{"id":39397,"date":"2015-02-20T23:04:23","date_gmt":"2015-02-20T15:04:23","guid":{"rendered":"https:\/\/wp-productionenv-bjg9h2g2bgg5b8aa.southeastasia-01.azurewebsites.net\/news\/advanced-boosters-progress-towards-a-solid-future-for-sls\/"},"modified":"2015-02-20T23:04:23","modified_gmt":"2015-02-20T15:04:23","slug":"advanced-boosters-progress-towards-a-solid-future-for-sls","status":"publish","type":"post","link":"https:\/\/starpath.global\/news\/advanced-boosters-progress-towards-a-solid-future-for-sls\/","title":{"rendered":"Advanced Boosters progress towards a solid future for SLS"},"content":{"rendered":"<p>The giant boosters that will help shove NASA\u2019s new monster rocket uphill are hitting milestones on two fronts. As Orbital ATK prepare for next month\u2019s Qualification Motor -1 (QM-1) test firing of the five segment solid motor, teams are also testing the technologies required for the Advanced Booster \u2013 a motor that is set to provide SLS with extra upmass capability from the mid 2020s onwards.<br \/>\nBoosters:<\/p>\n<p>The previously delayed QM-1 test firing now remains on track for March 11, still well within the critical path schedule for the debut launch of SLS in 2018.<\/p>\n<p>The five segment version is a direct descendant of the four segment motor that pushed Space Shuttles through their first stage flight \u2013 boosters that were continually upgraded and improved right through to their final mission with STS-135.<\/p>\n<p><img fetchpriority=\"high\" decoding=\"async\" class=\"alignleft size-medium wp-image-39349\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/02\/2015-02-20-15_14_00-NASA-Orbital-ATK-Preparing-Solid-Rocket-Booster-Avionics-for-Mission-Success-_--350x235.jpg\" alt=\"2015-02-20 15_14_00-NASA, Orbital ATK Preparing Solid Rocket Booster Avionics for Mission Success _\" width=\"350\" height=\"235\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/02\/2015-02-20-15_14_00-NASA-Orbital-ATK-Preparing-Solid-Rocket-Booster-Avionics-for-Mission-Success-_--350x235.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/02\/2015-02-20-15_14_00-NASA-Orbital-ATK-Preparing-Solid-Rocket-Booster-Avionics-for-Mission-Success-_--520x350.jpg 520w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/02\/2015-02-20-15_14_00-NASA-Orbital-ATK-Preparing-Solid-Rocket-Booster-Avionics-for-Mission-Success-_--768x517.jpg 768w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/02\/2015-02-20-15_14_00-NASA-Orbital-ATK-Preparing-Solid-Rocket-Booster-Avionics-for-Mission-Success-_--1170x787.jpg 1170w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/02\/2015-02-20-15_14_00-NASA-Orbital-ATK-Preparing-Solid-Rocket-Booster-Avionics-for-Mission-Success-_-.jpg 1246w\" sizes=\"(max-width: 350px) 100vw, 350px\">With the QM-1 motor now anchored into the ground at&nbsp;Orbital ATK\u2019s test facility in Promontory, Utah \u2013 preparations for its big, noisy day included final checks on the&nbsp;flight-like avionics system that will be tested during the firing.<\/p>\n<p>While the test will produce a huge amount of data on the booster\u2019s performance, the validation of the&nbsp;avionics system \u2013 responsible for igniting, steering and jettison of the boosters \u2013 will be critical.<\/p>\n<p>\u201cWe are designing a system for a human-rated vehicle that has to be at a minimum single-fault tolerant, which means no one failure on a critical system can result in a big problem for the mission,\u201d noted Eric Corder, avionics system manager for the SLS Booster Element at MSFC.<\/p>\n<p>\u201cWe don\u2019t want the rocket to just operate the way it\u2019s supposed to. Our team intentionally implements failure scenarios to the electronics to make sure, for example, a shorted circuit or faulty box doesn\u2019t compromise mission success. That\u2019s even an issue that may have a one-in-10,000 chance of occurring.\u201d<\/p>\n<h4 class=\"widget-title penci-border-arrow\">See Also<\/h4>\n<ul>\n<li>SLS Forum Section<\/li>\n<li>L2 SLS Section<\/li>\n<li>L2 SRB Section<\/li>\n<li>Click here to Join L2<\/li>\n<\/ul>\n<p>The heritage of mitigating potential issues during first stage flight was seen right through to the final Shuttle missions \u2013 such as the redesign of the&nbsp;Thrust Vector Control (TVC) Auxiliary Power Unit (APU) fuel pump ahead of STS-133.<\/p>\n<p>NASA educational resources<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>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>\n<p>     (adsbygoogle = window.adsbygoogle || []).push({});<\/p>\n<p>This design change eliminated the highest \u2013 albeit extremely unlikely to occur \u2013 \u201ccritical 1\u201d failure scenario in the system, which held the potential of a LOV\/C (Loss of Vehicle\/Crew) event.<\/p>\n<p>Ultimately, in tandem with improvements to numerous elements of the Space Shuttle system \u2013 such as the External Tank modifications,&nbsp;the final flights were the \u201csafest\u201d in Shuttle history. Post Flight IFA (In Flight Anomaly) documentation (L2) confirmed the final flights of the Shuttle Reusable Solid Rocket Motors (RSRM) performed extremely well.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft size-medium wp-image-39355\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/02\/2015-02-20-17_11_32-L2-Level_-Space-Launch-System-Update-Notes-And-Discussion-Sept-2014-onwards-350x277.jpg\" alt=\"2015-02-20 17_11_32-L2 Level_ Space Launch System Update Notes And Discussion - Sept, 2014 onwards\" width=\"350\" height=\"277\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/02\/2015-02-20-17_11_32-L2-Level_-Space-Launch-System-Update-Notes-And-Discussion-Sept-2014-onwards-350x277.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/02\/2015-02-20-17_11_32-L2-Level_-Space-Launch-System-Update-Notes-And-Discussion-Sept-2014-onwards-443x350.jpg 443w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/02\/2015-02-20-17_11_32-L2-Level_-Space-Launch-System-Update-Notes-And-Discussion-Sept-2014-onwards-768x607.jpg 768w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/02\/2015-02-20-17_11_32-L2-Level_-Space-Launch-System-Update-Notes-And-Discussion-Sept-2014-onwards.jpg 805w\" sizes=\"(max-width: 350px) 100vw, 350px\">With the Space Launch System (SLS) utilizing a large amount of Shuttle hardware, the heritage of the safety and performance improvements will naturally migrate into the monster rocket.<\/p>\n<p>The five segment booster \u2013 a direct descendant of the four segment motor \u2013 is expected to fly into at least the mid-2020s, with both the 70 mT Block 1 and the 105 mT Block 1B variant&nbsp;\u2013 with the latter expected to become the SLS workhorse.<\/p>\n<p>Early SLS manifests pointed to a switch to using the Advanced Booster in 2024, on a cargo mission \u2013 although it is likely this will now take place in the second half of the 2020s.<\/p>\n<p>The Advanced Booster drive became a competition, at the request of political powers, leading to&nbsp;NASA\u2019s SLS Advanced Booster Engineering Demonstration and\/or Risk Reduction (ABEDRR) procurement process.<\/p>\n<p>That in turn resulted in some interesting options for providing SLS with additional power for its eventual role of lofting large payloads into deep space.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2012\/11\/Z91.jpg\" alt=\"\" width=\"351\" height=\"226\">In 2012,&nbsp;Pratt &amp; Whitney Rocketdyne (PWR) \u2013 now Aerojet Rockeydyne \u2013 went straight into \u201cbeast mode\u201d with a proposal to utilize F-1 powerhouses from the heritage of the Saturn era, resulting two liquid boosters that could enable SLS to power 150 mT to orbit.<\/p>\n<p>Alabama company Dynetics was brought on board to mature the design that saw two&nbsp;modernized F-1 engines \u2013 known as the F-1B \u2013 paired on each booster.<\/p>\n<p>Internally, SLS engineers cited they were having issues with all versions of liquid boosters, claiming high acceleration forces were problematic for the stack, while a completely new Mobile Launcher design would be required for such a vehicle.<\/p>\n<p>It was also claimed that&nbsp;KSC Ground Operations were informed in the middle of 2014 that the boosters for SLS will be solids throughout the evolution of the vehicle. All work to revamp SLS\u2019 Pad 39B pad \u2013 including the new flame deflection and trench design \u2013 have the solids at the center of their evaluations.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2013\/01\/Z63.jpg\" alt=\"ATK Advanced Booster Slide - via L2\" width=\"308\" height=\"335\">As such, Orbital ATK\u2019s Advanced Booster proposal is the clear favorite to take over from the current five segment motor.<\/p>\n<p>These new super boosters \u2013 nicknamed \u201cThe Dark Knights\u201d \u2013 would be a large evolution on the current motors, both internally and externally.<\/p>\n<p>Moving away from the traditional steel casings, a switch to composite materials, fabricated from&nbsp;low cost, high strength fibers,&nbsp;provide a documented payload capability improvement of&nbsp;4,128lbm.<\/p>\n<p>With the move back to four segments, the simplified stage assemblies comparison cites this would become part of a saving of 480 man hours \u2013 resulting in a 50 percent reduction in the man hours compared to that required for the five segment motor.<\/p>\n<p>ATK claimed in their documentation that the booster would be 40 percent less expensive and 24 percent more reliable than the current SLS booster.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2013\/10\/Z773.jpg\" alt=\"Z77\" width=\"351\" height=\"199\">Testing of the composite materials picked up the pace in 2013, with ATK&nbsp;successfully completing the filament winding of a pathfinder Advanced Booster composite case \u2013 resulting in a 92-inch-diameter, 27-foot-long composite structure.<\/p>\n<p>At the time, ATK \u2013 as they were then known \u2013 confirmed&nbsp;they overcame challenges related to the affordability and performance required of an Advanced Booster during the case winding operations for the test article.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft size-medium wp-image-39350\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/02\/2015-02-20-16_13_08-A-Composite-Booster-Gets-a-Burst-of-Energy-_-NASA-350x269.jpg\" alt=\"2015-02-20 16_13_08-A Composite Booster Gets a Burst of Energy _ NASA\" width=\"350\" height=\"269\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/02\/2015-02-20-16_13_08-A-Composite-Booster-Gets-a-Burst-of-Energy-_-NASA-350x269.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/02\/2015-02-20-16_13_08-A-Composite-Booster-Gets-a-Burst-of-Energy-_-NASA-456x350.jpg 456w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/02\/2015-02-20-16_13_08-A-Composite-Booster-Gets-a-Burst-of-Energy-_-NASA.jpg 599w\" sizes=\"(max-width: 350px) 100vw, 350px\">The composite testing achieved another milestone this year, when engineers used a&nbsp;25 feet long and 92 inches in diameter composite case in a \u201cburst test\u201d \u2013 subjecting it to 3,000 pounds per square inch of pressure.<\/p>\n<p>*Click here for video of the test*<\/p>\n<p>\u201cThe test is very dramatic,\u201d noted Angie Jackman, of the SLS Spacecraft\/Payload Integration and Evolution (SPIE) office at MSFC. \u201cWhen composites fail, it\u2019s the glue or the resin that fails first \u2013 not the fiber that fails. There\u2019s a big boom, and it\u2019s all spaghetti.\u201d<\/p>\n<p>The test showed the casing performed as expected, failing well above the pressures associated with its role during a launch. It was even purposely damaged at multiple points on the casing to study what effect it would have on how the casing performed.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2013\/05\/Z51.jpg\" alt=\"ATK Advanced Booster Propellant Mixing\" width=\"289\" height=\"284\">Internal to the booster, technicians that are part of the Propellant\/Liner\/Insulation (PLI) Integrated Product Team (IPT) have been working on the all-important propellant mix, cooking up recipes for increased performance to aid SLS during first stage flight.<\/p>\n<p>Back in 2013, work involved testing&nbsp;66 unique propellant mixes to test candidate propellant formulations for burn rate performance and mechanical property characteristics.<\/p>\n<p>The team worked on selecting the best formulation within each design of experiments (DOE) matrix family to pursue further testing within larger scale mixes.<\/p>\n<p>Details of the favored mix is likely to have been made proprietary &nbsp;\u2013 although previous schedules have shown this winning mix is set for a test firing as earlier as this year.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft size-full wp-image-29468\" title=\"Nose Cone for ATK Advanced Booster\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2013\/05\/Z452.jpg\" alt=\"Nose Cone for ATK Advanced Booster\" width=\"351\" height=\"266\">Also under evaluation is a nose cone design change, with wind tunnel testing as early as 2013 showing engineers have been looking into solutions for an aeroacoustic loading issue (vibrations)&nbsp;\u2013 in the transonic flight region \u2013 impacting on the booster\/core attach points.<\/p>\n<p>Initial information pointed to potentially changing the nose cone design to that seen on boosters used by Ariane 5, or indeed the cone design currently portrayed by ATK\u2019s Advanced Boosters, in order to mitigate the issue.<\/p>\n<p>Currently, representations of the evolved Block 2 SLS show the nose cones as portrayed on all variants of the monster rocket. However, they also show an all-white vehicle, which is not accurate. The core of SLS won\u2019t be painted white.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2013\/10\/Z313.jpg\" alt=\"Z3\" width=\"305\" height=\"301\">However, Orbital ATK\u2019s fully evolved Block 2 SLS renderings show the nose cose design in place, albeit via graphics that are tagged as notional.<\/p>\n<p>It is also unclear whether SLS will require to switch back to an original plan of&nbsp;adding a fifth RS-25 engine on the core, in order to achieve the 130 mT requirement laid out by lawmakers. Currently, all variants of SLS have been baselined with four RS-25s on their cores.<\/p>\n<p>Also, SLS evaluations continue to show \u201cover performance\u201d against the baseline 70 mT and 105 mT ratings, which have been further aided by the future incorporation of the powerful Exploration Upper Stage (EUS).<\/p>\n<p>It has been claimed internally, that the Block 1B, with advanced boosters and EUS could achieve most \u2013 if not all \u2013 of NASA\u2019s deep space exploration goals, potentially removing the need to evolve to the Block 2.<\/p>\n<p>There is also an interesting future scenario based on when the Block 2 is expected to come on line, which is not until the 2030s, by which time SpaceX\u2019s more powerful Exploration Class rocket for its&nbsp;Mars Colonial Transporter (MCT) system should already be flying.<\/p>\n<p>(Images: NASA, Orbital ATK and L2 artist Nathan Koga via L2\u2019s SLS sections, which includes, presentations, videos, graphics and internal \u2013 interactive with actual SLS engineers \u2013 updates on the SLS and HLV, available on no other site.)<\/p>\n<p>(L2 is \u2013 as it has been for the past several years \u2013 providing full exclusive SLS and Exploration Planning coverage. To join L2, click here:&nbsp;http:\/\/www.nasaspaceflight.com\/l2\/)<\/p>\n","protected":false},"excerpt":{"rendered":"<p>The giant boosters that will help shove NASA\u2019s new monster rocket uphill are hitting milestones on two fronts. As Orbital ATK prepare for next month\u2019s Qualification Motor -1 (QM-1) test firing of the five segment solid motor, teams are also testing the technologies required for the Advanced Booster \u2013 a motor that is set to [&hellip;]<\/p>\n","protected":false},"author":1,"featured_media":30107,"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":[624,7806],"class_list":["post-39397","post","type-post","status-publish","format-standard","has-post-thumbnail","hentry","category-news","tag-sls","tag-srb"],"acf":[],"_links":{"self":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/39397"}],"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=39397"}],"version-history":[{"count":0,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/39397\/revisions"}],"wp:featuredmedia":[{"embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media\/30107"}],"wp:attachment":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media?parent=39397"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/categories?post=39397"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/tags?post=39397"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}