1976
DOI: 10.1175/1520-0477(1976)057<1094:amomtv>2.0.co;2
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Atmopspheric Measurements on Mars: the Viking Meteorology Experiment

Abstract: The Viking Meteorology Experiment is one of nine experiments to be carried out on the surface of Mars by each of two Viking Landers positioned at different latitudes and longitudes in the Northern Hemisphere. The meteorology experiment will measure pressure, temperature, wind speed, and wind direction at 1J h intervals throughout the Martian day. The duration of each measurement period, the interval between data samples for a measurement period, and the time at which the measurement period is started will be v… Show more

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Cited by 83 publications
(47 citation statements)
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“…After several failures, the first successful meteorological observations from the Martian surface were made in 1976 by the two Viking landers (Chamberlain et al 1976;Hess et al 1977;Tillman et al 1994). The main goals of these meteorological observations were to study meso-scale and planetary-scale systems and processes, to investigate boundary layer phenomena and to obtain a better understanding of the Earth's atmosphere through comparison with that of Mars.…”
Section: Viking Lander Missionsmentioning
confidence: 99%
“…After several failures, the first successful meteorological observations from the Martian surface were made in 1976 by the two Viking landers (Chamberlain et al 1976;Hess et al 1977;Tillman et al 1994). The main goals of these meteorological observations were to study meso-scale and planetary-scale systems and processes, to investigate boundary layer phenomena and to obtain a better understanding of the Earth's atmosphere through comparison with that of Mars.…”
Section: Viking Lander Missionsmentioning
confidence: 99%
“…There was one fortunate aspect in the new and old seasons-the expected surface pressure was almost identical. Evaluation of VL lander surface pressure data (Chamberlain et al 1976) and MSL REMS surface pressure data (Gomez-Elvira et al 2012) for the two seasons at the landing local time indicated that the pressure at L s = 295…”
Section: Atmosphere Definitionmentioning
confidence: 99%
“…Since exact power levels are difficult to predict, the power required from the MTV is set at twice that ex-pected. Survival power levels are estimated as 250 watts per satellite 22 which makes a total of 500 watts of electrical power required by each satellite while attached to the MTV. Minimum telemetry will be available.…”
Section: Mission Platform Designmentioning
confidence: 99%
“…The values shown in Table 13 are representative of the calculated AVs and mission durations associated with the conjunction class missions. 22 These class of scenarios represent Hohmann transfer trajectories and therefore have the smallest overall AV magnitudes. However, due to the lower AV totals, the mission durations are longer than any other scenario.…”
Section: State Transition Matrix Computation(93:106-117)mentioning
confidence: 99%