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Failure Simulation Testing of the Z-1 Spacesuit Titanium Bearing AssembliesThe Z-2 is a candidate for 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 the NASA White Sands Test Facility (WSTF) perform a series failure simulation tests on three titanium bearing assemblies, an elemental part of the joint construction used in new spacesuit designs. This testing simulated two undetected failures within the bearings and as a result the objective of this test program was to evaluate whether a failed or failing bearing could result in ignition of the titanium race material due to friction. 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. To evaluate this risk, the bearings were cycled in a simulated worst-case scenario environment, with 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 detailed descriptions of the test hardware, methodology, and results.
Document ID
20170009435
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
de Baca, Richard C.
(NASA White Sands Test Facility NM, United States)
Juarez, Alfredo
(Jacobs Technology, Inc. Las Cruces, NM, United States)
Peralta, Stephen
(NASA White Sands Test Facility NM, United States)
Tylka, Jonathan
(NASA White Sands Test Facility NM, United States)
Rhodes, Richard
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
October 3, 2017
Publication Date
July 10, 2016
Subject Category
Mechanical Engineering
Metals And Metallic Materials
Man/System Technology And Life Support
Report/Patent Number
JSC-CN-36631
ICES-2016-298
Meeting Information
Meeting: International Conference on Environmental Systems
Location: Vienna
Country: Austria
Start Date: July 10, 2016
End Date: July 14, 2016
Sponsors: International Conference On Environmental Systems, Inc.
Distribution Limits
Public
Copyright
Public Use Permitted.
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