JPL Technical Report Server

Life test failure of harmonic gears in a Two-axis Gimbal for the Mars Reconnaissance Orbiter Spacecraft

Show simple item record

dc.contributor.author Johnson, Michael R.
dc.contributor.author Gehling, Russ
dc.contributor.author Head, Ray
dc.date.accessioned 2006-06-12T23:10:54Z
dc.date.available 2006-06-12T23:10:54Z
dc.date.issued 2006-05-17
dc.identifier.citation Aerospace Mechanisms Symposium, Langley Research Center, Hampton, Virginia, May 17-19, 2006. en
dc.identifier.clearanceno 06-0231
dc.identifier.uri http://hdl.handle.net/2014/39336
dc.description.abstract This paper will present a process for increasing the stiffness of harmonic gear assemblies and recommend a maximum stiffness point that, if exceeded, compromises the reliability of the gear components for long life applications. en
dc.description.sponsorship NASA/JPL en
dc.format.extent 712964 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US en
dc.publisher Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2006. en
dc.subject galling en
dc.subject harmonic gears en
dc.subject Life Test Failure en
dc.subject Mars Reconnaissance Orbiter (MRO) en
dc.subject increased stiffness en
dc.title Life test failure of harmonic gears in a Two-axis Gimbal for the Mars Reconnaissance Orbiter Spacecraft en
dc.type Preprint en


Files in this item

This item appears in the following Collection(s)

Show simple item record

Search


Browse

My Account