances, −m(1−γ )/2 and as ρe at large distances. The absolute values of the currents are also higher for the current sheet model than for the dipole, by a factor of ∼4 for the Pedersen and equatorial currents, ∼10 for the total current flowing in the circuit, and ∼25 for the field-aligned current densities. These factors do not vary greatly over the range of system parameters considered here. Acknowledgements. JDN was supported during the course of this study by a PPARC Quota Studentship, and SWHC by PPARC Senior Fellowship PPA/N/S/2000/00197. Topical Editor T. Pulkkinen thanks V. M. Vasyliunas and another referee for their help in evaluating this paper. 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