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4243166871
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note
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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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4243081991
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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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40
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J. Lorell et al., Icarus 18, 304 (1973).
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The Viking lenders contained atmospheric pressure sensors that have also been used to calculate relative surface elevation These sensors measured pressure directly, so the Viking sites have the best-determined relative elevations on Mars. However, these measurements were not included in the USGS DEM. A comparison of the relative heights of these sites shows them to disagree with the lander site elevations in the DEM by ∼2 km and to be in the incorrect relative direction with respect to each other (41). In our geopotential topography model, the relative elevations of the sites agree with relative heights derived from the tender pressure data to within 49 m, and they are in the correct direction with respect to each other.
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42
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4243125199
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Our best-fit ellipsoid is triaxial with semimajor axis A = 3399.472 km, intermediate semiaxis B = 3394.329 km, and semiminor axis C = 3376.502 km, with an inverse flattening (1/f) of 166.53. The offset of the COF from the COM is × = -130 m, y = -1780 m, and z = -3081 m. The A axis of our ellipsoid is 4.9 km greater than that of the USGS DEM, and the B and C axes are greater by 1.0 km and 200 m, respectively.
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43
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G. S Downs, R M. Goldstein, R. R. Green, G. A. Moms. P. E. Reichley, Icarus 18, 8 (1973); G. S. Downs, P. E. Reichtey, R. R. Green, ibid. 26, 273 (1975).
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The primary source of error for the radar data is the planetary ephemeris (42); this error, combined with a lesser error induced by solar plasma effects, indicates a vertical accuracy of ≃300 m for these measurements, which is comparable to that of the occultation data. However, the radar measurement is an average for an area of several square kilometers, whereas the occultation measurement is a point location. Thus, a systematic difference between the radii derived from the two data sets might be expected. In a comparison of the topography derived from the radar data with that derived from the occultation data, a systematic difference in radius was detected, with a mean of 730 ± 173 m; the radar-derived radii were smaller than the occultation radii. The sign of this difference is consistent with the radar data, providing a measure of the planetary radius to the floors of valleys, and with the occultation data, providing a measure of the planetary radius to the higher topographic locations, such as mountains.
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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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