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Atmospheric Structure Investigation Accelerometers

NSSDCA ID: 2005-029A-08

Mission Name: Mars Reconnaissance Orbiter
Principal Investigator:Dr. Gerald M. Keating

Description

The Atmospheric Structure Investigation Accelerometers are engineering accelerometers mounted on the Mars Reconnaissance Orbiter. During aerobraking, these accelerometers will record the drag on the spacecraft, giving information on the density at the spacecraft altitude. This will provide information on the structure of the upper atmosphere and coupling between the upper and lower atmosphere.

Alternate Names

  • MarsReconnaissanceOrbiter/AtmosphericStructureInvestigationAccelerometers
  • urn:nasa:pds:context:instrument:accel.mro

Funding Agency

  • NASA-Office of Space Science Applications (United States)

Discipline

  • Planetary Science: Atmospheres

Additional Information

Questions and comments about this experiment can be directed to: Dr. David R. Williams

 

Personnel

NameRoleOriginal AffiliationE-mail
Dr. Gerald M. KeatingTeam LeaderNASA Langley Research Center
Dr. Stephen W. BougherTeam MemberUniversity of Michiganbougher@umich.edu

Selected References

  • Tolson, R., et al., Atmospheric Modeling Using Accelerometer Data During Mars Reconnaissance Orbiter Aerobraking Operations, J. Spacecr. Rockets, 42, No. 3, 511-518, doi:10.2514/1.34301, May 2008.
  • Bougher, S. W., et al., Prediction of the structure of the Martian upper atmosphere for the Mars Reconnaissance Orbiter (MRO) mission, Mars, 2, 10-20, doi:10.1555/mars.2006.0002, 2006.
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