{"id":41046,"date":"2009-07-18T18:10:42","date_gmt":"2009-07-18T10:10:42","guid":{"rendered":"https:\/\/wp-productionenv-bjg9h2g2bgg5b8aa.southeastasia-01.azurewebsites.net\/news\/sts-127-completes-eva-1-fuel-cell-issue-monitored-by-mmt\/"},"modified":"2009-07-18T18:10:42","modified_gmt":"2009-07-18T10:10:42","slug":"sts-127-completes-eva-1-fuel-cell-issue-monitored-by-mmt","status":"publish","type":"post","link":"https:\/\/starpath.global\/news\/sts-127-completes-eva-1-fuel-cell-issue-monitored-by-mmt\/","title":{"rendered":"STS-127 completes EVA-1 \u2013 Fuel Cell issue monitored by MMT"},"content":{"rendered":"<p>Endeavour\u2019s Dave Wolf and the ISS\u2019s Tim Kopra&nbsp;ventured outside the Shuttle\/Station complex on Saturday&nbsp;and completed the first of five EVAs (spacewalks) scheduled for the STS-127 mission.&nbsp; Meanwhile, the Mission Management Team (MMT) continues to monitor the Potassium Hydroxide (KOH) levels and operating temperature of Fuel Cell 3 on Endeavour as the docked portion of the Orbiter\u2019s mission begins.<\/p>\n<p>EVA-1:<\/p>\n<p>Wolf (EV-1) and Kopra (EV-2) were preparing the Japanese Exposed Facility (JEF) for unberth from Endeavour\u2019s Payload Bay and attachment to the Japanese Experiment Module (JEM) \u201cKibo.\u201d<\/p>\n<p>Following the planned order of EVA tasks, Wolf and Kopra, after egressing from the Station\u2019s Quest airlock, translated (moved) to the end of the JEM where they prepared the Active Berthing Mechanism for the installation of the JEF during the latter stages of the spacewalk.<\/p>\n<h4 class=\"widget-title penci-border-arrow\">See Also<\/h4>\n<ul>\n<li>LIVE STS-127 UPDATES<\/li>\n<li>L2 STS-127 Special Section<\/li>\n<li>Click here to Join L2<\/li>\n<\/ul>\n<p>During this procedure, Wolf and Kopra jettisoned the cover of the Active Berthing Mechanism into space.&nbsp; Pre-mission trajectory calculations indicate that the release of this cover (and five others throughout EVAs 1-3) will not violate the \u201c200m Keep-Out-Sphere\u201d around the Station as mandated by the ISS Jettison Policy.<\/p>\n<p>Furthermore, the jettison of these covers will not interfere or impinge upon Shuttle operations following Endeavour\u2019s undocking from the Station late in the mission (or earlier should contingency requirements mandate).<\/p>\n<p><img fetchpriority=\"high\" decoding=\"async\" class=\"alignleft size-full wp-image-10868\" title=\"C3\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2009\/07\/C3.jpg\" alt=\"C3\" width=\"294\" height=\"226\">Following the jettison of this Multilayer Insulation cover from Berthing Mechanism, Wolf and Kopra removed the grounding tab around the JEM Remote Manipulator System (RMS) before moving to Endeavour\u2019s Payload Bay to reconfigure the JEF and the LTA on the Integrated Cargo Carrier-Vertical Light-weight Deployable payload.<\/p>\n<p>After their work in Endeavour\u2019s Payload Bay was completed, Wolf and Kopra then relocated themselves to the Node-2 (Harmony) module of the ISS where they reconfigured a CBCS flap on the zenith side of the module.&nbsp; This&nbsp;was followed by a reconfiguration of a Crew and Equipment Translation Aid (CETA) cart on the truss of the Space Station.<\/p>\n<p>Spaceflight news subscription<path d=\"M7.59009 18.59L9.00009 20L17.0001 12L9.00009 4L7.59009 5.41L14.1701 12\" style=\"animation: initial !important; background: initial !important; border: 0px !important; box-shadow: none !important; color: inherit !important; cursor: inherit !important; direction: inherit !important; display: inline !important; fill: currentcolor !important; filter: initial !important; float: none !important; margin: 0px !important; opacity: initial !important; outline: 0px !important; overflow: initial !important; padding: 0px !important; stroke: initial !important; transform: initial !important; vertical-align: initial !important; visibility: inherit !important;\"><\/path>Technology News<path d=\"M7.59009 18.59L9.00009 20L17.0001 12L9.00009 4L7.59009 5.41L14.1701 12\" style=\"animation: initial !important; background: initial !important; border: 0px !important; box-shadow: none !important; color: inherit !important; cursor: inherit !important; direction: inherit !important; display: inline !important; fill: currentcolor !important; filter: initial !important; float: none !important; margin: 0px !important; opacity: initial !important; outline: 0px !important; overflow: initial !important; padding: 0px !important; stroke: initial !important; transform: initial !important; vertical-align: initial !important; visibility: inherit !important;\"><\/path>Aerospace &amp; Defense<path d=\"M7.59009 18.59L9.00009 20L17.0001 12L9.00009 4L7.59009 5.41L14.1701 12\" style=\"animation: initial !important; background: initial !important; border: 0px !important; box-shadow: none !important; color: inherit !important; cursor: inherit !important; direction: inherit !important; display: inline !important; fill: currentcolor !important; filter: initial !important; float: none !important; margin: 0px !important; opacity: initial !important; outline: 0px !important; overflow: initial !important; padding: 0px !important; stroke: initial !important; transform: initial !important; vertical-align: initial !important; visibility: inherit !important;\"><\/path>\n<p>     (adsbygoogle = window.adsbygoogle || []).push({});<\/p>\n<p>In the meantime, astronauts inside the ISS and Endeavour worked with the Space Station Remote Manipulator System (SSRMS) and the Shuttle Remote Manipulator System (SRMS) \u2013 more commonly known as the Station and Shuttle robot arms \u2013 to unberth the JEF from Endeavour\u2019s Payload Bay and install the facility onto the JEM.<\/p>\n<p>To accomplish this task, the SSRMS first grappled the JEF and pull it out of Endeavour\u2019s Payload Bay.&nbsp; Then, the JEF was handed off to the Shuttle RMS while the Station RMS was relocated to the Node-2 (Harmony) Mobile Base System.<\/p>\n<p>Following this relocation, the JEF was&nbsp;handed back to the Station RMS.&nbsp; Then, the robotics officer at the SSRMS working Station in the Destiny Science Lab of the ISS maneuvered the SSRMS with the JEF to the installation point on the JEM and gently guided the JEF to its permanent location on the exterior of the Station.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft size-full wp-image-10867\" title=\"C2\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2009\/07\/C2.jpg\" alt=\"C2\" width=\"278\" height=\"220\">After final alignments were&nbsp;confirmed, the JEF was then berthed to the JEM and docking latches secured to ensure a proper attachment of the JEF to the JEM.<\/p>\n<p>The list of&nbsp;get-ahead tasks for EVA-1 included: P3 truss Mobile Transporter stop stow, Ammonia Tank Assembly bolt release, Z1 truss tool box tool retrieval, Node-1 (Unity) Post CBCS flap reconfiguration, P3 truss Nadir UCCAS deployment, and\/or S3 Zenith Outboard Payload Attachment System deployment.<\/p>\n<p>The UCCAS (Unpressurized Cargo Carrier Attachment Systems) reconfiguring&nbsp;was a success, thanks to a special detent tool that designed for allowing the freeing of a hinge that had proved troublesome during STS-119.<\/p>\n<p>Finally, following the completion of EVA-1 and the ingress of Wolf and Kopra into the Quest airlock, the 2B power channel on the Port truss of the ISS will be deactivated in preparation for the P6 truss batteries removal and replacement activity later in the mission.<\/p>\n<p>Furthermore, as has been seen on the previous two Station missions, Endeavour\u2019s spacewalking astronauts used the new style gloves during all five EVAs, as outlined in the STS-127 Flight Readiness Review (FRR) EVA&nbsp;documentation, available on L2.<\/p>\n<p>These gloves were previously used on STS-126 in November 2008 and on STS-119 in March of this year with no issues discovered during post-flight inspections.<\/p>\n<p>The new gloves were introduced for all Station spacewalks following several instances of cut or damaged gloves on Shuttle\/Station missions in 2006 and 2007.<\/p>\n<p>Fuel Cell 3:<\/p>\n<p>As Endeavour\u2019s 23rd mission continues without any major issues, ground engineers have determined that the Orbiter\u2019s cryo margins for her Fuel Cells are 22-hours above the baselined 16+0+2 day mission without the use of SSPTS (Station to Shuttle Power Transfer System) and 44-hours above the 16+0+2 day baseline with the use of SSPTS.<\/p>\n<p>However, while any and all positive cryo margin is welcome, this is not the main area of concentration for the MMT (Mission Management Team) regarding Endeavour\u2019s Fuel Cells.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft size-full wp-image-10869\" title=\"C4\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2009\/07\/C4.jpg\" alt=\"C4\" width=\"309\" height=\"209\">In fact, the MMT is keeping a close eye on Fuel Cell-3 (FC-3) \u2013 specifically the KOH values in that Fuel Cell.<\/p>\n<p>According FD-2 (Flight Day 2) MMT briefing materials \u2013 available for download on L2 \u2013 \u201cPre-launch tests conducted to verify FC-3 KOH values remain within operation limits when FC-3 is loaded at an expected on-orbit SSPTS lower power level.\u201d<\/p>\n<p>These tests indicated that FC-3 could be operated at the lower power level without causing \u201ccell flooding.\u201d<\/p>\n<p>However, as Mike Moses, chairman of the pre-launch MMT at the Kennedy Space Center, explained during a pre-launch interview on Wednesday, \u201cAt the pad, water was cycled through the Fuel Cell to verify that we could transfer for drinking water.&nbsp; If we don\u2019t drain the water, it\u2019ll build up.&nbsp; Too much water would let the electrolyte compound (KOH) into Fuel Cell and end up drying out the Fuel Cell\u201d which would render it inoperative.<\/p>\n<p>Furthermore, Moses explained that \u201cWe can\u2019t monitor the exact KOH concentration on orbit, but we can on the ground.&nbsp; When we run the SSPTS system on orbit, it takes off a lot of the load from the Fuel Cells.&nbsp; That means we don\u2019t dry the fuel cells out enough and the temperatures in the Fuel Cells increase.<\/p>\n<p>\u201cIf we can\u2019t drain the Fuel Cells, then we can\u2019t take as much power from the SSPTS and we lose some mission duration.\u201d<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft size-full wp-image-10870\" title=\"C5\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2009\/07\/C5.jpg\" alt=\"C5\" width=\"324\" height=\"242\">Currently, the MER (Mission Evaluation Room) is processing \u2013 and working to approve \u2013 a request from EGIL (Electrical, General Instrumentation, and Lighting Engineer) to operate FC-3 below the 29 percent&nbsp;KOH limit set by the Combined Environmental Test document rules.<\/p>\n<p>As of now, FC-3 is functioning as expected and Endeavour\u2019s mission is proceeding as planned with Endeavour drawing power from the Space Station\u2019s solar arrays and batteries.<\/p>\n<p>Nevertheless, the Fuel Cells are a vital component of the Orbiter as they provide all the electrical energy necessary to operate the vehicle.&nbsp; As such, Flight Rules state that all three Fuel Cells have to be operating properly for a Shuttle mission to continue as planned.&nbsp;<\/p>\n<p>Should, for whatever reason, FC-3 become inoperative, Endeavour\u2019s crew would be forced into a Minimum Duration Flight situation \u2013 accomplishing only the Crit I objectives of the mission before undocking from the Station and landing on the first available opportunity in the United States.<\/p>\n<p><em><em>L2 members<\/em><\/em><em><em>:&nbsp;Documentation \u2013 from which the above article has quoted snippets \u2013 is available in full in the related L2 sections, now over 4000 gbs in size.<\/em><\/em><\/p>\n","protected":false},"excerpt":{"rendered":"<p>Endeavour\u2019s Dave Wolf and the ISS\u2019s Tim Kopra&nbsp;ventured outside the Shuttle\/Station complex on Saturday&nbsp;and completed the first of five EVAs (spacewalks) scheduled for the STS-127 mission.&nbsp; Meanwhile, the Mission Management Team (MMT) continues to monitor the Potassium Hydroxide (KOH) levels and operating temperature of Fuel Cell 3 on Endeavour as the docked portion of the [&hellip;]<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"","ping_status":"","sticky":false,"template":"","format":"standard","meta":{"_acf_changed":false,"inline_featured_image":false,"footnotes":"","_links_to":"","_links_to_target":""},"categories":[2],"tags":[567,9214,233,877,9038],"class_list":["post-41046","post","type-post","status-publish","format-standard","hentry","category-news","tag-eva","tag-fuel-cell","tag-iss","tag-jaxa","tag-sts-127"],"acf":[],"_links":{"self":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/41046"}],"collection":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/comments?post=41046"}],"version-history":[{"count":0,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/41046\/revisions"}],"wp:attachment":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media?parent=41046"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/categories?post=41046"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/tags?post=41046"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}