1997
DOI: 10.1029/96je03642
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Martian precession and rotation from Viking lander range data

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Cited by 117 publications
(87 citation statements)
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References 45 publications
(18 reference statements)
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“…2). The statistically significant shift from the previous result is thought to be due to systematic effects in the ranging data that were used exclusively in the previous analysis (1), whereas our seasonal estimates are dominated by the Viking Doppler data. The estimated semiannual term does not agree as well with the model (Fig.…”
contrasting
confidence: 42%
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“…2). The statistically significant shift from the previous result is thought to be due to systematic effects in the ranging data that were used exclusively in the previous analysis (1), whereas our seasonal estimates are dominated by the Viking Doppler data. The estimated semiannual term does not agree as well with the model (Fig.…”
contrasting
confidence: 42%
“…Determination of the polar moment of inertia yields information on the distribution of mass within the planet, such as whether the planet has a dense core surrounded by a lighter mantle. Analysis of radio tracking measurements from the Viking landers has determined the normalized polar moment of inertia C/MR 2 , where M is the mass of Mars and R is its mean radius, to be 0.355 Ϯ 0.015 (1). However, the uncertainty in this estimate is not small enough to determine with certainty that Mars has a dense core or to distinguish between interior models ranging from an Earth-like composition to iron-enriched compositions characteristic of the meteorites thought to originate from Mars (2).…”
mentioning
confidence: 99%
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“…The parameters of rotation of Mars and their accuracies were found to be close to the corresponding values taken from a paper by Yoder and Standish (1997).…”
Section: The Use Of the Epm Ephemerides In Scientific Researchmentioning
confidence: 56%
“…Pathfinder has provided tests of the validity of remote observations from Earth, orbit, and the surface (2). As predicted, the average elevation of the center of the site was about the same as that of the Viking 1 lander (VL-1) relative to the 6.1-mbar geoid (Table 2), based on delayDoppler radar measurements (17) and tracking results (18); the Doppler tracking and two-way ranging estimate for the elevation of the spacecraft (9) is only 45 m lower than that of the VL-1 and within 100 m of that expected, which is within the uncertainties of the measurements. After landing, surface pressures and winds (5 to 10 m/s) were similar to expectations based on Viking data, although temperatures were about 10 K warmer (6).…”
mentioning
confidence: 75%