2014
DOI: 10.1007/s11214-014-0095-x
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Application of MAVEN Accelerometer and Attitude Control Data to Mars Atmospheric Characterization

Abstract: The structure of the upper atmosphere of Mars (above ∼100 km) has been probed in situ mainly using spacecraft accelerometers during the aerobraking phases of 3 Mars orbiters. In a similar manner, the Mars Atmosphere and Volatile Evolution (MAVEN) Accelerometer Experiment (ACC) will also use atmospheric drag accelerations sensed by inertial measurement units (IMU) onboard the spacecraft to recover atmospheric density along the orbiter path. These densities are used to estimate hydrostatic 'vertical' density and… Show more

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Cited by 27 publications
(25 citation statements)
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“…Densities calculated for orbits beyond 748 are divided by a factor of 1.5331 to account for an observed change in the sensitivity of the instrument following DD1 due to detector gain stabilization after exposure to high atmospheric densities encountered during the DD (Benna & Elrod, ). This sensitivity change was discovered during a comparison of NGIMS densities with atmospheric densities derived from data obtained by the MAVEN Accelerometer Experiment (ACC; see Zurek et al, ). The change in sensitivity does not affect derived temperatures since it only alters the magnitude of a density profile, not the slope.…”
Section: Methodsmentioning
confidence: 93%
“…Densities calculated for orbits beyond 748 are divided by a factor of 1.5331 to account for an observed change in the sensitivity of the instrument following DD1 due to detector gain stabilization after exposure to high atmospheric densities encountered during the DD (Benna & Elrod, ). This sensitivity change was discovered during a comparison of NGIMS densities with atmospheric densities derived from data obtained by the MAVEN Accelerometer Experiment (ACC; see Zurek et al, ). The change in sensitivity does not affect derived temperatures since it only alters the magnitude of a density profile, not the slope.…”
Section: Methodsmentioning
confidence: 93%
“…An in-depth review of MAVEN and its mission is provided by Jakosky et al (2015). During the nominal science orbit, when periapsis altitude is near 160 km, the onboard accelerometer provides a data source for determining atmospheric density (Zurek et al, 2015). The ability to recover density depends strongly on orbit and spacecraft conditions.…”
Section: Datamentioning
confidence: 99%
“…MAVEN includes three instruments that are designed to characterize thermospheric density: The Accelerometer (ACC; Zurek et al, 2015), the Neutral Gas and Ion Mass Spectrometer (NGIMS; Mahaffy, Benna, King, et al, 2015), and the Imaging Ultraviolet Spectrograph (IUVS; McClintock et al, 2015). ACC and NGIMS make routine in situ density measurements near periapsis, with typical reliable measurement sensitivity between 145 and 250 km for NGIMS and between 145 and 170 km for ACC.…”
Section: Introductionmentioning
confidence: 99%