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Volumn 271, Issue 5246, 1996, Pages 184-188

The shape of mars and the topographic signature of the hemispheric dichotomy

Author keywords

[No Author keywords available]

Indexed keywords

ELLIPSE; ELLIPSOID; HEMISPHERIC DICHOTOMY; MARINER 9; PLANET SHAPE; PLANETARY SHAPE; TOPOGRAPHIC SIGNATURE; VIKING ORBITER;

EID: 0029730547     PISSN: 00368075     EISSN: None     Source Type: Journal    
DOI: 10.1126/science.271.5246.184     Document Type: Article
Times cited : (71)

References (62)
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    • The principal sources of error in the occultation data include the spacecraft position at the kilometer level (22), the timing of the loss of signal at the 0.1-s level (corresponding to a distance of ∼1 km), and the location of the grazing ray at the time of occultation (due to ephemeris errors, geodetic positioning uncertainties, and local topography) (19). Depending on the orbital radius of the spacecraft at the time of occultation, the geometry of the spacecraft and planet, and the topography of the limb, these errors have amounted to several kilometers in planetary radii (19-22).
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    • Determination of a planetary radius from occultation data requires precise knowledge of the spacecraft orbit. The uncertainty in the spacecraft orbit is frequently the largest source of error in the calculated radius. The original orbits for the Mariner 9 and Viking occultation measurements had radial accuracies of 1 to 3 km. To improve the estimation of the martian gravity field (28), we recalculated nearly all of the orbits for the Mariner 9 and Viking Orbiters. We used the GEODYN/SOLVE system of orbital analysis programs, which numerically integrate the spacecraft Cartesian state and force model partial derivatives by using a high-order predictor-corrector model The force modeling includes a spherical harmonic representation of the planet's gravity field, as well as point mass representations for the sun, Earth, and other planets. Solar radiation pressure, atmospheric drag on the spacecraft, tidal parameters, planetary rotation measurement and timing biases, and tracking station coordinates are estimated along with spacecraft orbits This analysis made use of improved planetary ephemerides (DE234), reference models (J2000), and parameters of the planetary coordinate system. We have improved the radial accuracy of spacecraft orbits with respect to Mars's COM by approximately an order of magnitude, from ≥ 1 km to ∼100 to 300 m (28)
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    • Planetary ephemens errors resulted in incorrect placement of the planet (by kilometers) at the time of the occultation (circa 1971), although the spacecraft position is with respect to the planet, and to first order the errors cancel, some small fraction of the error remains. Also, knowledge of the rotation of Mars has improved since the 1970s (40), and thus the position of the occultation point can be improved, principally in longitude, to ∼500 m.
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    • -3/2,whereP and Tare atmospheric pressure and temperature, respectively This expression (provided by D Hinson) assumes a constant atmospheric temperature and is estimated to be valid to ∼10% for small refraction angles The largest refraction corrections occurred at high latitudes, where the spacecraft were typically more distant from Mars. Refraction corrections to the radius were typically on the order of 1 to 2 km, but the largest was 12 km. The single largest source of error is the orbit at ∼400 m; the next largest is atmospheric refraction at ∼300 m, followed by occultation timing and planetary ephemens errors. The total root sum square error of a typical occultation is estimated to be a little over 500 m. The error model tor the atmospheric refraction was ∼10% of the total correction.
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    • We thank S Asmar and M Connolly for "rediscovering" the Viking occultation data in an unmarked file cabinet at the Jet Propulsion Laboratory, G Lindal for providing the refraction angles used to correct the Viking data D Hinson for helpful discussions regarding atmospheric corrections to the occultation data, D. Rowlands for software support in the processing of occultations, S Fncke for orbital computations, J Finnochiaro for assistance with atmospheric refraction corrections, R Jurgens and M Slade for radar data, F. Lemoine for assembling geord values used to determine geopotential topography, G Neumann for assistance with Fig. 1, S Solomon for discussions about interpretation of the results, and N Sleep and an anonymous referee for helpful reviews. The Mariner 9 data (A Kliore, principal investigator) were obtained from the National Space Science Data Center at the Goddard Space Flight Center Supported by the NASA Planetary Geology and Geophysics Program and the NASA Mars Global Surveyor Project.


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