{"id":24777,"date":"2021-12-02T22:17:41","date_gmt":"2021-12-02T14:17:41","guid":{"rendered":"https:\/\/wp-productionenv-bjg9h2g2bgg5b8aa.southeastasia-01.azurewebsites.net\/news\/neutron-switches-to-methane-oxygen-1-meganewton-archimedes-engine-revealed\/"},"modified":"2021-12-02T22:17:41","modified_gmt":"2021-12-02T14:17:41","slug":"neutron-switches-to-methane-oxygen-1-meganewton-archimedes-engine-revealed","status":"publish","type":"post","link":"https:\/\/starpath.global\/news\/neutron-switches-to-methane-oxygen-1-meganewton-archimedes-engine-revealed\/","title":{"rendered":"Neutron switches to methane\/oxygen, 1 Meganewton Archimedes engine revealed"},"content":{"rendered":"<p>Rocket Lab has provided a significant update in the progress of their Neutron rocket, a vehicle aimed primarily at the small-scale interplanetary and low Earth orbit mega-constellation markets at first.&nbsp;<\/p>\n<p>Among the major updates announced by Rocket Lab CEO Peter Beck were a complete switch of propellants, a firm Return To Launch Site landing plan with the elimination of down-range ocean landings, reveal of the building materials, and introduction of the new 1 Meganewton Archimedes engine.<\/p>\n<\/p>\n<p>As previously announced<\/p>\n<p>Neutron was revealed earlier this year on March 1 as a 40 m tall medium-lift launcher&nbsp;with a 4.5 m diameter payload fairing and a payload capacity to a 400 km low Earth orbit of 8,000 kg. In addition, the rocket would be capable of delivering roughly 2,000 kg to lunar orbit and 1,500 kg to Venus or Mars.<\/p>\n<p>At the time, Neutron was slated to launch on its first mission in 2024 with initial missions planned from Launch Pad 0A at the Mid-Atlantic Regional Spaceport in Virginia.&nbsp;<\/p>\n<p>After boosting the vehicle toward orbit, Neutron\u2019s first stage was designed to land on floating platforms downrange from the launch site in the ocean for recovery and reuse. Landing tests were planned to occur during operational flights so that the rocket would be available to customers during the period in which Rocket Lab worked out the landing and recovery process.<\/p>\n<p><img fetchpriority=\"high\" decoding=\"async\" aria-describedby=\"caption-attachment-82372\" class=\"size-full wp-image-82372\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/11\/NSF-2021-12-02-13-23-27-644.jpg\" alt=\"\" width=\"2025\" height=\"1136\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/11\/NSF-2021-12-02-13-23-27-644.jpg 2025w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/11\/NSF-2021-12-02-13-23-27-644-350x196.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/11\/NSF-2021-12-02-13-23-27-644-624x350.jpg 624w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/11\/NSF-2021-12-02-13-23-27-644-768x431.jpg 768w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/11\/NSF-2021-12-02-13-23-27-644-1920x1077.jpg 1920w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/11\/NSF-2021-12-02-13-23-27-644-1170x656.jpg 1170w\" sizes=\"(max-width: 2025px) 100vw, 2025px\"><\/p>\n<p id=\"caption-attachment-82372\" class=\"wp-caption-text\">The base of Neutron, with its static landing legs, and the rocket\u2019s stats behind Peter Beck (not to scale). (Credit: Rocket Lab)<\/p>\n<p>Also among the elements announced for the rocket was the intention to allow Neutron\u2019s design to eventually support human spaceflight activities \u2014 both in terms of low Earth orbit space station resupply missions and crewed flights.<\/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 mission updates<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>Space Shuttle models<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>At the time, no crew or cargo vehicle was in development.<\/p>\n<p>Additionally, Rocket Lab stated the vehicle would utilize RP-1 kerosene and liquid oxygen as its propellants but did not specify the to-be-developed engine the vehicle would use nor the number of engines on each of its two stages \u2014 though Beck did tell NASASpaceflight later that it would be the \u201cleast amount of engines practical.\u201d<\/p>\n<p>Beck further said that Neutron would be capable of lifting 98% of all satellites forecast to launch through 2029 \u2014 potentially including batches of Rocket Lab\u2019s own&nbsp;Photon&nbsp;satellites.<\/p>\n<p>December 2 update<\/p>\n<p>Today\u2019s update announced several major and significant changes to the Neutron design, including the types of propellants it will use, its overall flight profile, as well as its composition.<\/p>\n<\/p>\n<p><iframe title=\"Neutron Rocket | Development Update\" src=\"https:\/\/www.youtube.com\/embed\/7kwAPr5G6WA?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>Chief among the changes is the fact that Rocket Lab will no longer utilize deployable landing legs but instead utilize a fixed structure to eliminate as many potential failure points and create as simple of a design as possible.<\/p>\n<p>Also gone is the RP-1 kerosene and liquid oxygen mixture, replaced with liquid methane and liquid oxygen that will fuel a new engine called Archimedes. This 1 Meganewton thrust engine will have a specific impulse, or Isp, of at least 320 seconds. Seven Archimedes engines will power the first stage.<\/p>\n<p>Additionally, the payload fairings on Neutron will not deploy from the vehicle. Instead, at the end of the first stage burn, the top of the rocket will open like a clamshell \u2014 with renderings showing a four-plane separation system \u2014 to deploy the second stage that will continue taking the payload onward to its desired orbit or interplanetary destination.&nbsp;<\/p>\n<p>After second stage\/payload deployment, the clamshell will close and the entire first stage and payload fairing combination will then perform a Return To Launch Site (RTLS) landing.<\/p>\n<p>This RTLS landing profile is another major change in Neutron\u2019s design, with Peter Beck previously mentioning that such a maneuver would stretch the rocket, which was something Rocket Lab was previously uninterested in doing but have since switched to as the design has evolved.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" aria-describedby=\"caption-attachment-82368\" class=\"size-full wp-image-82368\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/11\/NSF-2021-12-02-13-25-23-432.jpg\" alt=\"\" width=\"2025\" height=\"1136\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/11\/NSF-2021-12-02-13-25-23-432.jpg 2025w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/11\/NSF-2021-12-02-13-25-23-432-350x196.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/11\/NSF-2021-12-02-13-25-23-432-624x350.jpg 624w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/11\/NSF-2021-12-02-13-25-23-432-768x431.jpg 768w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/11\/NSF-2021-12-02-13-25-23-432-1920x1077.jpg 1920w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/11\/NSF-2021-12-02-13-25-23-432-1170x656.jpg 1170w\" sizes=\"(max-width: 2025px) 100vw, 2025px\"><\/p>\n<p id=\"caption-attachment-82368\" class=\"wp-caption-text\">Neutron ends a mission with an RTLS landing. (Credit: Rocket Lab)<\/p>\n<p>In another major reversal from March, downrange landings in the ocean are now no longer planned for the rocket, and missions that cannot return to the launch site would be expended \u2014which would increase the total payload capacity of the rocket from 8,000 kg, with stage one return, to 15,000 kg with an expended first stage and fairings.<\/p>\n<p>For the upper stage, Beck noted that it has competing design requirements. \u201cIt has to be the lightest and the most high-performing structure as part of the launch vehicle, but it also has to be the lowest cost because for Neutron, at least at this point in time, it\u2019s a disposable stage.\u201d<\/p>\n<p>To this, and based on the clamshell design of the opening firings, the second stage is hung from the payload separation plane. According to Beck, Neutron\u2019s second stage is \u201cincredibly strong and the lightest upper stage ever in history.\u201d<\/p>\n<p>Overall, Neutron is now 7 m in diameter at its base with an increased payload fairing diameter of 5 m. The overall height of the rocket has not changed and remains 40 m.<\/p>\n<p>The rocket will be made of Rocket Lab\u2019s own carbon composite material. Peter Beck had previously noted that this material was not under consideration for reusable rockets, but in today\u2019s update, he said, \u201cSometimes carbon composites get a tough rap because they\u2019re expensive to manufacture and slow to produce. Not the case. We\u2019re gonna do this fast.\u201d<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" aria-describedby=\"caption-attachment-82376\" class=\"size-full wp-image-82376\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/11\/NSF-2021-12-02-13-24-41-677.jpg\" alt=\"\" width=\"2025\" height=\"1136\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/11\/NSF-2021-12-02-13-24-41-677.jpg 2025w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/11\/NSF-2021-12-02-13-24-41-677-350x196.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/11\/NSF-2021-12-02-13-24-41-677-624x350.jpg 624w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/11\/NSF-2021-12-02-13-24-41-677-768x431.jpg 768w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/11\/NSF-2021-12-02-13-24-41-677-1920x1077.jpg 1920w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/11\/NSF-2021-12-02-13-24-41-677-1170x656.jpg 1170w\" sizes=\"(max-width: 2025px) 100vw, 2025px\"><\/p>\n<p id=\"caption-attachment-82376\" class=\"wp-caption-text\">Seven Archimedes engines push the first stage of Neutron uphill. (Credit: Rocket Lab)<\/p>\n<p>Beck went on to say that the plan is to use automated fiber placement. \u201c3-D printing really changed the game when it came to rapid manufacture. With metallic 3-D printing, we measure the speed in millimeters per minute. With automated fiber placement, you measure the speed in meters per minute.\u201d<\/p>\n<p>\u201cWe have already shown with Electron that carbon composites are an ideal material for an orbital rocket,\u201d said Beck. \u201cNow, thanks to Neutron, it\u2019s gonna really come into its own as a rocket material of the future.\u201d<\/p>\n<p>Back further noted that prototype tanks for Neutron\u2019s two stages are already being built and that the first hot-fire test of the new Archimedes engine is planned for 2022.&nbsp;<\/p>\n<p>Notably absent from the presentation was an estimate on the first launch date, which had previously been 2024. Also absent was mention of the Mid-Atlantic Regional Spaceport in Virginia which had been planned as the initial launch site for the vehicle.<\/p>\n<p>Instead, Beck mentioned a launch facility devoid of most equipment \u2013 as simple as possible.<\/p>\n<p>A switch away from Pad 0A at the Mid-Atlantic Regional Spaceport would make sense given Neutron\u2019s desire to use a very simple launch pad and its switch of propellants from RP-1 kerosene and liquid oxygen (the ground support equipment for which is already present at Pad 0A) to liquid methane and liquid oxygen.<\/p>\n<p><em>(Lead image: Neutron on its simple launch pad. Credit: Rocket Lab)<\/em><\/p>\n","protected":false},"excerpt":{"rendered":"<p>Rocket Lab has provided a significant update in the progress of their Neutron rocket, a vehicle aimed primarily at the small-scale interplanetary and low Earth orbit mega-constellation markets at first.&nbsp; Among the major updates announced by Rocket Lab CEO Peter Beck were a complete switch of propellants, a firm Return To Launch Site landing plan [&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":[8115,758,544],"class_list":["post-24777","post","type-post","status-publish","format-standard","hentry","category-news","tag-archimedes","tag-neutron","tag-rocket-lab"],"acf":[],"_links":{"self":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/24777"}],"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=24777"}],"version-history":[{"count":0,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/24777\/revisions"}],"wp:attachment":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media?parent=24777"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/categories?post=24777"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/tags?post=24777"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}