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Micromechanisms for Optimism SeismometerWithin the framework of the Mars 94 mission, it was decided to design and build a new vertical axis seismometer in order to continuously record the seismic events occurring on the Mars planet. The mission requirements lead to very stringent constraints on power, volume, mass and shock resistance at the landing. The seismometer must be capable of automatic leveling and automatic fitting to the local gravity. This paper deals with the mechanisms designed for this seismometer. Due to the short allotted time for its development and low cost, the baseline was to apply the rules of spatial tribology and, when it was possible, to customize existing components for space applications.
Document ID
19950020872
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Nicolas Paulin
(Societe Anonyme d'Etudes et Realisations Nucleaires Limeil-Brevannes, France)
Pierre Dumas
(Societe Anonyme d'Etudes et Realisations Nucleaires Limeil-Brevannes, France)
Marc Pochard
(Societe Anonyme d'Etudes et Realisations Nucleaires Limeil-Brevannes, France)
Date Acquired
September 6, 2013
Publication Date
May 1, 1995
Publication Information
Publication: 29th Aerospace Mechanisms Symposium
Publisher: National Aeronautics and Space Administration
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-CP-3293
Meeting Information
Meeting: 29th Aerospace Mechanisms Symposium
Location: League City, TX
Country: US
Start Date: May 17, 1995
End Date: May 19, 1995
Sponsors: Lockheed Missiles and Space Company (United States), National Aeronautics and Space Administration
Accession Number
95N27292
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
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