{"id":40825,"date":"2010-04-05T22:14:45","date_gmt":"2010-04-05T14:14:45","guid":{"rendered":"https:\/\/wp-productionenv-bjg9h2g2bgg5b8aa.southeastasia-01.azurewebsites.net\/news\/sts-131-fd2-inspections-completed-smoothly-despite-lack-of-ku-capability\/"},"modified":"2010-04-05T22:14:45","modified_gmt":"2010-04-05T14:14:45","slug":"sts-131-fd2-inspections-completed-smoothly-despite-lack-of-ku-capability","status":"publish","type":"post","link":"https:\/\/starpath.global\/news\/sts-131-fd2-inspections-completed-smoothly-despite-lack-of-ku-capability\/","title":{"rendered":"STS-131: FD2 inspections completed smoothly despite lack of KU capability"},"content":{"rendered":"<p>Veteran orbiter Discovery is closing in on the end of Flight Day 2 on orbit, following her launch at the first attempt on Monday morning, kicking off the STS-131 mission. Inspections of Discovery\u2019s Reinforced Carbon Carbon (RCC) and other parts of her Thermal Protection System (TPS) have been completed, although footage of the surveys won\u2019t be downloaded until after ISS docking on Flight Day 3, due to a failure of the Ku band antenna system.<\/p>\n<p>STS-131 FD2 Tasks:<\/p>\n<p>Flight Day 2\u2019s main events are the TPS and OMS pod surveys via the OBSS (Orbiter Boom Sensor System). EMU (EVA Suit) checkout and Centerline camera installation. ODS (Orbiter Docking System) ring extension and Rendezvous tools checkout.<\/p>\n<p>Two course correction burns \u2013 known as NC2 and NC3 burns \u2013 are also being undertaken, as Discovery continues to close in on the International Space Station (ISS) for docking on Flight Day 3.<\/p>\n<h4 class=\"widget-title penci-border-arrow\">See Also<\/h4>\n<ul>\n<li>STS-131 LIVE UPDATES<\/li>\n<li>L2 STS-131 Special Section<\/li>\n<li>Click here to Join L2<\/li>\n<\/ul>\n<p>Current status shows three Mission Evaluation Room (MER) items, although only one \u2013 an issue with the Ku band antenna system \u2013 is being worked on.<\/p>\n<p>\u201c(Pre-launch) MER-01 FC 2 (Fuel Cell 2) H2 Pump Motor Controller Voltage Increase. MER-02 MPS (Main Propulsion System) Engine 3 LH2 Inlet Pressure 3 OSL (Off Scale Low). MER-03 Ku-Band Forward &amp; Return Link Failures,\u201d noted L2 information.<\/p>\n<p>With FC2 performing nominally throughout the remainder of the countdown, and only a transducer on the MPS triggering MER-02 1 hour 40 minutes into flight, evaluations on the health of the Ku band currently shows it has likely failed for the duration of the mission.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft size-full wp-image-14143\" title=\"A4\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2010\/04\/A43.jpg\" alt=\"\" width=\"264\" height=\"175\">The Ku band antenna \u2013 which provides the live video from Discovery when on orbit, along with the ability for high bandwidth downloading and uploading between the ground and the orbiter, and radar range for rendezvous and docking \u2013 undergoes activation after the Payload Bay Doors (PLBDs) are opened on Flight Day 1.<\/p>\n<p>Rocket building kits<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>Spaceflight<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>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>\n<p>     (adsbygoogle = window.adsbygoogle || []).push({});<\/p>\n<p>The hardware on the antenna system is then put through a self test checkout, which failed. Commands to power cycle the two black boxes on the hardware failed to correct the problem, which has resulted in the Ku band antenna being unable to work on both the forward and return links.<\/p>\n<p>Its ability to provide a role on the black box which relates to radar range for rendezvous when Discovery closes in on docking with the ISS on Flight Day 3, won\u2019t be fully known until the crew attempt to use it for that purpose.<\/p>\n<p><img fetchpriority=\"high\" decoding=\"async\" class=\"alignleft size-full wp-image-14144\" title=\"A313\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2010\/04\/A313.jpg\" alt=\"\" width=\"304\" height=\"234\">The confirmed loss of the forward and return links has resulted in a change of plan for the downloading of ascent data \u2013 such as the WLE IDS (Wing Leading Edge Impact Detection System), and hi res photographs of the External Tank \u2013 and the ability to send the footage taken by the OBSS during FD2 inspections.<\/p>\n<p>This collection of data will instead be sent down on Flight Day 3, after docking with the ISS, using the Station\u2019s own Ku band assets. During FD2, the crew will create footage of the inspections via a Windows Movie Maker program on one of the orbiter\u2019s laptops.<\/p>\n<p>Although the Ku will now be unable to make up for patches in communication via the S-band and UHF assets on Discovery \u2013 resulting in additional levels of \u201cratty comm\u201d \u2013 the mission will be able to proceed as planned for the bulk of the flight.<\/p>\n<p>Yet to be decided by managers will be if they need to carry out Late Inspections whilst still being docked with the ISS \u2013 allowing for the footage to be sent down to the ground via ISS Ku. The potential to add an additional docked day on Station is available in the mission timeline options.<\/p>\n<p>MMT presentations have started to arrive into L2, and an article based on their content will be published on Tuesday.<\/p>\n<p>STS-131 Specific Articles: http:\/\/www.nasaspaceflight.com\/tag\/sts-131\/<\/p>\n<p>FD2 Inspection Tasks:<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft size-full wp-image-14141\" title=\"A37\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2010\/04\/A37.jpg\" alt=\"\" width=\"307\" height=\"230\">Normally, the handheld photography and ET Umbilical Well imagery would already be in the process of being downloaded to the ground for the Damage Assessment Team (DAT) to begin their evaluations into any foam liberation events.<\/p>\n<p>Given the Ku antenna problem, that footage \u2013 along with the FD2 inspections of the health of Discovery\u2019s heatshield \u2013 won\u2019t arrive at the DAT office until later of FD3.<\/p>\n<p>With the NC2 and NC3 Rendezvous burns planned into the flight day, the main role for the crew was the unberthing of the OBSS via the RMS (Remote Manipulator System), in order to carry out surveys of Discovery\u2019s wing and nose cap, before heading to the OMS Pods to check for any tile damage or protruding blankets.<\/p>\n<p>\u201cTPS Surveys: All RCC (Reinforced Carbon Carbon) is inspected during the OBSS Starboard Wing, Nose Cap, and Port Wing surveys. The two wing surveys also cover most of the areas of the crew cabin. The OMS Pod is inspected using a handheld camera to take pictures from the aft flight deck windows,\u201d noted Flight Readiness Review (FRR) mission outline documentation (L2).<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft size-full wp-image-14142\" title=\"A26\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2010\/04\/A26.jpg\" alt=\"\" width=\"270\" height=\"198\">The OBSS survey procedures incorporate the use of supplemental IDC (Digital Camera) images during LDRI (Laser Dynamic Range Imager) scans, thus reducing the likelihood of needing Focused Inspection. The OBSS unberth procedure incorporates the LDRI 3D calibration and the starboard survey the flat field calibration.<\/p>\n<p>Three crewmembers are required continuously during the surveys, two for the SRMS\/OBSS ops and one to operate the situational awareness cameras and sensors. Only two crewmembers are required during unberthing and berthing operations (non-laser ops).<\/p>\n<p>Scans of the entire starboard wing are scheduled first, given they are not easily performed, or are impossible to perform while docked \u2013 providing a challenge should a docked late inspection be required. The surveys are scheduled to continue through the night passes, but the crew may elect to pause if the night time visuals are not sufficient.<\/p>\n<p>\u201cThe LDRI survey attitude requires no sun within a +\/-20 degree field of view (FOV) of the laser bore-sight. Additionally, no sun can be within a 10 degree half-cone directly behind the instrument; however it is highly desired to keep the sun at a 90 degree half cone behind the instrument as long as it\u2019s not directly behind,\u201d added the FRR overview.<\/p>\n<p>Although Flight Day 3\u2019s RPM (Rbar Pitch Maneuver) \u2013 carried out \u2018underneath\u2019 the ISS ahead of docking \u2013 will provide a near-complete overview of Discovery\u2019s heatshield, the OBSS inspections will give the opening insights into the extent of any damage sustained during the ride uphill.<\/p>\n<p>A level of review is already been undertaken by engineers on the ground, who are able to review ground-based camera and radar footage relating to debris events.<\/p>\n","protected":false},"excerpt":{"rendered":"<p>Veteran orbiter Discovery is closing in on the end of Flight Day 2 on orbit, following her launch at the first attempt on Monday morning, kicking off the STS-131 mission. Inspections of Discovery\u2019s Reinforced Carbon Carbon (RCC) and other parts of her Thermal Protection System (TPS) have been completed, although footage of the surveys won\u2019t [&hellip;]<\/p>\n","protected":false},"author":1,"featured_media":29525,"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":[9116,9184,7935],"class_list":["post-40825","post","type-post","status-publish","format-standard","has-post-thumbnail","hentry","category-news","tag-ku","tag-sts-131","tag-tps"],"acf":[],"_links":{"self":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/40825"}],"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=40825"}],"version-history":[{"count":0,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/40825\/revisions"}],"wp:featuredmedia":[{"embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media\/29525"}],"wp:attachment":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media?parent=40825"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/categories?post=40825"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/tags?post=40825"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}