Planet. Space Sci., Vol. 44, No. 11, pp. 1251-1268, 1996 Pergamon Cotwright 0 1996 Elsevier Science Ltd Printed-in GreatBritain. All rights reserved 0032-0633/96 $15.00+0.00 PII: SOO32-0633(96)OOOSf%i Theoretical seismic models of Mars of the mantle : the importance of the iron content A. Mocquet, P. Vacher, 0. Grasset and C. Sotin Laboratoire 03, France Received de Gtophysique 13 October et Planetologie, U.F.R. des Sciences et Techniques, 1995; revised 4 June 1996; accepted 44072 Nantes CCdex 7 June 1996 Abstract. Present-day averaged temperature proGles of the mantle of Mars are computed &&x4gh~numorical convection experiments performed with : L+ symmetricalgeometiy, for different vaIues of core r&hi and d&rent boundary conditions at the core-mantle boundary. Internal heating of the mantle js considered in each case. It is found that Zhe temljerature p~diles of the man& are very stable whatever the imposed conditioas at the core-tiantle boundary.’ A 300km thick thermal lithosphere, displaying a temperature gradients equal to 4.4ISkrW’ is followed ‘at greater depths by a quasi-iscvthemd mantle, the temperature of which is faukid in a 12@O-f600K temperature range. A mean tempbature equal to 1400 K is in a goad agreement with the low Q ofMars at ti&l frequencies. These characteristics, together with the small increase of pressure with depth, of the order of 0.01 OPakm-*, induce tfiepresence OFa 1ow:velocity zone similar to the Earth’s one, dawn to 300 km depth. Densities and seismic velocit&i corresponding to these thermoi$yaamical conditions are computed using Clirtineisen’s and fhirdorder finite strain theory for diff&erit values of the iron content of mantle r&e-ra%. B.&W SQpkm depth, the values of d&&ties and se&r& vehxities have ‘&hesame order of magnitude a3 within iLEe Earth’s t&&ion zone.’ An increase of the iron conrent of the Martian mantie with respect to the Earth’s one results (1) in an imrease of density, and a Gecrease of seismic velo&ies, which em reacti more t&an, 2 B/sof ttie values expected from an Earth like composition, (2) in a homogeniz$ion of mantle structure thrmgb the smmtbing out of seitie discontinuities over a thickxqss of .a few hundred kilo;nretses. This smuothing pmss is due to the large pressure domams of coexistence between different phases of &vine @hen the iron comeat of this latter mineral increases. Plausible domains of core Correspondence to: A. Mocquet 2 rue de la Houssinibre, 1. Introduction The present-day averaged structure of a planet is intrinsically related to its accretion history, to its core formation, and to its subsequent thermal and tectonic evolutions. In the absence of preliminary seismic data, tentative bulk compositions of the mantle and core can be inferred from the mean density, and from the principal moment of inertia of the planet using geochemical arguments. A choice among different plausible models can then be achieved by constructing theoretical density and seismic velocity profiles, using available mineral physics data (e.g. Anderson et al., 1977; Okal and Anderson, 1978; Lognonne and Mosser, 1993) and by comparing these latter with seismological models of internal structure derived from observation, in the same way as this is presently done for the Earth’s mantle (e.g. Dully and Anderson, 1989; Vacher et al., 1996). In the Earth’s case, this type of procedure has successfully shown, for instance, that seismic velocity gradients agree with a nearly adiabatic behaviour of the upper mantle in the depth range 100-400 km, the temperature at the foot of the adiabat being close to 1200°C (e.g. Vacher et al., 1996), but that the transition zone looks highly subadiabatic (e.g. Anderson and Bass, 1986; Duffy and Anderson, 1989). The 1252 comparison between geochemical, seismological, and mineral physics data enriched the debate concerning the bulk composition of the Earth’s mantle (e.g. Bass and Anderson, 1984; Weidner, 1985), leading to a compositional model (Ito and Takahashi, 1987) which adequately fits spherically symmetric reference Earth’s models derived from seismology (Weidner and Ito, 1987 ; Vacher et al., 1996). Similarly, the results of tomographic studies indicating that the magnitude of relative shear velocity variations are at least twice as large as the magnitude of relative compressional velocity variations led Duffy and Ahrens (1992) to conclude that small amounts of water-rich partial melt could exist in the Earth’s lower mantle. In the case of planet Mars, such tomographic studies are far beyond the scope of future planetary missions. Nevertheless, it may be hoped that American, European, Japanese, and Russian projects which are presently impulsed will provide, within a few years, important seismological data from which preliminary one-dimensional seismic models will be constructed and, henceforth, important conclusions regarding the composition of the Martian mantle and state of the core will be accessible. In particular, a mantle composition close to the one derived from the study of SNC (Shergottites, Nakhlites, Chassigny) meteorites is characterized by an enrichment in iron relative to the Earth’s composition (Ringwood, 1979 ; Dreibus and Wanke, 1985; McSween, 1985). If correct, such enrichments should greatly influence the density of the mantle, its seismic structure, together with the values of the mean principal moment of inertia I (Ohtani and Kamaya, 1992). In fact, one of the major difficulties encountered in a study of Mars is the poor knowledge of the mean principal moment of inertia. The actual value of the ratio I/MR’, where M is the total mass of the planet, and R its mean radius, is still under debate (e.g. Reasenberg, 1977 ; Bills, 1989 ; Kaula et al., 1989 ; Kaula and Asimow, 1991). Johnston et al. (1974) performed one of the first calculations of the thermal history of the planet, and of its core formation. They computed a rather high I/MR2 value (0.377) which implied in turn high values of mantle densities, of the order of 3.72 g cme3. Nevertheless, more recent studies tend towards I/MR2 values ranging from 0.345 to 0.365. It is still not possible to choose either the lower or the upper bound of this range. For instance, Bills (1990) emphasized that a small increase of the ratio I/MR2 could lead to a large domain of possible compositions for the whole planet. Bills and Rubincam (1995) even showed that, under the assumption of a two-layer piecewise constant density model, it was not necessary to invoke geochemically implausible density extrema in order to reach any IIMR’ value in the range 0.325-0.365. In particular, the mean densities of the mantle and core are istrongly influenced by the respective amounts of iron effectively present in both layers. Anderson (1972) suggested, on the basis of chemical criteria, that the amount of iron oxide in the Martian mantle is higher than the Earth’s one. Similarly, Lewis (1972) estimated that the weight ratio FeO/(FeO + MgO) of the Martian mantle is close to 0.5. A useful constraint on the internal structure of Mars is provided by the significant acceleration in the longitude of Phobos (Sharpless, 1945) due to solid-body tides raised by Phobos in Mars (e.g. Burns, 1977 ; Pollack, 1977 ; Lam- A. Mocquet et al.: Theoretical seismic models of Mars beck, 1979). The value of this acceleration is now known with a good accuracy (Table 1). The successive improvements in its determination have been reviewed by Burns (1986,1992). To the first order in the angular displacement, in radians, between Phobos’ longitude and the maximum of the induced tide on Mars, the dissipation function Q’, and the Love number k2 of the planet are related to the orbital parameters listed in Table 1 through (e.g. Lambeck, 1979 ; Burns, 1986) (1) where a is the semimajor orbital axis of Phobos around Mars, m its mass, y1 its angular velocity, ti its secular acceleration, and F the universal gravitational constant. The values listed in Table 1 lead to k,Q-‘-(1.834+0.061) x 1O-3 (2) where the uncertainty is in 20. Any model of Mars’ inner structure must fulfil equation (2). The Love number k, is provided by the distributions at depth of the density and elastic moduli. Previous estimates of 1~ range from 0.08 (Ward et al., 1979) to 0.15 (Lognonne and Mosser, 1993). According to equation (2), this range of values correspond to 42~ Q<85. Smith and Born (1976) and Ward et al. (1979) proposed 50 < Q < 150. However, a more recent determination of ri by Chapron-Touze (1990) argue in favour of the lowest end of this range, because, according to equation (2), Q values as high as 150 would require k2 values higher than 0.26. Possible explanations for this low Q value have been reviewed by Lognonne and Mosser (1993). According to the seismic absorption band model of Anderson and Given (1982), the frequency dependence of Q is governed, at tidal frequencies, by the value of the long period relaxation time z2. This latter parameter depends on pressure P and temperature T through z2 = z. exp where z0 is a pre-exponential constant, E* and V* the activation energy and volume, respectively, and R* the gas constant. In equation (3), the activation energy and volume are set equal to 60 kcalmol-’ and 10e5 m3 mol-‘, respectively (Anderson and Minster, 1981). At constant pressure, equation (3) implies that a temperature decrease of 200 K translates into a two decade shift of the absorption band towards long periods, and, consequently, to a decrease of Q. Thus, the low Martian Q values might be the signature of a cold Martian mantle, as compared to the Earth’s upper mantle (Anderson and Given, 1982 ; Lognonne and Mosser, 1993). Alternative explanations invoke the presence of volatiles and/or partial melting within the mantle of Mars (Toksiiz et al., 1978 ; Lambeck, 1979 ; Lognonne and Mosser, 1993). Since available data on the internal structure of Mars are sparse, it would be hopeless to pretend describing in an overdetailed way the actual fine structure of the planet. On the other hand, our goal is to derive a plausible range of mineralogy and composition of the Martian mantle, putting emphasis on the associated range of seismic struc- A. Mocquet et al.: Theoretical seismic models of Mars 1253 Table 1. Parameters used in the study of the secular acceleration in the longitude of Phobos (equation (1)) Parameter Mars mass M (x 1O23kg) mean radius R Phobos semimajor axis a angular velocity n secular acceleration A mass m Uncertainties Value Reference 6.4179 +0.0031 3389.916* 0.038 km Born (1974) Bills and Ferrari (1978) 9378.5 km 2.28 x 10m4rad s-’ (4.45kO.03) x 10-20rads-2 (10.81-0.1) x 10r5kg Chapron-TouzC (1990) Lambeck (1979) Chapron-TouzC (1990) Avanesov et al. (1989) are in lo. tures eventually detected by future missions on Mars. In a first part, three different temperature profiles of the mantle are constructed, corresponding to different radii of the core-mantle boundary, boundary conditions at the base of the mantle, and liquid or solid state of the core. These input parameters are taken from Sotin et al. (1996). In order to take into account the small radius of the planet, the mean temperature profiles of the mantle are derived from two-dimensional convection experiments performed with axisymmetrical geometry. Griineisen’s and third-order finite strain theories are subsequently used to compute the mean densities and seismic velocities as a function of depth, following the methods of Duffy and Anderson (1989) and Vacher et al. (1996). At this stage, the experimental work on the phase transition of olivine (Katsura and Ito, 1989) is used to assess crude mineralogical models of the Martian mantle as a function of the amount of iron. The reliability of the temperature profiles and seismic models of the upper mantle is subsequently checked back by computing their associated moment of inertia ratio, Love numbers and Q values (equations (2) and (3)). 2. Convection experiments Previous studies (e.g. Stevenson et al., 1983; Schubert and Spohn, 1990) considered parameterized convection to describe the heat transfer throughout the Martian mantle. In a preliminary study (Mocquet et al., 1994), we conducted the whole procedure described here using Cartesian coordinates, and a parameterized convection formalism, in order to get a range of plausible starting values for subsequent time-dependent numerical calculations in a two-dimensional spherical geometry, and for a study of the Martian core thermal history (Sotin et al., 1996). The present study only describes the final stage of the computations. It is entirely devoted to the mantle, and references to the Martian core are only made when they are necessary for the discussion of the mantle structure. The time-dependent numerical calculations are performed in a similar way to that employed by Zhou et al. (1995), except that internal heating is taken into account in our study, and that we do not include the influence of the phase transitions of olivine on the convection geometry. Sections 2.1 and 2.2 will describe the numerical procedure, and its application, respectively. 2.1. Numerical aspects The general form of the equations describing convection can be written as (e.g. Busse, 1989) g+v.(p”)=o thermal (4) P[~+(uTu]= -vp+pg+v.z (5) ,cF(~+“.vT)-aT(~+“.vP) = pFzps I-Lx(T-TT,)-f [ v (kvT)+pH+p@ (6) $(P-Ps). (7) ’ T 1 In equations (4)-(7), p is the density, t the time, II the fluid velocity, P the pressure, g the gravity, z the stress tensor, C, the heat capacity, T the temperature, CI the thermal expansion coefficient, k the thermal conductivity, H the rate of heating by radioactive disintegration, CDthe dissipation function which gives the amount of heat released by viscous forces, and KT the bulk modulus at constant temperature. Subscripts S refer to adiabatic values. A present-day value of H = 6.2 x lo-l2 W kg-’ is assumed. Equations (4)-(6) express the conserva.tion of mass, momentum, and energy in their most general form, respectively. Equation (7) is the equation of state. A number of simplifications are done. First, the Boussinesq approximation is used. It means that a constant density is assumed, except in the gravity term of equation (5), and that the pressure dependence of the density is negligible compared to the temperature dependence. Second, the thermal conductivity is constant, and following Stevenson et al. (1983), and Schubert and Spohn (1990) the viscosity only depends on the mean temperature of the mantle. It implies that a calculated dissipation function would not be realistic. It is therefore neglected in the present study. The effect of pressure is also neglected in the equation describing the conservation of energy. It means that models are valid at surface pressure conditions. This peculiarity will be used later on for the computation of seismic wave velocities. Finally, the Prandtl number is very large (> 10”) and the left-hand side of equation (5) is negligible. A. Mocquet et al.: Theoretical seismic models of Mars 1254 stream function of the following As long as a liquid outer core is present, the temperature at the core-mantle boundary (CMB) is equal to the temperature of the liquidus at the inner core boundary (ICB) since the adiabatic gradient in the core is negligible in Mars’ condition. Once the core is solid, the temperature at the CMB may vary with latitude. The temperature of the upper surface is equal to 220K. Thermal convection is calculated by time-stepping the conservation equation for thermal energy (equation (6)) recasted in non-dimensional variables on a unit sphere. Equation (6) becomes . VT’ = V2T’+ a2Y!’ I a2yl ar”+r”ae?_---= The scales for temperature, T- To H" (10) U (12) lc respectively, where K is the thermal diffusivity of the mantle. The energy equation (8) is approximated with central differences for the conduction terms, and upwind differencing of the advection terms. The velocity at each grid point of the mantle is calculated at each time step by solving the continuity and momentum equations describing thermal convection of an infinite Prandtl number, isoviscous fluid : v*u=o (13) -vP+pV2U+f = 0 (14) where ~1is the fluid viscosity, and f the buoyancy force. Under the assumptions stated previously, equations (13) and (14) correspond to equations (4) and (5), respectively. The three unknowns are the pressure, and the radial and colatitudinal components of the velocity, u, and us, respectively. Following Zebib et al. (1980) and Machete1 (1986) equation (14) is more easily solved in two-dimensional spherical geometry by defining the non-dimensional Table 2. Constant values used in the calculations Thermal conductivity, k (W m-’ K-l) 4 Thermal expansivity, CI(K-l) 2 x 10-5 (15) (16) (17) where q = p/p is the kinematic viscosity. The temperature dependence of the viscosity is similar to equation (3). It is given by are AT R - Y, wWa - rJ3 Krl ” = (R:;c)2 u’ - = ~==kexp time, and velocity T'= Ra (9) ’ k , --w where r ’ is the non-dimensional radial distance, and 0 the colatitude. The Rayleigh number Ra on the right-hand side of equation (16) is equal to p@;;)2f$ ~ff(R--r,)~ = c0teayf r‘2 a8 dT’ = Ra . sin8 . x where T’, t’, and u’ are non-dimensional temperature, time, and velocity, respectively, and Y, the core radius. When a liquid core is present, AT is the temperature difference between the temperature at the CMB and the temperature at the surface To. For a solid core, we replace the temperature difference by AT !I” and vorticity w ’ which are solutions set of equations : ( 1 ~~ (18) where H* is the activation enthalpy (H* = E* + PV*), T the mean temperature of the mantle, and ,V = 1021Pas for i’ = 1350°C. This latter value is chosen to be consistent with the value of the Earth’s upper mantle viscosity. At the pressure conditions of the Martian mantle, the values of activation energy and volume used in equation (3) yield H*-300kJmol-‘. Equations (15) and (16) are solved using finite difference approximations. A multigrid algorithm is used. It is derived from the one described by Stuben and Trottenberg (1982). This solver is based on alternate zebra relaxation (smoothing operator), transfer from fine to coarse grids (restriction operator) by half injection, and transfer from coarse to fine grids (extrapolation operator) by linear interpolation. The upper boundary is a rigid surface. The lower boundary is a free-slip surface in the case of a liquid core, and a rigid surface in the case of a solid core. The solution of equations (8), (15), and (16) is time-dependent because there is no steady-state pattern of convection. The calculations are carried out for a large number of time steps, and the heat flux coming out of the planet oscillates about a value which remains constant. The mean temperature profile of the mantle is chosen such that the heating term aT’/dt’, and the misfit between the left- and right-hand sides of the conservation equation of thermal energy (equation (8)) are minimum. At the final stage of the numerical experiments, the results are subsequently recasted in a dimensional reference frame using the values listed in Tables 2 and 3. of the temperature profiles Surface gravity, 9 (m sP2) 3.7 Thermal diffusivity, IC(m’s_‘) 1o-6 A. Mocquet et al.: Theoretical seismic models of Mars Table 3. Input parameters of the three studied limit cases (Sotin et al., 1996) Model 1 Model 2 Model 3 Mean mantle density p, kg rn-’ 3416 3471 3471 Liquid core radius, km 1841 1546 Solid core radius, km 1338 1546 Total mass of the core M,, 1.7 x 1023 1.3 x 1023 1.3 x 1023 kg CMB temperature T,, K 1600 1700 Liquid core bulk modulus, GPa 145 200 T, values at the core-mantle boundary (CMB) include an adiabatic contribution equal to 0.1 Kkm-i. The values of bulk moduli were estimated by Sotin et al. (1996) after the experimental works of Boehler et al. (1990), Boehler (1992), and Fei et al. (1995). 2.2. Temperature andpressure projiles Following the studies by Schubert and Spohn (1990) and Sotin et al. (1996) on the crystallization of the Martian core, three limit cases are considered. The first case considers that the liquid core is enriched in sulfur, namely that the averaged mass fraction xFeS is equal to 0.608 (Schubert and Spohn, 1990). This hypothesis induces the presence of a large liquid core, 1841 km in radius, surrounding a solid core 1338 km in radius (Sotin et al., 1996). Conversely, both last limit cases consider that the core is uniquely composed of iron, either liquid (case 2) or solid (case 3). Since the density is unaffected by the liquid or solid state of iron, both cases correspond to a core radius equal to 1546 km. Additional values of the constant parameters are listed in Table 2, and the input parameters corresponding to the three different cases are listed in Table 3. At the final stage of the calculations, the values of Rayleigh number and kinematic viscosity are equal to 105, and 101gm2s-‘, respectively, for cases 1 and 2. In the solid core case, the final values of Rayleigh number and kinematic viscosity are equal to 8 x 105, and 5.3 x 10” m2 s-‘, respectively. In Fig. 1, the three temperature profiles of the mantle are plotted as a function of depth z, and compared to the previous result of Johnston and Toksiiz (1977). One of 0 P 400 1255 the main results of the computations is that the nature of the core (either liquid or solid) and the boundary conditions at the CMB have a minor influence on the values of the temperature over more than 65% of the mantle radius, namely from the surface down to 1200 km depth. Going from the surface downwards, the three profiles are first characterized by a linear increase of temperature with depth, with an associated slope equal to dT/dz = 4.4K km-‘. This linear increase of temperature defines a 300 km thick conductive thermal boundary layer. This latter value can be interpreted as representative of the lithospheric thickness. Both values of temperature gradient and lithospheric thickness are identical to the results of Johnston and Toksiiz (1977) in this depth range. A 300 km thick thermal lithosphere is also in good agreement with the thermal history calculations of Breuer et al. (1993), who included the effects of mantle differentiation by crustal growth. Breuer et al. (1993) obtained values of thermal lithosphere thickness as large as 15&250 km, and up to 500 km, in the northern and southern hemisphere of Mars, respectively. A maximum value of temperature (- 1600 K) is reached at a depth equal to1 600 km. This maximum is followed deeper by a negative gradient of temperature, of the order of -0.4 Kkn-‘. Down to 1200 km depth, the maximum difference between the three profiles hardly reaches 100 K. At greater depths, down to the CMB, more significant differences appear, due to the different core radii and boundary conditions at the CMB. When a liquid core is present (cases 1 and 2) the CMB is overlain by a thermal boundary layer, about 250 km thick, which is induced by the fixed temperature condition at the CMB. This thermal boundary layer vanishes in the case of a solid core (case 3), and the temperature remains almost constant at a value close to 1300 K, from 1200 km depth down to the CMB. These temperature profiles indicate that, below a depth of 300 km, the Martian mantle temperature is bracketed in a 1200-1600 K range of temperature. These latter values contrast with[ the model of Johnston and Toksdz (1977), which does, not include a decrease of temperature below the lithosphere, and where the temperature at the CMB reaches a high value equal to 2100K. The temperatures that we obtain are also up to 500 K colder than the values of Schubert et al. (1992). Since the three cases that we studied are limit cases, the stability of the profiles whatever the core radii or the boundary conditions strengthen our opinion that the mean temperature of the Martian mantle must be close to a value equal to 1400 K. The temperature profiles displayed in Fig. 1 can be reproduced using the fifth-order polynomial coefficients listed in Table 4. For a constant density Martian mantle, the radial dependence of pressure P(r) is given by l(Turcotte and Schubert, 1982) 1600 L i t / 400 800 / ,I 1200 Tempwature,K 1600 Fig. 1. Temperature profiles in the mantle of Mars. Plotted values include an adiabatic gradient of temperature equal to 0.1 Kkn-’ where M, is the total mass of both liquid and solid cores. In fact, it can be easily verified that, using equation (19) and the values listed in Table 3, the relatively small radius A. Mocquet 1256 Table 4. Fifth-order Core Liquid + solid Liquid Solid The temperature polynomial fit to the temperature Fig. 2. Relaxation -..._._---. profiles (Fig. 1) Cl, 105 c2, lo5 cg, 105 cq, 105 cg, 105 -0.9312 0.8347 0.2587 6.5817 - 5.9847 - 1.9590 - 17.6860 17.4590 6.3040 22.8560 -25.5170 - 10.2290 - 14.1190 18.6930 8.3332 3.3007 - 5.4823 -2.7055 T is given in Kelvin by T(x) = I’= ,,c,x’, where x is the normalized 38.193rlR (20) where the unit of P is GPa. The approximate relationship (20) does not give exactly P(R) = OGPa, but the discrepancy (0.407 GPa) has absolutely no effect on the results of the following sections. The pressure reached at the CMB is equal to 18 GPa in case 1, and 2 1.4 GPa in cases 2 and 3. In order to check the plausibility of a 1400 K Martian mantle, the relaxation time ratio r2/r,, (equation (3)) is computed as a function of pressure for five cases (Fig. 2) : the three models obtained in this study, the temperature profile proposed by Johnston and Toksoz (1977), and an adiabatic profile representative of the Earth’s upper mantle (Vacher et al., 1996). This latter linear profile is constrained using values of temperatures equal to 1523 K (Davaille and Jaupart, 1994), and 1873 K (y-spinel+perovskite + magnesiowtistite) at the base of the Earth’s lithosphere (80 km depth), and at 660 km depth, respectively. The curve corresponding to the temperature profile of Schubert et al. (1992) would follow the curve corresponding to the Earth’s case. Figure 2 shows that our temperature profiles are consistent with a low Martian mantle Q. Between 5 and 15 GPa, the relaxation time ratio z&, increases to values up to lo2 higher than in the Earth’s / seismic models of Mars co, 10s of planet Mars induces that, in any case, the radial dependence of pressure can be approximated by a straight line with sufficient accuracy. Moreover, the pressure profile of the first studied case differs by only 0.1 MPa km-’ from the pressure profile corresponding to cases 2 and 3. Therefore, we use a single pressure versus radius law whatever the studied case. This law is approximated by P(P) = 39.2- et al.: Theoretical Johnsto;:&To!isoz (1977) time ratios (equation (3)) corresponding to the three temperature profiles displayed in Fig. 1. Similar calculations for the model of Johnston and Toksiiz (1977) and an adiabatic model of the Earth’s upper mantle are shown for comparison. The temperature profile proposed by Schubert et al. (1992) would lead to a curve similar to the Earth’s case at pressures higher than 5 GPa radius (x = v/R). case. At higher pressures, the differences in temperature between the three models involve large variations of relaxation time ratios. For model 1 (liquid and solid cores case) zz/zo remains constant, whereas for model 3 (solid core case), z2/zo reaches values up to lo5 higher than the Earth’s values at P = 20 GPa. These are extreme cases. A mean mantle temperature of the order of 1400K (liquid core, case 2) leads to a maximum of a three decade shift of z2 with respect to the Earth’s value, as would be expected from the tidal Q values of the respective planets. On the other hand, mantle temperatures higher than 1800 K cannot explain the low Q value of Mars in a straightforward way. The temperature profile proposed by Schubert et al. (1992) would provide z2/zo ratios similar to the Earth’s values, and the model of Johnston and Toksiiz (1977) predicts a Q value higher than the Earth’s one. In both cases, the presence of volatile and/or partial melting in the mantle would be required to explain the low Q value of Mars at tidal frequencies. This additional explanation is not required by our models. Note that our three cases display a minimum zZ/zo value at a pressure close to 5 GPa, which corresponds to the base of the Martian lithosphere. Such a minimum should induce a minimum of attenuation in this depth range (Lognonne and Mosser, 1993). 3. Seismic structure of the Martian mantle The main result of the previous section was the very stable behaviour of both temperature and pressure profiles whatever the limit cases considered. Moreover, since the pressure gradient inside Mars is very small, it is expected that temperature will constrain more heavily the seismic structure of the mantle than pressure. With temperature and pressure profiles at hand, density and seismic velocity profiles are computed as a function of depth using Grtineisen’s and third-order finite strain theory (Duffy and Anderson, 1989; Vacher et al., 1996). At this stage, a compositional model of the mantle is necessary. Section 3.1 will briefly describe the method used for the computation of density and seismic velocity profiles as a function of temperature and pressure. The choice of the mineralogical models will subsequently be argumented, with emphasis on the iron content of the mantle. In Section 3.3 the seismic profiles corresponding to the different thermal and compositional states of the mantle considered will be presented. 3.1. Method The computation of seismic velocities and density from known thermodynamical conditions and mineraIogies has A. Mocquet et nl.: Theoretical seismic models of Mars been extensively explained by previous investigators (e.g. Davies and Dziewonski, 1975 ; Anderson, 1988 ; Duffy and Anderson, 1989; Vacher et al., 1996). Therefore, the method will be only briefly outlined in this paper. For specific formulas and computational details, we refer the reader to Duffy and Anderson (1989) and Vacher et al. (1996). First, available data on densities and thermo-elastical properties of mantle minerals are corrected for temperature effects at surface pressure conditions using Grtineisen’s theory. The corrected values are subsequently projected adiabatically at depth using third-order finite strain theory. In the convection experiments, the compressibility of mantle materials and hydrostatic pressure conditions at depths are neglected. The temperature profiles obtained previously are hence valid at zero pressure, and the individual temperature values can be used directly as a series of temperatures To(z) which correspond to the feet of the adiabats valid at the respective depths z. Duffy and Anderson (1989) showed that the uncertainties introduced by the approximations of the theory are much smaller than the uncertainties on the elastic and thermal parameters of mantle minerals provided by mineral physics experiments performed at surface pressure conditions. The maximum uncertainties on the computed densities and elastic moduli do not exceed 1 and 2% of their values, respectively. The first two steps of the procedure are performed separately for each individual mineral. The last step is to compute the elastic properties of the mantle from the properties of individual minerals. This is achieved by bracketing the averaged values of the elastic moduli for the composite material between highest and lowest bounds. The Voigt-Reuss-Hill (VRH) averaging method is often used for this purpose (e.g. Bass and Anderson, 1984). However, we prefer to use the more accurate procedure (HS) proposed by Hashin and Shtrikman (1963) which is based on energetic variational principles. Indeed, Watt et al. (1976) showed that the VRH average can be a poor approximation which can eventually lie outside the two HS bounds. The better accuracy of the HS procedure with respect to VRH has also been verified by Vacher et al. (1996). 3.2, Mineralogical models Since no seismological data concerning the interior of Mars are available yet, we base our calculations on crude mineralogical models. Doing so, we prefer to make a few very simple assumptions concerning the mineralogical composition of the mantle of Mars than to use rather detailed models (Dreibus and Wanke, 1985; Laul et al., 1986; Longhi et al., 1992), because, as has been noted by Bills and Rubincam (1995), these latter models are more constrained by plausible assumptions than relevant observations. The major mantle constituents of terrestrial planets are expected to be a-olivine, /3- and y-spine1 phases of olivine, garnet, clinopyroxenes, and orthopyroxenes (Ringwood, 1975). While some work has been done on the effects of the transformation of y-spine1 to perovskite on mantle convection of Mars (e.g. Weinstein, 1995), we do not need to consider ultra-high pressure phases such 1257 20 15 10 100 80 Mg2 Si O4 , Mel 60 % 40 Fig. 3. Phase diagram in the system Mg,SiOb-Fe$iO, at 1473K, after Katsura and Ito (1989).The grey shaded area indicates the domain studied in this paper : a, a-olivine ; b and y, p- and yspine1phases of olivine, respectively as magnesiowtistite, perovskite, and stishovite, because the pressure attained at the CMB does not exceed 21.5 GPa in our models. On the other hand, the pressure dependence of the phase transformations of olivine is strongly controlled by the iron content of minerals (Katsura and Ito, 1989). In the case of planet Mars, this pressure dependence is very important because the low pressure gradient of the mantle (equation (20)) implies that a relatively small change in pressure (e.g. 1 GPa) corresponds to a large variation of depth (> 85 km). In order to assess the influence of the molar fraction of iron X,, on the density and seismic structure of the mantle, we span a wide domain varying from X,, = 10 to 40%. The corresponding phase transformations are displayed in Fig. 3, and the mineralogical models are presented in Fig. 4. The increase of X,, has two main effects. First, it allows for the coexistence of two phases at the same pressure, for instance a-olivine and y-spine1 between 8 and 12GPa (X,, = 30%). We already pointed out that, within Mars, a small range of pressure corresponds to a large range of depths. Therefore, the coexistence of two different phases can occur over a large thickness. In the latter example, CIolivine and y-spine1 coexist over 360 km, from 660 down to 1020km (Fig. 4). Second, within the coexistence domain of two different phases, the iron content of one phase can be very high. For example, in the case X,, = 30%, the iron content of the y-spine1 phase at 8.5GPa reaches a value as high as 60% (Fig. 4). Such behaviours have important effects on densities and seismic velocities. This point is addressed in the next sub-section. In view of the uncertainties on the experimental data, the coexistence domain of two different phases is only taken into account when it spans more than 1 GPa. Therefore, the (a-olivine + fi-spinel) and (P-spine1 + y-spinel) domains which are present around 13 and 17 GPa, respec- 1800 y -spine1 . 1600 Gt 1400 y -spine1 Gt 1400 16 p-spine1 1200 4 1000 8 2 a 800 / / 600 cpx wolivine I- 400 1 a-olivine CPX 400 4 OP 200 0 I0 20 40 60 0 80 OP X 200 I I I 20 40 60 0 0 100 volume fraction, % I lO( volume fraction, % f I 1800 f80 I IXFe=40% . 1800 20 y-spine1 id0 . 1600 y-spine1 Gt 1400 16 1200 1400 . 1200 . Gt 17% i # A s k 4 1000 12 13% ” f \ 800 8 a-olivine 600 400 2 lo* z 2 5 5 800 “$‘O w 600 1 400 . 200 . a-olivine 4 200 0 O L 20 40 60 volume fraction, % Fig. 4. Simplified 0 0 I 20 I I80 40 60 volume fraction, % compositional models, based on the phase diagram displayed in Fig. 3. The coexistence of different phases of olivine is taken into account only if the involved pressure range extends over more than 1 GPa. The molar fraction of iron of each individual phase is indicated in per cent at the beginning and at the end of the coexistence domains : Gt, garnet ; Cpx, clinopyroxene ; Opx, orthopyroxene ; cc,ol-olivine ; p and y, p- and y-spine1 phases of olivine, respectively ; X,,, molar fraction of iron A. Mocquet et al.: Theoretical seismic models of Mars 1259 Table 5. Thermal and elastical parameters used in the calculations of densities and seismic velocities. Unless stated otherwise, the values are taken from DuEy and Anderson (1989) and are valid at pressure P = 0 GPa, and temperature T = 298 K a-Olivine y-Spine1 Pyrope 732 27.2” 3.222+1.182X,, 130b 82-31X,, 5.32 2.0 1.00188 952 21.5 3.472+1.240X,, 174 11&41x,, 6.42 2.0 1.00256 849 19.3 3.548+1.300X,, 184 11941x,, 16.5 1.5 1.00337 981” 23.8 3.562+0.758X,, 175 +x,, 90 + 8X,, 5.1 1.8 -0.016 -0.013 4.7* 1.9* -0.018 -0.014 4.8 1.8 -0.017 -0.014 4.9 1.4 -0.021 -0.010 5.044 2.05 QO, lO”Jmol-’ k, 1.00390 a,, lo-* @I,, K CI,10-6K-’ P, gcmp3 K, GPa G, GPa P-Spine1 aK/aP acyap aK/aT, GPa K-’ aG/aT, GPa K-’ CPx 3.93 1.75 1.00332 941” 25.5 3.277+0.380X,, 113+7x,, 67-6X,, 4.5 1.7 -0.013 -0.010 OPx 3.68 1.75 1.00402 935 26.0 3.204+0.799x,, 104 77-24X,, 5.0 2.0 -0.012 -0.011 Cpx, clinopyroxene ; Opx, orthopyroxene ; Q,,, ratio of heat capacity over thermal expansion at T = 0 K ; k,, anharmonic parameter proportional to the pressure derivative of the bulk modulus at T = 0 K ; a,, volume ratio at T = 298 and 0 K, respectively; Or,, Debye’s temperature ; cc,thermal expansivity ; p, density ; K, bulk modulus ; G, shear modulus ; X,,, molar fraction of iron. “Isaak et al. (1989). bIsaak (1992). “Ita and Stixrude (1992). *Ridgen et aE. (1992). tively, for X,, = 10% in Fig. 3, are not taken into account in Fig. 4, where the respective phase transitions are considered to occur sharply, A similar approximation is used for the (a-olivine + y-spinel) to P-spine1 transformation (X,, = 20%) at P = 12 GPa, where the (a-olivine + /?-spinel) coexistence domain is discarded. Since the coexistence of two phases induces a smoothing of the density and seismic velocity discontinuities (see Section 3.3), these approximations are equivalent to sharpen the discontinuities in the seismic models. 3.3. Density and seismic velocity proJiles The thermal and elastical parameters necessary for the computation of densities and seismic velocities at given pressure and temperature conditions are listed in Table 5. These experimental data rely basically on the compilation of Duffy and Anderson (1989) updated by later works of Isaak et al. (1989), Isaak (1992), Ita and Stixrude (1992) and Ridgen et al. (1992). The data available at the present time show a strong linear dependence of density and shear moduli values on the iron content of minerals. For instance, if X,, = lo%, the density of olivine phases increases and their shear modulus G decreases by 3.6% of their values at X,, = 0%. In comparison, a 3.6% decrease of the G value by temperature effects alone requires a thermal increase of the order of 270 K at surface pressure conditions. In addition, both density and G decrease with temperature at constant pressure. The bulk modulus K is not affected by the iron content of olivine phases. Therefore, since seismic velocities are proportional to the square root of the elastic mod&i, and inversely proportional to the square root of density, it is expected that seismic velocities are more sensitive to the X,, value than to the temperature difference between thermal profiles. This is clearly visible in Figs 5-7, where the computed densities, P-wave, and S-wave velocities, respectively, are plotted as a function of depth for different values of X,,, and for the three temperature profiles obtained previously. In each figure, the model of Anderson et al. (1977) is shown for reference. For a given X,, value, the density and seismic velocity profiles are almost identical whatever the temperature profile. Among the three limit cases considered in Section 1, the largest difference of temperature (400 K) was obtained at the CMB between cases 2 and 3. This difference of temperature corresponds to differences equal to 0.02 gcme3 (0.5%), 0.09 km s-’ (0.9%), an.d 0.07 km s-’ (1.3%), for density, V, and Vs, respectively. These latter values are within the range of uncertainty (l-2%) associated with the experimental data on thermal and elastical parameters. Therefore, in what follows, we consider density and seismic velocity profiles averaged over the three limit cases considered in Section 1. These averaged profiles are considered to be a good first-order approximation of the radial upper mantle structure of Mars for a given iron content of mantle minerals, whatever the structure of the Martian core. The averaged’ profiles, listed in Table 6, display the following characteristics. As noted previously by Anderson et al. (1977), the values of density and seismic velocity are within the range of values attained in the Earth’s transition zone. The seismic structure at the CMB on Mars is close to the structure of PREM (Dziewonski and Anderson, 1981) at a depth of 600 km. The uppermost 300 km of the Martian mantle are characterized by a lowvelocity zone (LVZ) which corresponds to the shallow conductive thermal boundary layer observed in Fig. 1. This LVZ is due to the increase of temperature with depth (4.4 K km- ‘) which is relatively large when compared with the small pressure gradient (0.01 GPa km-‘) in this depth range. If we take the density and P- and S-wave velocities 1260 A. Mocquet $, 3.8 et ul.: Theoretical seismic models of Mars - 3.4 ” 3.2t:’ 0 0 ” 500 ’ ” 3.2” ” ” 500 ” ’ ” ” 1500 1000 depth, km ’ ” ” I’ 3.2 2000 :I ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ L ’ 500 0 ” ’ ” 1500 3.2 ’ ” 2000 km .’ 0 1500 1000 depth, 1000 depth, ’ * ” 2000 km ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ 500 1500 1000 depth, 2000 km Fig. 5. Density versus depth profiles computed for the four compositional models displayed in Fig. 4, and for the three temperature profiles displayed in Fig. 1 and listed in Table 4. Heavy solid curve, case 1 (liquid and solid cores) ; thin solid curve, case 2 (liquid core) ; heavy dashed curve, solid core (case 3); dotted curve, density model of Anderson et al. (1977). When the value of X,, is fixed, the density profiles are almost indistinguishable whatever the case at a depth of 60 km as reference values, these parameters decrease by amounts of 0.5, 2, and 3%, respectively, within the LVZ of PREM (Dziewonski and Anderson, 198 1). These relative decreases reach the same amounts in our models of Mars, regardless of the X,, value, except for S-wave velocities, for which the relative decreases reach values as high as 5%. We can thus conclude that a LVZ similar to the Earth’s one should exist at the base of the Martian lithosphere. As stated previously, X,, is the parameter which mainly controls the variations of density and seismic velocities among all models. First, an increase of X,, results in an increase of the densities, and in a decrease of seismic velocities. For instance, the values of p and Vs for X,, = 20% differ by 2% from their respective values at Xr, = 10%. Similarly, the values for X,, = 30% vary by 4% from the values corresponding to X,, = 10%. The effect on V, is smaller in our calculations (1.4%) because, to our knowledge, there is no experimental data relating the bulk modulus and the iron content of olivine phases (Table 5). This value of 1.4% should thus be regarded as a lower bound on the decrease of P-wave velocities between X,, = 20 and 10%. The relative variations quoted above might appear small when compared to the relative uncertainties (l-2% ; Duffy and Anderson, 1989) associated with the laboratory data listed in Table 5. However, it must be kept in mind that these relative variations of seismic velocities extend over the entire mantle. Therefore, A. Mocquet et al.: Theoretical seismic models of Mars 126 8.5 8.0 8.5 - 7.5t:’” a 8.0 .--- I’ ” 500 ” ” ” ” ” 1500 1000 ’ I1 7.5 2000 0 500 depth, km 1500 1000 depth, 2000 km 10.0 8.5 8.0 ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ 7.& 0 500 1500 1000 depth, 2000 0 km 500 1500 1000 depth, 2000 km Fig. 6. Same as Fig. 5 for P-wave velocities as seismic waves travel inside the mantle, time delays are accumulating along ray pass. The preliminary calculations that we are presently carrying out show that the P-wave travel times computed using the X,, = 30% model are delayed by an amount of 10 s with respect to the travel times associated with the X,, = 10% model; for epicentral distances larger than 3.5” (Mocquet et al., 1996). The second effect of X,, on the density and seismic velocities is to control the sharpness of seismic discontinuities associated with the phase transitions of olivine. In Section 3.2, we pointed out that, according to Katsura and Ito (1989), an increase of the Xr, value induces the coexistence of different phases of olivine over a large range of depths (Figs 3 and 4). In terms of density and seismic velocity profiles, this gradual transition from one phase to another one smoothes out the discontinuities over the thickness of the coexistence domain of olivine phases (Figs 5-7). In what follows, we will only describe the behaviour of seismic discontinuities for P-waves (Fig. 6) because identical descriptions can be made regarding the behaviour of density and S-wave velocities (Figs 5 and 7, respectively) using the values listed in Table 6. For an Earth-like composition (X,, = 10%) the a-olivine to fispinel, and /?-spine1 to y-spine1 phase transitions translate into velocityjumps equal to 0.51 km s-l (5.5%) at 1130 km depth, and 0.09 km s-r (0.9%) at 1425 km depth, respectively. For X,, = 20 and 30%, the velocity jumps appear at a shallower depth, around 1000 km. The amplitude of the X,, = 20% discontinuity is similar to the amplitude of the X,, = 10% discontinuity. For X,, = 30%, this velocity jump decreases to 0.26 kms-’ (2.9%), and vanishes for X,, = 40%. For X,, values higher than lo%, the dis- A. Mocquet et al.: Theoretical seismic models of Mars 1262 4.2~~“““““““““,I 0 500 ’ ” 4.2”’ 1000 depth, km 2000 1500 0 ’ ’ ’ ’ ’ ” 500 ’ ’ ’ ’ ’ ’ ” 1000 depth, ’ 1500 2000 1500 2000 km 5.2 4.8 4.8 4.6 4.6 4.4 4.4 4.2”’ ” 0 ’ ” 500 ” ” ’ ” 1000 depth, ” 1500 ” I .’ b ’ ” 2000 0 km 500 1000 depth, km Fig. 7. Same as Fig. 5 for S-wave velocities continuity at 1425 km depth disappears. The smoothing process of the 1130 km discontinuity is accompanied by an increase of the velocity gradient dV,/dz over a 300 km thick layer, in the 83&l 130 km depth range, where dI/,/dz increasesfr0m0.11s-‘(X,,=10%)t00.18s-’(X,,=30%). Therefore, an iron-rich Martian mantle should rather be characterized by large seismic velocity gradients extending over a thickness of several hundred kilometres, than by sharp seismic discontinuities. We would like to emphasize that the effects of the iron content described in the previous paragraphs are valid independently of the chosen temperature profile. Indeed, densities and seismic velocities computed using the temperature profile of Johnston and Toksiiz (1977) display identical characteristics to those described previously : an increase of X,, induces an increase of the densities, a decrease of seismic velocities, and a smoothing out of the seismic discontinuities associated sitions of olivine (Fig. 8). with the phase tran- 4. Discussion In the previous sections, we described the influence of the iron content of the Martian mantle on the behaviour of phase transitions, but we neglected the consequences of these phase transitions on the temperature profiles, because these latter effects had not been taken into account in the convection experiments. In fact, both CIolivine to /?-spinel, and p-spine1 to y-spine1 phase transformations are exothennic, and hence increase the temperature of the mantle. This “Verhoogen effect” (Jeanloz and Thompson, 1983) results in an increase of temperature A. Mocquet et al.: Theoretical seismic models of Mars 1263 Table 6. Averaged density p and seismic profiles of the Martian values are not included in this table x,, = Depth &ml 0 59 119 178 238 297 356 416 475 534 594 653 712 772 831 891 950 1009 1069 1128 1188 1247 1306 1366 1425 1484 1544 1603 1662 1722 1781 1841 1852 (g &-') 3.39 3.38 3.37 3.37 3.37 3.37 3.37 3.39 3.40 3.42 3.44 3.46 3.47 3.49 3.52 3.55 3.58 3.62 3.65 3.68 3.82 3.84 3.85 3.86 3.87 3.92 3.94 3.95 3.96 3.97 3.98 3.99 3.99 10% x,, VP (km s-‘) (km s-‘) 8.32 8.26 8.18 8.13 8.10 8.09 8.11 8.15 8.20 8.26 8.32 8.39 8.46 8.53 8.61 8.73 8.84 8.95 9.06 9.19 9.70 9.75 9.80 9.84 9.88 9.97 10.02 10.08 10.11 10.13 10.16 10.18 10.19 4.82 4.75 4.68 4.62 4.58 4.56 4.55 4.55 4.56 4.58 4.60 4.62 4.64 4.67 4.70 4.76 4.81 4.86 4.90 4.97 5.32 5.35 5.36 5.38 5.39 5.42 5.44 5.46 5.47 5.48 5.48 5.49 5.49 VS mantle, computed = 20% for different molar fractions x,, = 30% VP VS (gcz-‘) (kms-‘) (kms-‘) (g c&‘) 3.46 3.45 3.44 3.43 3.43 3.43 3.44 3.45 3.47 3.48 3.50 3.52 3.54 3.56 3.59 3.62 3.67 3.72 3.84 3.87 3.89 3.92 3.97 3.99 3.99 4.00 4.01 4.03 4.04 4.05 4.06 4.07 4.07 8.20 8.14 8.07 8.01 7.98 7.98 7.99 8.03 8.09 8.14 8.21 8.28 8.34 8.41 8.49 8.61 8.76 8.92 9.38 9.49 9.58 9.63 9.70 9.79 9.83 9.86 9.89 9.95 9.98 10.01 10.03 10.05 10.06 4.72 4.66 4.58 4.53 4.48 4.46 4.45 4.46 4.46 4.48 4.50 4.53 4.55 4.57 4.61 4.66 4.74 4.83 5.14 5.19 5.23 5.24 5.26 5.30 5.31 5.32 5.34 5.37 5.37 5.38 5.39 5.39 5.39 3.52 3.51 3.50 3.50 3.49 3.50 3.51 3.52 3.53 3.55 3.57 3.59 3.61 3.64 3.69 3.76 3.81 3.87 3.98 4.00 4.02 4.03 4.05 4.06 4.07 4.08 4.09 4.11 4.12 4.12 4.13 4.15 4.15 lower than lOOK. In the case of the a-olivine to /?-spine1 phase transformation within the Earth, at 410 km depth, Vacher et al. (1996) computed a value of P-wave discontinuity (0.40 kms-‘) very close to the value of the spherically symmetric Earth’s model IASP (0.33 km s-’ ; Kennett and Engdahl, 1991), when the Verhoogen effect was taken into account. If this latter effect was neglected, the velocity jump discrepancy was doubled. Since the Verhoogen effect tends to diminish the values of velocity jumps at seismic discontinuities, the values determined in the preceding section should thus be regarded as maximum values. It is therefore expected that the mantle of Mars does not display sharp seismic discontinuities, in contrast with the model initially proposed by Anderson et al. (1977) (dotted curves in Figs 5-Q but that it is rather characterized by smooth velocity gradients. Zhou et al. (1995) considered an Earth-like composition for the Martian mantle (X,, = 12%), and showed that, in this case, the phase transitions of olivine could favour the amplification and superheating of megaplumes in Mars. However, these effects remain locally distributed in space and should not affect significantly the average temperature profile of the mantle. On the other hand, if of iron X,,. Crustal x,, = 40% VP VS (km s-‘) (km s-‘) (g c&-j) (km s-‘) (km s-l) 4.63 4.56 4.49 4.43 4.38 4.36 4.35 4.36 4.37 4.39 4.41 4.43 4.46 4.50 4.58 4.67 4.77 4.87 5.03 5.09 5.15 5.17 5.19 5.20 5.22 5.23 5.24 5.27 5.28 5.28 5.29 5.29 5.29 3.59 3.58 3.57 3.56 3.56 3.56 3.57 3.58 3.60 3.64 3.68 3.73 3.77 3.82 3.85 3.91 3.95 4.00 4.04 4.07 4.07 4.11 4.12 4.14 4.15 4.16 4.17 4.18 4.19 4.20 4.21 4.22 4.23 7.97 7.91 7.84 7.78 7.75 7.75 7.77 7.81 7.86 7.95 8.06 8.17 8.29 8.41 8.54 8.72 8.90 9.07 9.21 9.32 9.41 9.46 9.50 9.54 9.58 9.61 9.64 9.70 9.73 9.75 9.78 9.80 9.81 4.53 4.46 4.39 4.33 4.29 4.26 4.26 4.26 4.27 4.31 4.37 4.42 4.48 4.55 4.62 4.71 4.81 4.90 4.97 5.02 5.05 5.08 5.09 5.11 5.12 5.13 5.14 5.17 5.18 5.19 5.19 5.20 5.20 8.09 8.02 7.95 7.89 7.86 7.86 7.90 7.92 7.97 8.03 8.09 8.16 8.23 8.32 8.46 8.64 8.82 9.00 9.26 9.40 9.53 9.58 9.62 9.66 9.70 9.73 9.76 9.82 9.85 9.88 9.90 9.93 9.94 VP VS the iron content of the Martian mantle is greater than that of the Earth, the induced smoothness and homogenization of mantle structure should diminish the influence of phase transitions on the geometry of mantle convection. 4.1. Limitations of the mineralogical models The mineralogical models that we use in this study present two major crude simplifications. First, the volume fraction of olivine vs. garnet and pyroxenes remains constant whatever X,,. Doing so, we follow the usual procedure which separates the bulk composition of the mineral assemblage in two subsystems, olivine on one hand, and the remaining minerals on the other hand (Jeanloz and Thompson, 1983 ; Irifune, 1987). It is hence assumed that both subsystems do not affect each other’s phase equilibria (Ita and Stixrude, 1992). Ita and Stixrude (1992) noticed that this assumption is consistent with the results of Akaogi and Akimoto (1979) which show no change in the relative proportions of both subsystems up to at least 20 GPa. Second, the lack of experimental data does not 1264 A. Mocquet et al.: Theoretical seismic models of Mars L5 ti 4.2 c 8 tb i: .% 2 4 _g 0.5 4 -1 3.8 0.0 1 [i P ; -0.5 L -1.0 3.6 Anderson et al. (1977) i 3.2 0 1000 Depth, km 500 1500 2000 0 500 1000 Depth, km 1500 2000 Fig. 9. Relative variations between the values of densities and seismic velocities obtained for a pure olivine mantle (X,, = 30%), and the mineralogical model valid for X,, = 30% (Fig. 4), using an identical amount of iron for all minerals. The values obtained for the case of the pure olivine mantle are used as references. All calculations are performed using a temperature distribution averaged over the three profiles displayed in Fig. 1 ..’ 4.2 0 _:I 0 Anderson et al. (1977) ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ 1000 500 1500 Depth, km ’ ’ 2000 los? Anderson et al. (1977) 0 500 1000 Depth, km Fig. 8. Same as Figs 5-7 using the temperature 1500 2000 profile of John- previously. The first case considers a pure olivine mantle with X,, = 30%. In the second case, the mineralogical model valid for X,, = 30% is used (Fig. 4), but an identical amount of iron is equally assigned to all minerals. The values obtained for a pure olivine mantle are used as references. The relative variations between both cases are plotted as a function of depth in Fig. 9. As can be expected from Fig. 4, the main differences (< 1.5%) occur down to 500 km depth. At greater depths, the decreasing amount of pyroxenes induces a sharp decrease of the relative variations. Below 1000 km, these latter never exceed - 0.4%, and l%, for seismic velocities and density, respectively. Even though this test is performed for two extreme cases, these latter values are smaller than the uncertainties of laboratory measurements, and more than one order of magnitude smaller than the variations of densities and seismic velocities reported in the previous section. Therefore, present-day available data on the behaviour of pyroxenes and garnets as a function of their iron content (Table 5 ; Duffy and Anderson, 1989) support our hypothesis that the influence of the iron content of the mantle on its seismic structure is mainly governed by olivine. 4.2. Relationships between mantle and core structures ston and Toksiiz (1977) let us take into account the effect of the increasing amount of iron in pyroxenes and garnets. Our calculations are thus based on the basic assumption that the phase transitions in the olivine system are the major causes of seismic discontinuities (e.g. Ringwood, 1975), whereas other minerals form a complex solid solution with transitions spanning a wide depth interval (Akaogi et aZ., 1987). In order to test the influence of this assumption on our results, the distributions at depth of densities and seismic velocities are computed for two additional limit cases, using a temperature profile averaged over the three ones obtained In the previous section, we pointed out that the density and seismic velocity profiles were almost independent of the thermal history and present-day structure of the core, and a large domain of iron content was considered for the mantle. Even though astronomical constraints on the inner structure of Mars are sparse, we can however test our models by computing their associated ranges of Love numbers, Q factors (equations (1) and (2)), and I/MR’ ratios. The Love numbers h, and k, are computed for y1= 2, 3, and 4 using the values of Table 6. The bulk modulus of the liquid and solid cores (Table 3) were estimated by Sotin et al. (1996) using the experimental data of Boehler A. Mocquet et al.: Theoretical seismic models of Mars 1265 0.35 0.30 0.25 c 0.20 0.15 0.10 0.05 LO 15 20 25 30 35 40 xFe% 0.20 = 1750 km (LM) \\\\S\\\\\ 0.15 ti 0.10 0.05 0.00 r I I I I I I 10 15 20 25 30 35 40 xFe% Fig. 10. Love numbers h, and k, (n = 2, 3, and 4) corresponding to the models of Table 6. Due to the lack of data on the shear modulus of iron at the pressure and temperature conditions of a solid Martian core, a liquid core is assumed (Table 3). The values computed by Lambeck (1979) and Lognonne and Mosser (1993) (LM) are also shown et al. (1990), Boehler (1992), and Fei et al. (1995). To our knowledge, there is no experimental determination of the shear modulus of iron at the pressures and temperatures relevant to a Martian solid core. An extrapolation of Poisson’s ratio of the Earth’s inner core to Martian pressure conditions yield a very low value, of the order of 12GPa. The very large difference between Martian and Earth’s core pressure conditions makes this estimate very suspect. Therefore, we prefer not to consider the solid core, and focus instead on the radius of the liquid core. The results (Fig. 10) are in a very good agreement with previous authors’ estimates. The values increase with increasing core radius, as it is predicted by the theory. In addition, an increase of the iron content of the mantle induces a small increase of the Love numbers (N 10% between X,, = 10 and 40%). The Q values corresponding to the k2 values shown in Fig. 10 are, following equation (2), in the range 48 < Q < 95. Our models thus favour a very low Q Martian mantle, with 50~ Q< 100 at tidal frequencies. Following Bills (1990), the mean density (p), and the mean principal moment of inertia M,, with M2 = ; <p)I/MR’ (21) enable to bracket the density versus depth distribution of the planet. Apart from petrological or geochemical arguments on the composition of the Martian crust, mantle, and core, an additional condition must be fulfilled: if the core is composed of pure iron and/or iron sulfur, its mean density must be greater than 5.77 g cme3, and lower than 8.09gcmM3 (Schubert and Spohn, 1990). Under such constraints, possible values of outer core radius and core density, and the corresponding moment of inertia ratios I/MR2, can be computed for each of the models of mantle density listed in Table 6. Three limit cases are considered (Fig. 11). In the first case (top panel) a two-layered model without crust is considered. A threelayered model (middle panel), where the mean crustal density is assumed at a value equal to 2.64gcmp3 (Anderson et al., 1977) is considered in the second case. The crustal thickness is set equal to 100 km. The two latter cases have been chosen in such a way that they bracket the presently unknown averaged crustal thickness of Mars. The last case (bottom panel) considers a four-layered model. Crustal parameters are identical to the previous case, and, following Sotin et al. (1996), a high density (8.09 g cm-“) solid inner core is assumed., with a radius equal to 1338 km. Unknown parameters are the radius and density of the overlying liquid outer core. In Fig. 10, the straight dashed lines correspond to .the computed outer core radii. Their respective values are indicated in km at the end of each line. Following Bills (1990), we consider that I/MR2 cannot exceed 0.365. As expected from the definition of the mean principal moment of inertia, the presence of a thick low-density crust shifts the computed values of outer core radii towards smaller values of IjMR” when X,, is set at a constant value. The domains of possible values of outer core radius, outer core density, and X,, content of the mantle are in very good agreement with the results of previous investigators. For example, if we assume an I/MR2 value close to 0.365, an outer core radius equal to 1700 km is obtained either with a very thin crust and a Martian mantle composition close to that of the Earth (X,, = 10% ; top panel), or with a thick crust and an iron-rich Martian mantle (X,, = 30% ; middle panel). This value of outer core radius agrees with the previous estimate of Longhi et al. (1992). Though we did not use geochemical arguments in our modelling approach, the density versus depth profiles computed for X,, = 20 and 30% (Table 6) support previous propositions that the mantle of Mars contains a large proportion of iron with respect to the Earth’s mantle (Dreibus and Wanke, 1985 ; McSween, 1985). According to Fig. 10, iron contents higher than Xr, = 30% should be avoided, because, whatever the considered case (two-, three-, or four-layered model), these contents lead to I/MR2 values higher than 0.365. This is particularly visible for X,, = 40%, for which I/MR2 values as high as 0.380 (top panel) and 0.370 (middle panel) are obtained for the two- and three-layered models, respectively. Iron contents higher than 20% are also impossible if a four-layered planet is considered (bottom panel), because these contents involve unrealistic liquid core densities lower than 5 gem-3. Two additional conclusions can be drawn from Fig. 10. First, ifwe consider that an Earth-like mantle composition A. Mocquet 1266 0.350 0.360 0.370 0.380 outer core should et al.: Theoretical be small, seismic models of Mars 8.0 of 30&400 km. the weakness (or magnetic field on of the order This small thickness might explain absence?) of an internally generated Mars. 5. Conclusion 8.0 5.0 j t I/Ma2 Fig. 11. Domains of compatibility between profiles of mantle density (Table 6), outer core radius (labelled dashed curves, km) and density, and principal moment of inertia ratio I/MR’. The rectangles delimit the domain of realistic possibilities. They are defined such that the I/MR2 ratio is lower or equal to 0.365 (Bills, 1990), and that the averaged outer core density is comprised between 5.77 and 8.09 gcme3 (Schubert and Spohn, 1990). Open circles, X,, = 10% ; black dots, X,, = 20% ; open squares, X,, = 30% ; black squares, X,, = 40%. Top panel, two-layered planet (mantle and core); middle panel, three-layered planet (crust, mantle, and core) ; bottom panel, four-layered planet (crust, mantle, outer and inner core). A 100 km thick crust with an average density equal to 2.64 gcmm3 (Anderson et al., 1977) is considered in both latter cases. An inner core radius equal to 1338 km and an inner core density equal to 8.09 g cme3 are used for the four-layered planet case (X,, = 10%) represents of the Martian mantle, the lowest limit of the iron content the ratio I/MR2 cannot be lower than 0.355. Second, if a solid inner core is present centre of the planet, the thickness of the overlying at the liquid The present-day averaged temperature profile of the Martian mantle is found to be almost independent of the thermal history of the core. A 300 km thick thermal lithosphere, displaying a temperature gradient equal to 4.4 K km-’ is followed at greater depths by a quasi-isothermal mantle, the temperature of which is bracketed in a 1200-l 600 K temperature range. These temperature and associated seismic models favour a very low Q Martian mantle, with 50 < Q < 100 at tidal frequencies. The lithospheric gradient of temperature, together with the small increase of pressure with depth, of the order of 0.01 GPa km-‘, induce the presence of a low-velocity zone similar to that of the Earth, down to 300 km depth. At greater depths, computed densities and seismic velocities have the same order of magnitude as within the Earth’s transition zone. An increase of the iron content of the Martian mantle with respect to that of the Earth results (1) in an increase of density, and a decrease of seismic velocities, which can reach more than 2% of the values expected from an Earth-like composition, (2) in a homogenization of mantle structure through the smoothing out of seismic discontinuities over a thickness of a few hundred kilometres. It is therefore expected that a composition of the mantle of Mars similar to the one derived from the studies of SNC meteorites (Ringwood, 1979; Dreibus and Wanke, 1985 ; McSween, 1985) should be detectable by seismic methods. Aclznowledgements. This work has been conducted as a contribution to the preparation of future exploratory missions to Mars, as a collaboration between European, American, and Russian space agencies. Financial support by French Ministry of Research, Centre National de la Recherche Scientifique (C.N.R.S.) and Programme National de Planetologie are acknowledged. 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