{"id":38284,"date":"2018-09-22T00:33:58","date_gmt":"2018-09-21T16:33:58","guid":{"rendered":"https:\/\/wp-productionenv-bjg9h2g2bgg5b8aa.southeastasia-01.azurewebsites.net\/news\/ngis-fires-up-gem-63-motor-destined-for-future-ula-launches\/"},"modified":"2018-09-22T00:33:58","modified_gmt":"2018-09-21T16:33:58","slug":"ngis-fires-up-gem-63-motor-destined-for-future-ula-launches","status":"publish","type":"post","link":"https:\/\/starpath.global\/news\/ngis-fires-up-gem-63-motor-destined-for-future-ula-launches\/","title":{"rendered":"NGIS fires up GEM-63 motor destined for future ULA launches"},"content":{"rendered":"<p>A new milestone for the future of United Launch Alliance\u2019s rockets was conducted by Northrop Grumman&nbsp;Innovation Systems (NGIS) on Thursday, when the first GEM-63 motor was test-fired for 110 seconds during the QM-1 firing at the NGIS testing facility in Promontory, Utah \u2013 sending 373,000 lbs of thrust along with bright fire, loud noise and vibration into the sunny desert sky.<br \/>\nThis test was the first of two qualification firings required before the GEM-63 is used in operational missions on the Atlas V, as a \u201cdrop in\u201d replacement for the current Aerojet Rocketdyne AJ-60A boosters.<\/p>\n<p>The GEM-63 fired was conditioned to a temperature of 40 degrees Fahrenheit to test the motor\u2019s performance in cold conditions. Ballistic, insulation, nozzle plug, igniter insulator performance and ablative nozzle erosion measurements were taken with over 160 instrumentation channels, and these were the main qualification objectives.<\/p>\n<\/p>\n<p><iframe title=\"GEM 63 Rocket Motor QM-1 Static Test\" src=\"https:\/\/www.youtube.com\/embed\/nwlOG9Z7YHU?feature=oembed\" frameborder=\"0\" allow=\"accelerometer; autoplay; clipboard-write; encrypted-media; gyroscope; picture-in-picture; web-share\" allowfullscreen=\"\" name=\"fitvid0\" data-gtm-yt-inspected-14=\"true\" data-gtm-yt-inspected-21=\"true\"><\/iframe><\/p>\n<p>Additional objectives included vibration, acoustic, and heat data, motor axial elongation and radiative heat monitoring data. This firing would take 110 seconds due to the cold conditioning, whereas it would normally fire for around 90 seconds (84 for the GEM-63, 94 for the XL). The cold conditioned test was done first as it is the most taxing test of the motor and its systems, including the fixed, non-steerable nozzle.<\/p>\n<p>The next test (QM-2) is a risk mitigation test for the US Air Force and will be hot conditioned to 90 degrees Fahrenheit. It is currently set for early December 2018, and if all goes well the first Atlas V launch with GEM-63\u2019s would take place in July 2019 with the STP-3 mission, which will use five boosters on the Atlas V.<\/p>\n<p>The GEM-63XL to follow will be the version that flies on the ULA Vulcan rocket, and it is set for its first test firing in October 2019, with its first launch to be determined.<\/p>\n<p><img fetchpriority=\"high\" decoding=\"async\" aria-describedby=\"caption-attachment-58210\" class=\"size-full wp-image-58210\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/09\/2018-09-21-192108.jpg\" alt=\"\" width=\"1681\" height=\"825\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/09\/2018-09-21-192108.jpg 1681w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/09\/2018-09-21-192108-350x172.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/09\/2018-09-21-192108-630x309.jpg 630w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/09\/2018-09-21-192108-768x377.jpg 768w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/09\/2018-09-21-192108-1170x574.jpg 1170w\" sizes=\"(max-width: 1681px) 100vw, 1681px\"><\/p>\n<p id=\"caption-attachment-58210\" class=\"wp-caption-text\">Vulcan heading uphill with four boosters \u2013 as envisioned by Nathan Koga for NSF\/L2<\/p>\n<p>The GEM-63XL at 864 inches in length is longer than the current GEM-63 tested today (791 inches in length) and the XL will use a pointed nosecone as opposed to the blunt curved nosecone that is currently used on the AJ-60A and that will be used on the GEM-63.<\/p>\n<p>The XL\u2019s exit plane diameter is 56 inches and its propellant mass is 105,900 lbs as opposed to a 54 in exit plane and 97,500 lb propellant mass for the GEM-63 tested today.<\/p>\n<p>Space Shuttle<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>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>Aerospace industry analysis<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 GEM-63 is not only three inches wider than the GEM-60 (used on the Delta IV), it is also much longer, and the GEM-63XL (the first case of which has already been spun) is the largest monolithic composite solid rocket casing that NGIS has ever produced. The biggest challenge that the widened and lengthened GEM booster posed for NGIS was building a new casting pit which was required due to the length of the booster.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" aria-describedby=\"caption-attachment-58208\" class=\"size-full wp-image-58208\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/09\/2018-09-21-191731.jpg\" alt=\"\" width=\"1123\" height=\"727\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/09\/2018-09-21-191731.jpg 1123w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/09\/2018-09-21-191731-350x227.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/09\/2018-09-21-191731-541x350.jpg 541w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/09\/2018-09-21-191731-768x497.jpg 768w\" sizes=\"(max-width: 1123px) 100vw, 1123px\"><\/p>\n<p id=\"caption-attachment-58208\" class=\"wp-caption-text\">The QM-1 motor before the test firing \u2013 via NGIS<\/p>\n<p>The casing is spun at the NGIS facility in Clearfield, UT, which is south of Promontory and Ogden, and other prep work is done at the Promontory and Bacchus facilities (in Magna near the Oquirrh Mountains, well south of Clearfield) before the final assembly is done and the rocket booster is sent on its way to the launch site, using a large wheeled transporter as part of the process.<\/p>\n<h4 class=\"widget-title penci-border-arrow\">See Also<\/h4>\n<ul>\n<li>NGIS Forum Section<\/li>\n<li>ULA Forum Section<\/li>\n<li>L2 NGIS Section<\/li>\n<li>Click here to Join L2<\/li>\n<\/ul>\n<p>The GEM-63 and GEM-63XL have been developed as a response to SpaceX\u2019s disruption of the space launch market, to help lower costs and increase performance for the ULA Atlas and Vulcan launch vehicles, as ULA and others need to control costs to stay competitive in the new era.<\/p>\n<p>\u201cNorthrop Grumman has been supplying solid propulsion motors for a variety of launch vehicles since 1964,\u201d said Scott Lehr, president, flight systems, Northrop Grumman.<\/p>\n<p>\u201cAs ULA\u2019s largest legacy supplier of solid propulsion, we\u2019re pleased that our most recent product has reached this important milestone. The successful completion of this test enables full production to begin.\u201d<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" aria-describedby=\"caption-attachment-58211\" class=\"size-full wp-image-58211\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/09\/2018-09-21-192240.jpg\" alt=\"\" width=\"1173\" height=\"606\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/09\/2018-09-21-192240.jpg 1173w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/09\/2018-09-21-192240-350x181.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/09\/2018-09-21-192240-630x325.jpg 630w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/09\/2018-09-21-192240-768x397.jpg 768w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/09\/2018-09-21-192240-1170x604.jpg 1170w\" sizes=\"(max-width: 1173px) 100vw, 1173px\"><\/p>\n<p id=\"caption-attachment-58211\" class=\"wp-caption-text\">GEM-63 firing \u2013 photo by Justin Davenport for NSF\/L2<\/p>\n<p>Sixty GEM-63\/63XL rockets have been ordered, 30 for each program. One booster per day will be shipped to launch sites when the process is in full swing, and production has already begun.<\/p>\n<p>The Northrop Grumman Innovation Systems unit and its Propulsion Systems Division have drawn on a heritage of six decades of work on solid rocket motors ranging from the Sidewinder to the Minuteman, the Shuttle, the Castor and earlier GEM graphite-epoxy motors and is one of two solid rocket production companies in the United States now.<\/p>\n<p>The GEM-63 and GEM-63XL are the latest solid rocket motors to be built and tested at the Promontory facility in the Utah desert, and these boosters will help power Atlas and Vulcan launch vehicles into the next decade.<\/p>\n","protected":false},"excerpt":{"rendered":"<p>A new milestone for the future of United Launch Alliance\u2019s rockets was conducted by Northrop Grumman&nbsp;Innovation Systems (NGIS) on Thursday, when the first GEM-63 motor was test-fired for 110 seconds during the QM-1 firing at the NGIS testing facility in Promontory, Utah \u2013 sending 373,000 lbs of thrust along with bright fire, loud noise and [&hellip;]<\/p>\n","protected":false},"author":1,"featured_media":38287,"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":[7758,8936,2899,363,364],"class_list":["post-38284","post","type-post","status-publish","format-standard","has-post-thumbnail","hentry","category-news","tag-atlas-v","tag-ngis","tag-orbital-atk","tag-ula","tag-vulcan"],"acf":[],"_links":{"self":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/38284"}],"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=38284"}],"version-history":[{"count":0,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/38284\/revisions"}],"wp:featuredmedia":[{"embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media\/38287"}],"wp:attachment":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media?parent=38284"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/categories?post=38284"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/tags?post=38284"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}