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

The 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...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: de Baca, Richard C., Juarez, Alfredo, Peralta, Stephen, Tylka, Jonathan, Rhodes, Richard
Format: Tagungsbericht
Sprache:eng
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue
container_start_page
container_title
container_volume
creator de Baca, Richard C.
Juarez, Alfredo
Peralta, Stephen
Tylka, Jonathan
Rhodes, Richard
description The 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.
format Conference Proceeding
fullrecord <record><control><sourceid>nasa_CYI</sourceid><recordid>TN_cdi_nasa_ntrs_20170009435</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>20170009435</sourcerecordid><originalsourceid>FETCH-nasa_ntrs_201700094353</originalsourceid><addsrcrecordid>eNrjZPB2S8zMKS1KVQjOzC3NSSzJzM9TCEktLsnMS1fIT1MoyUhViNI1VAguSExOLS7NLFEIySxJzMsszVVwSk0sAqlyLC5OzU3KyUwt5mFgTUvMKU7lhdLcDDJuriHOHrp5icWJ8XklRcXxRgaG5gYGBpYmxqbGBKQBzx4wkw</addsrcrecordid><sourcetype>Publisher</sourcetype><iscdi>true</iscdi><recordtype>conference_proceeding</recordtype></control><display><type>conference_proceeding</type><title>Failure Simulation Testing of the Z-1 Spacesuit Titanium Bearing Assemblies</title><source>NASA Technical Reports Server</source><creator>de Baca, Richard C. ; Juarez, Alfredo ; Peralta, Stephen ; Tylka, Jonathan ; Rhodes, Richard</creator><creatorcontrib>de Baca, Richard C. ; Juarez, Alfredo ; Peralta, Stephen ; Tylka, Jonathan ; Rhodes, Richard</creatorcontrib><description>The 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.</description><language>eng</language><publisher>Johnson Space Center</publisher><subject>Man/System Technology And Life Support ; Mechanical Engineering ; Metals And Metallic Materials</subject><creationdate>2016</creationdate><rights>Copyright Determination: PUBLIC_USE_PERMITTED</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>309,780,800</link.rule.ids><linktorsrc>$$Uhttps://ntrs.nasa.gov/citations/20170009435$$EView_record_in_NASA$$FView_record_in_$$GNASA$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>de Baca, Richard C.</creatorcontrib><creatorcontrib>Juarez, Alfredo</creatorcontrib><creatorcontrib>Peralta, Stephen</creatorcontrib><creatorcontrib>Tylka, Jonathan</creatorcontrib><creatorcontrib>Rhodes, Richard</creatorcontrib><title>Failure Simulation Testing of the Z-1 Spacesuit Titanium Bearing Assemblies</title><description>The 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.</description><subject>Man/System Technology And Life Support</subject><subject>Mechanical Engineering</subject><subject>Metals And Metallic Materials</subject><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2016</creationdate><recordtype>conference_proceeding</recordtype><sourceid>CYI</sourceid><recordid>eNrjZPB2S8zMKS1KVQjOzC3NSSzJzM9TCEktLsnMS1fIT1MoyUhViNI1VAguSExOLS7NLFEIySxJzMsszVVwSk0sAqlyLC5OzU3KyUwt5mFgTUvMKU7lhdLcDDJuriHOHrp5icWJ8XklRcXxRgaG5gYGBpYmxqbGBKQBzx4wkw</recordid><startdate>20160710</startdate><enddate>20160710</enddate><creator>de Baca, Richard C.</creator><creator>Juarez, Alfredo</creator><creator>Peralta, Stephen</creator><creator>Tylka, Jonathan</creator><creator>Rhodes, Richard</creator><scope>CYE</scope><scope>CYI</scope></search><sort><creationdate>20160710</creationdate><title>Failure Simulation Testing of the Z-1 Spacesuit Titanium Bearing Assemblies</title><author>de Baca, Richard C. ; Juarez, Alfredo ; Peralta, Stephen ; Tylka, Jonathan ; Rhodes, Richard</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-nasa_ntrs_201700094353</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2016</creationdate><topic>Man/System Technology And Life Support</topic><topic>Mechanical Engineering</topic><topic>Metals And Metallic Materials</topic><toplevel>online_resources</toplevel><creatorcontrib>de Baca, Richard C.</creatorcontrib><creatorcontrib>Juarez, Alfredo</creatorcontrib><creatorcontrib>Peralta, Stephen</creatorcontrib><creatorcontrib>Tylka, Jonathan</creatorcontrib><creatorcontrib>Rhodes, Richard</creatorcontrib><collection>NASA Scientific and Technical Information</collection><collection>NASA Technical Reports Server</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>de Baca, Richard C.</au><au>Juarez, Alfredo</au><au>Peralta, Stephen</au><au>Tylka, Jonathan</au><au>Rhodes, Richard</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Failure Simulation Testing of the Z-1 Spacesuit Titanium Bearing Assemblies</atitle><date>2016-07-10</date><risdate>2016</risdate><abstract>The 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.</abstract><cop>Johnson Space Center</cop><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng
recordid cdi_nasa_ntrs_20170009435
source NASA Technical Reports Server
subjects Man/System Technology And Life Support
Mechanical Engineering
Metals And Metallic Materials
title Failure Simulation Testing of the Z-1 Spacesuit Titanium Bearing Assemblies
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-08T21%3A01%3A42IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-nasa_CYI&rft_val_fmt=info:ofi/fmt:kev:mtx:book&rft.genre=proceeding&rft.atitle=Failure%20Simulation%20Testing%20of%20the%20Z-1%20Spacesuit%20Titanium%20Bearing%20Assemblies&rft.au=de%20Baca,%20Richard%20C.&rft.date=2016-07-10&rft_id=info:doi/&rft_dat=%3Cnasa_CYI%3E20170009435%3C/nasa_CYI%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true