Publications (166)996.28 Total impact
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ABSTRACT: The total electron content (TEC) of the solar corona in June 2002 is calculated by three observational techniques and the results are compared. The first technique is solar rotational tomography (SRT) applied to a 14day time series of LASCOC2 polarized brightness images, and the other two techniques use the Cassini spacecraft radio beacon for Doppler tracking (phase delay) and ranging (group delay). While the Dopplertracking technique has an arbitrary zeropoint, it is otherwise found that the three methods produce consistent estimates of the TEC to within established uncertainties, providing an independent check on the calibrations. The verification of the accuracy of the Dopplertracking technique enables a significant improvement to the use of spacecraft data sets in studying the heliosphere: the density component to Faraday rotation can be separated from the magneticfield component as variable structures cross, such as coronal mass ejections and magnetohydrodynamic waves. Furthermore, we show that the unique frequencytime variable characteristics of the hydrodynamic components of waves can be studied. Based on this work, future Faraday rotation studies of variable solar phenomena will isolate the electron density changes from the magneticfield contribution. This capability will enable advanced research into variable heliospheric magnetic fields. 
Article: Constraining the Location and Dimensions of Mass Anomalies on Mercury from Mariner 10 Doppler Data
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ABSTRACT: Analysis of radio Doppler data generated by the Deep Space Network with Mariner 10 during its first and third encounters with Mercury yielded a quadrupole gravitational field with J2 equal to 6.0 ± 2.0 and C22 equal to 1.0 ± 0.5 in units of 105 (Anderson et al., Icarus 71, 337, 1987) . However, this underlying global field leaves systematic Doppler residuals for the third encounter (Esposito et al., COSPAR: Space Res. 17, 639, 1978), residuals that are most likely caused by a large gravity anomaly in the region of closest approach to Mercury at latitude 67.96° and east longitude 53.09°. We report here a detailed characterization of the likely sources producing the putative gravity anomaly. The recovered Doppler residuals and ground track from Esposito et al. (1978) are fit by a model that includes the spacecraft's six trajectory initial conditions along with Mercury's mass GM = 22,032.09 ± 0.91 km3 s2 (Anderson et al., 1987) and the two quadrupole coefficients. After convergence to the bestfit trajectory, any remaining residuals represent an unmodeled signal that is assumed to arise from anomalous mass concentrations on Mercury plus noise. In order to reduce the noise evident in the Doppler residuals, we smooth them with a variablewidth Gaussian filter (Palguta et al., Icarus 180, 428, 2006). The filter width in the time domain increases with the spacecraft altitude, reducing the noise before and after closest approach. Accelerations along the line of sight (LOS) are calculated by sampling the differentiated Doppler smoothing curve at a 10second time interval, the sample interval for the Doppler frequency data. Multiple sphericalcap disk models are then used to fit the LOS acceleration data. The sphericalcap disk models not only provide the locations and magnitudes of anomalous mass concentrations on Mercury, but also their vertical and horizontal dimensions. We find that a minimum of four mass anomalies on or near Mercury's surface is required to explain the LOS acceleration data. Although at least four masses are required to reproduce all the major acceleration features, we show that the fit to the data can be improved by including up to seven sphericalcap disks. The modeled mass anomalies are on the order of 1018  1019 kg. Additionally, at least two negative and two positive mass anomalies are present in each model. Although there is some variability in the placement of the mass anomalies among the different models, we find that positive mass anomalies are typically found near the beginning and end of the Mariner 10 trajectory path (20° N, 25° E) and (55° N, 177° E). 
Article: Jupiter: Internal Dynamics and Shape
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ABSTRACT: The physical shape of a giant planet reveals important information about its rotation and internal structure. We investigate how differential rotation on cylinders affects Jupiter's shape. We project Jupiter's measured zonal wind velocities along cylinders to describe its centrifugal potential which is then used to derive Jupiter's shape using an equipotential surface theory. The derived shape for different cylindrical radii is then compared with Jupiter's shape from radio occultation measurements. It is found that both solidbody rotation (System III rotation rate) and differential rotation up to a latitude of ~ 2030 degrees are consistent with Jupiter's measured shape. We next use a firstorder theory that relates the second gravitational coefficient J_2 to the flattening to calculate the corrections to J_2 for the different rotational configurations. We find that the contribution of the flattening to J_2 is significant. We therefore suggest that interior models of the giant planets must account for J_2n corrections caused by both shape (flattening) and internal dynamics. 
Article: FirstOrder Theory of Figures for Synchronous Rotation and Tides: Application to Rhea and Titan
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ABSTRACT: A new approach is presented to evaluate the shape, the gravitational coefficients J2 and C22 and the normalized axial moment of inertia C/MR2 for a rotating, axially symmetric satellite in hydrostatic equilibrium and distorted by synchronous rotation and tides. C is the axial moment of inertia and M and R are the mass and radius of the body, respectively. The theory is valid for an arbitrary interior density profile. Application is made to Rhea and Titan assuming that these bodies are in hydrostatic equilibrium. A likely internal structure for Rhea is a uniform mixture of ice and rock, 75% ice and 25% rock, by mass, with an ice Iice II phase change occurring within Rhea at a fractional radius of about 0.4 to 0.55.  [Show abstract] [Hide abstract]
ABSTRACT: Asteroid 21 Lutetia was approached by the Rosetta spacecraft on 10 July 2010. The additional Doppler shift of the spacecraft radio signals imposed by 21 Lutetia's gravitational perturbation on the flyby trajectory were used to determine the mass of the asteroid. Calibrating and correcting for all Doppler contributions not associated with Lutetia, a leastsquares fit to the residual frequency observations from 4 hours before to 6 hours after closest approach yields a mass of (1.700 ± 0.017) × 10(18) kilograms. Using the volume model of Lutetia determined by the Rosetta Optical, Spectroscopic, and Infrared Remote Imaging System (OSIRIS) camera, the bulk density, an important parameter for clues to its composition and interior, is (3.4 ± 0.3) × 10(3) kilograms per cubic meter.  [Show abstract] [Hide abstract]
ABSTRACT: The Rosetta spacecraft encountered its second asteroid target (21) Lutetia on 10th July 2010. The asteroid perturbed the flyby trajectory and velocity of the spacecraft (closest approach is at 3168 km). The mass of the asteroid was determined from the shift of the radio carrier signal frequency at Xband (8.4 GHz). Altough the flyby geometry as suboptimal and there is a tracking gap at closest approach, the mass was determined to 1.7 1018 kg at an uncertainty of 1%. Major driver of the uncertainty are the frequency noise level, the tropospheric correction and the uncertainty of the closest approach distance. The Rosetta camera OSIRIS determined the size and volume of Lutetia. The bulk density is derived from the determined mass and volume to (3400 +/ 275) kg/m3. The precision of the bulk density is driven by the precision of the volume estimate. Knowledge of the mass and bulk density is an important contributor to understand the asteroid's composition, internal structure and porosity. Lutetia is considered to be a major perturber of a number of smaller asteroids and a perturber of the motion of Mars. The derived mass from the Rosetta flyby will therefore be compared with those mass values derived from astrometry.  [Show abstract] [Hide abstract]
ABSTRACT: The moment of inertia of a giant planet reveals important information about the planet's internal density structure and this information is not identical to that contained in the gravitational moments. The forthcoming Juno mission to Jupiter and the Solstice Mission (Cassini XXM) to Saturn might determine the angular momentum of the planets, and therefore their moments of inertia NMoI=C/MR2 by measuring the planets' pole precession, and the LenseThirring acceleration of the spacecraft (C is the axial moment of inertia, and M and R are the planet's mass and mean radius, respectively). The possible range of NMoI values for Jupiter and Saturn based on their measured gravitational fields using a simple core/envelope model are presented. The model suggests that Jupiter's NMoI lies in the range 0.2629  0.2645. Saturn's NMoI is found to be ∼ 0.218. Constraining Saturn's NMoI value, however, is possible only if an accurate determination of Saturn's rotation period is available.  [Show abstract] [Hide abstract]
ABSTRACT: The present OSS mission continues a long and bright tradition by associating the communities of fundamental physics and planetary sciences in a single mission with ambitious goals in both domains. OSS is an Mclass mission to explore the Neptune system almost half a century after flyby of the Voyager 2 spacecraft. Several discoveries were made by Voyager 2, including the Great Dark Spot (which has now disappeared) and Triton's geysers. Voyager 2 revealed the dynamics of Neptune's atmosphere and found four rings and evidence of ring arcs above Neptune. Benefiting from a greatly improved instrumentation, it will result in a striking advance in the study of the farthest planet of the Solar System. Furthermore, OSS will provide a unique opportunity to visit a selected Kuiper Belt object subsequent to the passage of the Neptunian system. It will consolidate the hypothesis of the origin of Triton as a KBO captured by Neptune, and improve our knowledge on the formation of the Solar system. The probe will embark instruments allowing precise tracking of the probe during cruise. It allows to perform the best controlled experiment for testing, in deep space, the General Relativity, on which is based all the models of Solar system formation. OSS is proposed as an international cooperation between ESA and NASA, giving the capability for ESA to launch an Mclass mission towards the farthest planet of the Solar system, and to a Kuiper Belt object. The proposed mission profile would allow to deliver a 500 kg class spacecraft. The design of the probe is mainly constrained by the deep space gravity test in order to minimise the perturbation of the accelerometer measurement.   [Show abstract] [Hide abstract]
ABSTRACT: The shapes and gravitational fields of rotationally and tidally distorted planets and satellites depend on their interior mass distributions. Measurements of these observable characteristics are therefore used to infer the internal structure of planetary bodies. Interpretations are based on approximate formulae such as the RadauDarwin relation derivable from the theory of figures or more accurate evaluations of the theory. The exact solution for the shape and gravitational field of the rotationally distorted constant density Maclaurin spheroid has, until now, provided one of the only ways to assess the accuracy and range of validity of approximate theory of figure predictions. We generalize the Maclaurin spheroid solution to a 2layer coreenvelope body, a more realistic model of a real planet or moon. The exact 2layer Maclaurin spheroid solution, e. g., the shapes of the surface and coreenvelope interface, depend on 3 parameters, the coreenvelope density ratio, the fractional volume of the core, and Omega2/2piGrho2, where Omega is the rotation rate, G is the gravitational constant, and rho2 is the envelope density. For realistic parameter values, the flattening of the interface is smaller than that of the surface. Results of the exact solution are compared with predictions of the theory of figures up to order 3 in the small rotational parameter of the theory. The exact solution serves as a benchmark for numerical models that attempt to invert gravitational and shape data to infer internal planetary structure.  [Show abstract] [Hide abstract]
ABSTRACT: The Rosetta spacecraft flew by its second asteroid target (21) Lutetia on 10th July 2010. The flyby and recording of the radio carrier signals went very well. The frequency noise recorded at NASA's DSS63 70m antenna near Madrid was lower than expected. The asteroid perturbed the flyby trajectory and velocity of the spacecraft (closest approach was at 3160 km). The mass of the asteroid was determined from the Doppler shift of the radio signal carrier frequencies. A preliminary analysis of the flyby data and the housekeeping data show contributions from the rotation of the spacecraft body during flyby which still need to be corrected (The abstract is written one week after data reception at the institute). Preflyby simulations showed that a mass determination of the asteroid to an accuracy of 1% or better shall be possible even tough the flyby geometry was suboptimal and there was a tracking gap at closest approach. The bulk density will be derived from the determined mass and the volume. Volume estimates from the OSIRIS camera and from ground observations will be applied. Knowledge of the mass and bulk density is an important contributor to understand the asteroid's composition, internal structure and porosity and may probably also give clues for the definition of the asteroid's type. Lutetia is considered to be a major perturber of a number of smaller asteroids. The derived mass from the flyby will therefore be compared with those mass values derived from asteroid orbit perturbations.  [Show abstract] [Hide abstract]
ABSTRACT: The interior structures of Uranus and Neptune are not well constrained. We present 'empirical' models (pressure vs. density) of Uranus and Neptune interiors constrained by the gravitational coefficients J2, J4, and the planetary radii and masses, using Voyager's solidbody rotation periods. The empirical pressuredensity profiles are then interpreted in terms of physical equations of state of hydrogen, helium, ice (H2O), and rock (SiO2) to test the physical plausibility of the models. The interiors of Uranus and Neptune are found to be very similar. Our analysis suggests that the concentration of heavier elements inside both Uranus and Neptune interiors could increase gradually towards the planetary centers, without having sharp compositional transitions as typically assumed. Uranus and Neptune (solidbody) rotation periods, 17.24h and 16.11h, respectively, are based on Voyager 2 measurements of variations in the planets' radio signals and on fits to the planets' magnetic fields. The realization that Saturn's radio period does not represent the planet's deep interior rotation and the complexity of the magnetic fields of Uranus and Neptune raise the possibility that the Voyager 2 radio and magnetic periods might not represent the deep interior rotation periods of the planets. We use wind and shape data to investigate the rotation of Uranus and Neptune. Minimization of wind velocities or dynamic heights of the 1 bar isosurfaces, constrained by the single occultation radii and gravitational coefficients of the planets, leads to solidbody rotation periods of 16.58h for Uranus and 17.46h for Neptune. We derive shapes for the planets based on these rotation rates. Wind velocities with respect to these rotation periods are essentially identical on Uranus and Neptune and wind speeds are slower than previously thought. Alternatively, if we interpret wind measurements in terms of differential rotation on cylinders there are essentially no residual atmospheric winds.  [Show abstract] [Hide abstract]
ABSTRACT: To a first approximation, most planetary objects consist of a dense core region surrounded by a lowdensity envelope. The flattening of the coreenvelope interface and the surface can reveal important information about internal structure and rotation. The flattening of the internal interface is also important for constraining the dynamics of motions in a liquid core. We determine the flattening of the coreenvelope boundary and the surface for constant density layers. The flattening is calculated in two ways. One approach makes use of an exact semianalytical solution. A second approach is based on the theory of figures valid to third order in the standard smallness parameter. We evaluate the accuracy of the approximate theory of figure solutions by comparing these solutions for first, second, and third order in the smallness parameter with the exact solution. We find that the flattening at the coreenvelope interface can be significantly different from that at the planetary surface.  [Show abstract] [Hide abstract]
ABSTRACT: The Rosetta spacecraft will fly by its second target asteroid (21) Lutetia on 10 July 2010. Simulations based on the currently known size of Lutetia and assumptions on the bulk density show that tracking of two radiocarrier frequencies at Xband (8.4 GHz) and Sband (2.3 GHz) during the flyby will determine the mass at less than 1% accuracy. Derivation of the asteroid volume by camera observation will drive the uncertainty in derivation of the bulk density. Mass and bulk density provide valuable clues that might help resolve the difficulties in determining the taxonomic class of the asteroid.  [Show abstract] [Hide abstract]
ABSTRACT: The constraints on giant planet interior models with density discontinuities, for example, a coreenvelope boundary, are more difficult to treat than a continuous density distribution that decreases monotonically and continuously from the center to the surface of the planet. We revise our previous interior calculations (Anderson, J. D., and G. Schubert, Saturn's gravitational field, internal rotation, and interior structure, 2007, Science, 317, 13841387, doi: 101126/science.1144835, 2007), which solved a system of integrodifferential equations to third order in the smallness parameter omega2a3/GM (omega is the angular velocity of the planet, a is the planet's equatorial radius, G is the gravitational constant, and M is the planet's mass), and introduce Clairaut's differential equation for the flattening f, with appropriate boundary conditions at the planet's surface and at its center. The calculations can be carried to second order in the smallness parameter by solving Darwin's differential equation for k, a parameter that describes a secondorder deviation from sphericity. In principle, the calculations can be extended to differential equations of arbitrary order in smallness. As with our earlier method, we apply this revised method to the outer planets with interiors comprising a compressible core, obeying a linear density distribution, and an envelope in which density vs. radius is described by a sixth degree polynomial. This method of gravity sounding, with cores and envelope polynomial density distributions, can yield insights into a class of possible cores that fit the boundary conditions, consisting of the measured even zonal gravitational harmonics, plus the measured size and total mass of the planet. We apply the method to the four outer planets.  [Show abstract] [Hide abstract]
ABSTRACT: The four giant planets, Jupiter, Saturn, Uranus, and Neptune have strong zonal winds with velocities up to a few hundred meters per second. These zonal wind velocities, however, are based on assumed values of the solidbody rotation periods of the planets. Jupiter's kilometric radiation period of 9h 55m 29s has not changed in many decades, the 10h 39m 22s rotation period of Saturn, however, which derives from the Voyager era periodicity in Saturn's kilometric radiation (SKR), is now known to be variable and Saturn's rotation rate is therefore uncertain. Accordingly, the atmospheric zonal wind velocities with respect to the underlying rotating planet are unknown for Saturn. Uranus and Neptune rotation periods were derived from Voyager 2 radio astronomy observations to be 17h 14m 24s and 16h 06m 36s, respectively. Since we now realize that the kilometric radiation period might not represent the planet's deep interior rotation, we must consider the possibility that the Voyager 2 radio periodicities also do not represent the deep interior rotation of Uranus and Neptune. We use wind and shape data to investigate the rotation periods of Jupiter, Saturn, Uranus and Neptune. We show that Jupiter's and Saturn's shapes are consistent with solidbody rotation periods of 9h 55m and 10h 32m, respectively. We suggest that zonal winds have a minor effect on the planetary shape for both Jupiter and Saturn. Uranus and Neptune shapes (oblateness) are found to be inconsistent with Voyager's solidbody rotation periods. We address the possibility of deep differential rotation on cylinders.  [Show abstract] [Hide abstract]
ABSTRACT: It has been generally believed that a rotation period could be assigned to each of the giant planets. Accepted values of these periods, till now, are 9h 55m 29s, 10h 39m 22s, 17h 14m 24s, and 16h 06m 36s for Jupiter, Saturn, Uranus, and Neptune, respectively. The rotation period of Jupiter is based on the periodic variations in the planet's kilometric radiation and magnetic field, periodicities that have been unchanged since the Voyager flybys. The association of these periodicities with Jupiter's internal rotation period is based on the idea that the radio and magnetic phenomena are tied to the planet's magnetic field lines anchored deep within Jupiter. The periodic variations of the Saturnian Kilometric Radiation (SKR), unlike those of Jupiter, have not been rock solid, however; the periodicity has changed from 10h 39m 22s at the time of Voyager to 10h 45m 45s at the time of Cassini. Clearly, the SKR period does not represent the internal rotation period of Saturn, and it raises the possibility that the rotation periods of the other giant planets are uncertain. In fact, we must seriously reconsider whether the interiors of the giant planets are in solid body rotation with a single period. Even for Jupiter, the 9h 55m 29s rotation period might represent only the rotation of the region in which the magnetic field is generated. The dynamo region could extend from some unknown inner radius out to about 0.9 Jovian radius. The deeper Jovian interior could be rotating with a different period. A recent attempt to model the interior of Jupiter with new equation of state data concluded that the gravitational coefficients of Jupiter could not be fit unless Jupiter's internal rotation rate was constant on cylinders parallel to the rotation axis (Militzer, B., W.B. Hubbard, J. Vorberger, I. Tamblyn, and S.A. Bonev, A massive core in Jupiter predicted from firstprinciples simulations, 2008, ApJ, 688, L45L48 [doi: 10.1086/594364]). For Saturn, two studies of the atmospheric motions (Anderson, J.D. and G. Schubert, 2007, Saturn's gravitational field, internal rotation, and interior structure, Science, 317, 13841387 [doi: 10.1126/science.1144835]; Read, P.L., T.E. Dowling, and G. Schubert, Saturn's rotation period from its atmospheric planetarywave configuration, 2009, Nature, 460, 608610 [doi:10.1038/nature08194 Letter]) have inferred planetary rotation periods significantly shorter than the Voyager period, implying Jovianlike atmospheric winds. The inferred shapes (oblateness) of Uranus and Neptune are inconsistent with heretofore accepted planetary rotation rates. Either the shapes or the rotation periods of the icy giants are not well determined. If the magnetic fields of Uranus and Neptune are generated in relatively thin shells (Stanley, S., and J. Bloxham, Convectiveregion geometry as the cause of Uranus' and Neptune's unusual magnetic fields, Nature, 428, 151153 [doi:10.1038/nature02376] Letter), then the periodicities of the fields might not reflect the rotation of the bulk of the planets.  [Show abstract] [Hide abstract]
ABSTRACT: We summarise the scientific and technological aspects of the SAGAS (Search for Anomalous Gravitation using Atomic Sensors) project, submitted to ESA in June 2007 in response to the Cosmic Vision 20152025 call for proposals. The proposed mission aims at flying highly sensitive atomic sensors (optical clock, cold atom accelerometer, optical link) on a Solar System escape trajectory in the 2020 to 2030 timeframe. SAGAS has numerous science objectives in fundamental physics and Solar System science, for example numerous tests of general relativity and the exploration of the Kuiper belt. The combination of highly sensitive atomic sensors and of the laser link well adapted for large distances will allow measurements with unprecedented accuracy and on scales never reached before. We present the proposed mission in some detail, with particular emphasis on the science goals and associated measurements.  [Show abstract] [Hide abstract]
ABSTRACT: In response to ESA´s Call for proposalsof 5 March 2007 of the COSMIC VISION 20152025 plan of the ESA science programme, we propose a Mclass satellite mission to test the Equivalence Principle in the quantum domain by investigating the extend free fall of matter waves instead of macroscopic bodies as in the case of GAUGE, MICROSCOPE or STEP. The satellite, called Matter Wave Explorer of Gravity, will carry an experiment to test gravity, namely the measurement of the equal rate of free fall with various isotopes of distinct atomic species with precision cold atom interferometry in the vicinity of the earth. This will allow for a first quantum test of the Equivalence with spin polarized particles and with pure fermionic and bosonic atomic ensembles. Due to teh space conditions, the free fall of Rubidium and Potassium isotopes will be compared with a maximum accelerational sensitivity of 5 x 10^16 m/s^2 corresponding to an accuracy of the test of the Equivalence Principle of 1 part in 10^16. Besides the primary scientific goal, the quantum test of the Equivalence Principle, the mission can be extended to provide additional information about the gravitational field of the earth or for testing theories of fundamental processes of decoherence which are investigated by various theory groups in the context of quantum gravity phenomenology. In this proposal we present in detail the mission objectives and the technical aspects of the proposed mission. 
Article: Odyssey: a Solar System Mission
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ABSTRACT: The Solar System Odyssey mission uses modernday highprecision experimental techniques to test some the laws questions of fundamental physics which determine dynamics in the solar system. It could lead to a major discoveries by using demonstrated technologies and could be flown within the Cosmic Vision time frame. The mission proposes to perform a set of precision gravitation experiments from the vicinity of Earth to the outer. Its scientific objectives can be summarized as follows: (1) test of gravity force law in the Solar System up to and beyond the orbit Saturn; (2) precise investigation of navigation anomalies at the flybys, (3) measurement of Eddington´s parameter at occultation, (4) mapping of gravity field in the outer solar system and study of the Kuiper belt. To aim this, the Odyssey mission is built up on a main spacecraft, designed to fly up to 13 AU, with the following components: (a) a high precision accelerometer, with biasrejection system, measuring the deviation of the trajectory from the geodesics, that is also giving gravitational forces; (b) Kaband transponders, as for Cassini, for a precise range and Doppler measurement up to 13 AU, with additional VLBI equipment; (c) optional laser equipment, which would allow one to improve the range and Doppler measurement, resulting in particular in an improved measurement (with respect to Cassini) of the Eddington´s parameter. In this baseline concept, the main spacecraft is designed to operate beyond the Saturn orbit, up to 13 AU. It experiences multiple planetary flybys at Earth, Mars, or Venus, and Jupiter. The cruise and flyby phases allow the mission to schieve its baseline scientific objectives [(1) to (3) in the above list]. In addition to this baseline concept, the Odyssey mission proposes the release of the Enigma radiobeacon at Saturn, allowing one to extend the deep space gravity test up to at least 50 AU, while achieving the scientific objective of a mapping of gravity field in the outer Solar System [(4) in the above list].  [Show abstract] [Hide abstract]
ABSTRACT: Anderson and Schubert (2007, Science, 317, 1384) proposed that Saturn's rotation period might be ascertained by minimizing the dynamic heights of the 100 mbar isosurface with respect to the geoid; they derived a rotation period of 10h 32m 35s. We investigate the same approach for Jupiter to see if the Jovian rotation period is predicted by minimizing the dynamical heights of its isobaric (1 bar pressure level) surface. The shape of the Jovian pressure isosurface is derived from zonal wind data (GarcíaMelendo and SanchezLavega, 2001, Icarus, 316) and the Jovian geoid. Then, by regarding the Jovian geoid as undetermined in terms of Jupiter's rotation rate, we vary the rotation rate and the geoid and search for the geoid that minimizes the dynamical heights of the pressure isosurface in an rms sense. A rotation period of 9h 54m 29.7s is found to minimize the dynamical heights of the pressure isosurface. This rotation period is only one minute shorter than the measured period of Jupiter. The successful application of the method to Jupiter lends support to its relevance for Saturn. Application of the approach to Neptune and Uranus will also be discussed.
Publication Stats
4k  Citations  
996.28  Total Impact Points  
Top Journals
 Science (17)
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Institutions

2011

NASA
Вашингтон, West Virginia, United States


19682011

California Institute of Technology
 Jet Propulsion Laboratory
Pasadena, California, United States


19982004

University of California, Los Angeles
 • Department of Earth and Space Sciences (ESS)
 • Institute of Geophysics and Planetary Physics
Los Ángeles, California, United States


2002

Los Alamos National Laboratory
 Theoretical Division
Los Alamos, California, United States 
Cornell University
 Center for Radiophysics and Space Research (CRSR)
Итак, New York, United States


19861988

Stanford University
 Department of Electrical Engineering
Stanford, California, United States


1974

Pasadena City College
Pasadena, Texas, United States


1970

Massachusetts Institute of Technology
Cambridge, Massachusetts, United States
