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It was also notable that ATK continued to refine and tweak the motors during the final flights, with one example being the redesign to the SRB Thrust Vector Control (TVC) Auxiliary Power Unit (APU) fuel pump for the final three Shuttle missions, removing a \u201ccritical 1\u201d failure scenario that held the small potential of a LOV\/C (Loss of Vehicle\/Crew) event.<\/p>\n
While the boosters are continuing to evolve, the huge legacy of their role with the Space Shuttle will directly feed into their use on the SLS \u2013 a Shuttle Derived (SD) Heavy Lift Launch Vehicle (HLV).<\/p>\n
ATK Boosters with SLS Block 1:<\/p>\n
SpaceX launch tickets
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The SLS will debut at the end of 2017 as the Block 1 configuration consisting of a core stage using four Pratt and Whitney Rocketdyne (PWD) RS-25Ds \u2013 formerly used by the Shuttle Program \u2013 two ATK five segment Solid Rocket Boosters (SRBs) and an Interim Cryogenic Propulsion Stage (ICPS), highly likely to be a Delta Cryogenic Second Stage (DCSS).<\/p>\n
Three static fire tests have already taken place on the five segment boosters, as the motor transferred its service from the now-defunct Ares 1\u2019s first stage to SLS.<\/p>\n
![\"Screenshot](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2013\/01\/A3171.jpg\" "\\"Screenshot")
The latest test \u2013 DM-3 \u2013 took place in 2011 and was the last in a series of development motors to be tested. It was also the most heavily instrumented solid rocket motor in NASA history, with a total of 37 test objectives measured through more than 970 instruments.<\/p>\n(Image taken from the amazing 220mb super slow-mo DM-3 Five Seg Motor Ground Test Video \u2013 available in L2 \u2013 LINK).<\/p>\n
The previous test \u2013 DM-2 in 2010 \u2013 was carried out with a total of 53 design objectives, measured through more than 760 instruments. For that test, the motor was cooled to 40 degrees F \u2013 a \u201ccold motor\u201d test \u2013 in order to measure solid rocket motor performance at low temperature, as well as to verify design requirements of new materials in the motor joints.<\/p>\n
Click here for SRB Articles: http:\/\/www.nasaspaceflight.com\/tag\/srb\/<\/p>\n
![\"DM-3](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2013\/01\/Z52-350x205.jpg\" "\\"DM-3")
The DM-3 incorporated several performance-based improvements to the designs of the first two development motors. Additionally, the core of DM-3 was heated to 90 degrees Fahrenheit for this full-duration firing to verify the motor\u2019s performance at high temperatures.<\/p>\nATK are already deep into preparations for the first qualification firing of the five segment booster, with QM-1 set to take place in May, 2013.<\/p>\n
It is expected that the five segment solid motor will be used on all SLS flights until at least the middle of the 2020s, with source information noting SLS managers have the option to launch up to 10 missions using the current five segment booster design.<\/p>\n
ATK Advanced Booster:<\/p>\n
The forward path for SLS is to evolve from the 70mT HLV into the 105mt \u2013 known as the Block IA \u2013 before eventually advancing into the 130mT Super Heavy launcher known as the Block II.<\/p>\n
As part of enabling this evolution, a competition will decide between numerous proposals that will create an \u201cadvanced booster\u201d option for SLS, which will be implemented on the Block 1A (or Block 1B \u2013 depending on the configuration), prior to its role with the Block II from its first launch.<\/p>\n
![\"Dynetics\/PWR](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2013\/01\/Z91-350x225.jpg\" "\\"Dynetics\/PWR")
One such proposal \u2013 which is currently being worked on under NASA\u2019s SLS Advanced Booster Engineering Demonstration and\/or Risk Reduction (ABEDRR) procurement \u2013 was reported on by this site after Dynetics, Inc. and Pratt & Whitney Rocketdyne (PWR) formed a team \u201cto offer an affordable booster approach that meets the evolved capabilities of the SLS\u201d \u2013 and presented their overview at the 63rd International Astronautical Congress, Naples, Italy in October, 2012.<\/p>\nTheir liquid booster approach \u2013 using the baseline of the famous Saturn V F-1 engines \u2013 claims they could advance SLS\u2019 capability to launch payloads of 150mT to orbit.<\/p>\n
![\"ATK](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2013\/01\/Z63.jpg\" "\\"ATK")
ATK\u2019s proposal \u2013 outlined in a presentation acquired by L2 \u2013 builds on their legacy, with a motor that is \u201cadvanced\u201d on several levels, by \u201cprovid(ing) NASA the capability for the SLS to achieve 130 mT payload with significant margin, utilizing a booster that is 40 percent less expensive and 24 percent more reliable than the current SLS booster.<\/p>\n\u201cSome of the characteristics of the Advanced Booster include features that have been identified by NASA as important for the next-generation booster are: an energetic propellant to improve performance and reduce cost, a composite case using low cost fiber\/resin, electric Thrust Vector Control (TVC), and an adaptable core attach design to minimize interface concerns.\u201d<\/p>\n
ATK cite advanced manufacturing techniques and streamlined processes \u2013 combined with an innovative design that includes the nose cone reshaped to reduce aerodynamic loads on the core stage \u2013 as a major part of the 40 percent reduction in costs when compared to the five-segment SRBs.<\/p>\n
![\"ATK](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2013\/01\/Z82.jpg\" "\\"ATK")
The advanced booster will utilize composite casing with low cost, high strength fibers \u2013 represented as black casings in notional graphics.<\/p>\nATK are also proposing to reduce the number of segments \u2013 back to four \u2013 to improve processing at launch site, along with simplified forward and aft structures and increased comparability with the overall vehicle avionics architecture.<\/p>\n
A key line in the presentation cites the Advanced Booster \u201cwill provide 42 percent of SLS vehicle impulse while making up only 18 percent of the total vehicle propulsion cost.\u201d<\/p>\n
Click here for SLS Articles: http:\/\/www.nasaspaceflight.com\/tag\/hlv\/<\/p>\n
Charts provided in the presentation expand on areas where performance will be improved, all while reducing costs when compared to the five segment motor.<\/p>\n
![\"ATK](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2013\/01\/Z71.jpg\" "\\"ATK")
This can be clearly seen in examples such as the use of the composite casings, which provide a 4,128lbm payload capability improvement. The simplified stage assemblies comparison cites the saving of 480 man hours \u2013 a 50 percent reduction in the man hours required on the five segment motor.<\/p>\nMost impressive is the improved ballistics, with the higher ISP density of the propellent boosting payload performance by nearly 25,000lbm, yet saving $9.2m in costs per booster.<\/p>\n
As listed, the increased operating pressure, improved propellant, tailored thrust profile, increased expansion ratio all combine to provide a 15.1mT boost to the SLS\u2019 payload capability.<\/p>\n
However, what can\u2019t be estimated is ATK\u2019s foothold as the provider of boosters for NASA\u2019s human space flight program for the past 30 years. A continuation with the familiarity of the solid motors is continually classed as the favored option by SLS sources.<\/p>\n
(Images: Via NASA and L2 content from L2\u2032s SLS specific L2 section, 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
(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: http:\/\/www.nasaspaceflight.com\/l2\/)<\/p>\n","protected":false},"excerpt":{"rendered":"
A presentation overviewing ATK\u2019s preliminary proposal for the upcoming advanced booster competition for Space Launch System (SLS) claims the new motor will be 40 percent cheaper and 23.5 percent more reliable than the five segment booster that will initially launch with the Heavy Lift Launch Vehicle (HLV) \u2013 all while adding 15.1mT of additional performance. […]<\/p>\n","protected":false},"author":1,"featured_media":30316,"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":[4144,9034,8665,624,7806],"class_list":["post-39934","post","type-post","status-publish","format-standard","has-post-thumbnail","hentry","category-news","tag-atk","tag-hlv","tag-rsrm","tag-sls","tag-srb"],"acf":[],"_links":{"self":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/39934"}],"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=39934"}],"version-history":[{"count":0,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/39934\/revisions"}],"wp:featuredmedia":[{"embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media\/30316"}],"wp:attachment":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media?parent=39934"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/categories?post=39934"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/tags?post=39934"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}