Failure Simulation Testing of the Z-1 Spacesuit Titanium Bearing Assemblies

dc.creatorPeralta, Stephen
dc.creatorJuarez, Alfredo
dc.creatorTylka, Jonathan
dc.creatorRhodes, Richard
dc.date.accessioned2016-07-28T19:19:46Z
dc.date.available2016-07-28T19:19:46Z
dc.date.issued2016-07-10
dc.descriptionUnited States
dc.descriptionNASA JSC / WSTF
dc.descriptionJacobs
dc.descriptionNASA
dc.description400
dc.descriptionICES400: Extravehicular Activity: Space Suits
dc.descriptionVienna, Austria
dc.descriptionRichard C de Baca, NASA Johnson Space Center White Sands Test Facility, USA
dc.descriptionAlfredo Juarez, NASA Johnson Space Center White Sands Test Facility, USA
dc.descriptionStephen Peralta, NASA Johnson Space Center White Sands Test Facility, USA
dc.descriptionJonathan Tylka, NASA Johnson Space Center White Sands Test Facility, USA
dc.descriptionRichard Rhodes, NASA Johnson Space Center, USA
dc.descriptionThe 46th International Conference on Environmental Systems was held in Vienna, Austria, USA on 10 July 2016 through 14 July 2016.
dc.description.abstractThe Z-1 is NASA's next generation spacesuit, designed for a range of possible missions with enhanced mobility for spacewalks both on planetary surfaces and in microgravity. Increased mobility was accomplished through innovations in shoulder and hip joints, using a number of new bearings to allow spacesuit wearers to dip, walk, and bend with ease; all important tasks for a planetary explorer collecting samples or traveling over rough terrain. The Advanced Spacesuit Development Team of NASA Johnson Space Center requested that NASA White Sands Test Facility (WSTF) perform a simulation test on three titanium bearing assemblies, an elemental part of the joint construction used in the Z-1 spacesuit. This testing simulated two undetected failures within the bearings. The first failure was an inner seal leak sufficient to pressurize the race with +99 percent oxygen. The second failure was an improperly installed or mismatched ball port that created a protrusion in the ball bearing race, partially obstructing the nominal rolling path of each ball bearing. When the spacesuit bearings are assembled, bearing balls are loaded into the assembly via a ball port. The ball port is specific and unique to each bearing assembly (matched pair). The simulated mismatched ball port is a significant source of friction, which would be caused by an assembly error. The objective of this test program was to evaluate whether a failed or failing bearing can result in ignition of the titanium race material due to friction. To evaluate this risk, the bearings were cycled in a simulated worst case scenario environment, operational loads, and potential flaw conditions. During test the amount of actuation torque required and heat generated through continuous operation were measured and the bearings were observed for sparks or burning events. This paper provides details descriptions of the test hardware, methodology, and results.
dc.format.mimetypeapplication/pdf
dc.identifier.otherICES_2016_298
dc.identifier.urihttp://hdl.handle.net/2346/67651
dc.language.isoeng
dc.publisher46th International Conference on Environmental Systems
dc.subjectSpacesuit
dc.subjectZ-1
dc.subjectTitanium
dc.subjectBearing
dc.titleFailure Simulation Testing of the Z-1 Spacesuit Titanium Bearing Assemblies
dc.typePresentation

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