{"id":499,"date":"2022-11-30T19:45:46","date_gmt":"2022-11-30T19:45:46","guid":{"rendered":"https:\/\/public.ksc.nasa.gov\/kscsma\/?page_id=499"},"modified":"2023-02-24T15:46:33","modified_gmt":"2023-02-24T15:46:33","slug":"nasa-flight-termination-system-fts-design-requirements","status":"publish","type":"page","link":"https:\/\/public.ksc.nasa.gov\/kscsma\/nasa-flight-termination-system-fts-design-requirements\/","title":{"rendered":"NASA Flight Termination System (FTS) Design Requirements"},"content":{"rendered":"\n<div class=\"wp-block-cover alignfull\" style=\"min-height:220px;aspect-ratio:unset;\"><span aria-hidden=\"true\" class=\"wp-block-cover__background has-ast-global-color-8-background-color has-background-dim-30 has-background-dim\"><\/span><img loading=\"lazy\" decoding=\"async\" width=\"1920\" height=\"400\" class=\"wp-block-cover__image-background wp-image-55\" alt=\"KSC Safety &amp; Mission Assurance\" src=\"https:\/\/public.ksc.nasa.gov\/kscsma\/wp-content\/uploads\/sites\/12\/2022\/10\/SMAhero1.jpg\" data-object-fit=\"cover\" \/><div class=\"wp-block-cover__inner-container is-layout-flow wp-block-cover-is-layout-flow\">\n<div class=\"wp-block-uagb-advanced-heading uagb-block-fbabaaa6 advgb-block-fbabaaa6\"><h1 class=\"uagb-heading-text\">NASA Flight Termination System (FTS) Design Requirements<\/h1><\/div>\n<\/div><\/div>\n\n\n\n<p><\/p>\n\n\n\n<h4 class=\"alignwide wp-block-heading\"><strong>FTS Design<\/strong><\/h4>\n\n\n\n<p>&#8211; FTS must render each power stage and \/ or any other propulsion system, including any that are part of a payload, non-propulsive<br>&#8211; If flight analysis determines the public is not endangered, an FTS may not be required<\/p>\n\n\n\n<p><strong>Good FTS Design Features include:<\/strong><br>&#8211; Redundancy<br>&#8211; Physical separation of redundant strings<br>&#8211; Independence from other vehicle systems<br>&#8211; Inadvertent separation destruct system when solid rocket motors used<br>&#8211; Both engine shutdown and destruct capability on liquid fueled vehicles<br>&#8211; Feathers that allow complete and thorough (end-to-end) testing<br><strong>Test Requirements for approval of FTS<\/strong><br>&#8211; Component level: Qualification, acceptance and lot testing<br>&#8211; System level: Pre-launch confidence tests and end-to-end verification<br>&#8211; Typical components of an airbourne FTS<\/p>\n\n\n\n<figure class=\"wp-block-image aligncenter size-large is-resized\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/public.ksc.nasa.gov\/kscsma\/wp-content\/uploads\/sites\/12\/2023\/02\/FTS-Design-1024x520.png\" alt=\"FTS Design\" class=\"wp-image-656\" width=\"710\" height=\"359\" \/><\/figure>\n\n\n\n<p>FTS Ground Systems consist of redundant UHF transmitters capable of sending command destruct signals<br>FTS reliability goal: 0.999 @ 95% confidence<br>Considerations during design \u2013 all these directly influence Ec<br><strong>Reliability<\/strong> \u2013 Hardware \/ software failure rates and redundancy | <strong>Propellants<\/strong> \u2013 Affects blast and toxic analyses and ground hazards | <strong>Trajectories<\/strong> \u2013 Affects \u201cat risk\u201d population | <strong>Range selection<\/strong> \u2013 Affects ground, sea and air hazard zones<\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p>FTS Design &#8211; FTS must render each power stage and \/ or any other propulsion system, including any that are part of a payload, non-propulsive&#8211; If flight analysis determines the public is not endangered, an FTS may not be required Good FTS Design Features include:&#8211; Redundancy&#8211; Physical separation of redundant strings&#8211; Independence from other vehicle [&hellip;]<\/p>\n","protected":false},"author":42,"featured_media":0,"parent":0,"menu_order":0,"comment_status":"closed","ping_status":"closed","template":"","meta":{"_uag_custom_page_level_css":"","_lmt_disableupdate":"","_lmt_disable":"","advgb_blocks_editor_width":"","advgb_blocks_columns_visual_guide":"","site-sidebar-layout":"no-sidebar","site-content-layout":"page-builder","ast-site-content-layout":"default","site-content-style":"default","site-sidebar-style":"default","ast-global-header-display":"","ast-banner-title-visibility":"","ast-main-header-display":"","ast-hfb-above-header-display":"","ast-hfb-below-header-display":"","ast-hfb-mobile-header-display":"","site-post-title":"disabled","ast-breadcrumbs-content":"","ast-featured-img":"","footer-sml-layout":"","ast-disable-related-posts":"","theme-transparent-header-meta":"","adv-header-id-meta":"","stick-header-meta":"","header-above-stick-meta":"","header-main-stick-meta":"","header-below-stick-meta":"","astra-migrate-meta-layouts":"default","ast-page-background-enabled":"default","ast-page-background-meta":{"desktop":{"background-color":"var(--ast-global-color-4)","background-image":"","background-repeat":"repeat","background-position":"center center","background-size":"auto","background-attachment":"scroll","background-type":"","background-media":"","overlay-type":"","overlay-color":"","overlay-opacity":"","overlay-gradient":""},"tablet":{"background-color":"","background-image":"","background-repeat":"repeat","background-position":"center center","background-size":"auto","background-attachment":"scroll","background-type":"","background-media":"","overlay-type":"","overlay-color":"","overlay-opacity":"","overlay-gradient":""},"mobile":{"background-color":"","background-image":"","background-repeat":"repeat","background-position":"center center","background-size":"auto","background-attachment":"scroll","background-type":"","background-media":"","overlay-type":"","overlay-color":"","overlay-opacity":"","overlay-gradient":""}},"ast-content-background-meta":{"desktop":{"background-color":"var(--ast-global-color-5)","background-image":"","background-repeat":"repeat","background-position":"center center","background-size":"auto","background-attachment":"scroll","background-type":"","background-media":"","overlay-type":"","overlay-color":"","overlay-opacity":"","overlay-gradient":""},"tablet":{"background-color":"var(--ast-global-color-5)","background-image":"","background-repeat":"repeat","background-position":"center center","background-size":"auto","background-attachment":"scroll","background-type":"","background-media":"","overlay-type":"","overlay-color":"","overlay-opacity":"","overlay-gradient":""},"mobile":{"background-color":"var(--ast-global-color-5)","background-image":"","background-repeat":"repeat","background-position":"center center","background-size":"auto","background-attachment":"scroll","background-type":"","background-media":"","overlay-type":"","overlay-color":"","overlay-opacity":"","overlay-gradient":""}},"footnotes":""},"class_list":["post-499","page","type-page","status-publish","hentry"],"pp_statuses_selecting_workflow":false,"pp_workflow_action":"current","pp_status_selection":"publish","pp_force_visibility":null,"pp_subpost_visibility":null,"pp_inherited_force_visibility":null,"pp_inherited_subpost_visibility":null,"pp_post_mime_type":"","uagb_featured_image_src":{"full":false,"thumbnail":false,"medium":false,"medium_large":false,"large":false,"1536x1536":false,"2048x2048":false,"gform-image-choice-sm":false,"gform-image-choice-md":false,"gform-image-choice-lg":false},"uagb_author_info":{"display_name":"Jenifer Kalis","author_link":"https:\/\/public.ksc.nasa.gov\/kscsma\/author\/jkalis\/"},"uagb_comment_info":0,"uagb_excerpt":"FTS Design &#8211; FTS must render each power stage and \/ or any other propulsion system, including any that are part of a payload, non-propulsive&#8211; If flight analysis determines the public is not endangered, an FTS may not be required Good FTS Design Features include:&#8211; Redundancy&#8211; Physical separation of redundant strings&#8211; Independence from other vehicle&hellip;","coauthors":[],"author_meta":{"author_link":"https:\/\/public.ksc.nasa.gov\/kscsma\/author\/jkalis\/","display_name":"Jenifer Kalis"},"relative_dates":{"created":"Posted 4 years ago","modified":"Updated 4 years ago"},"absolute_dates":{"created":"Posted on November 30, 2022","modified":"Updated on February 24, 2023"},"absolute_dates_time":{"created":"Posted on November 30, 2022 7:45 pm","modified":"Updated on February 24, 2023 3:46 pm"},"featured_img_caption":"","featured_img":false,"series_order":"","_links":{"self":[{"href":"https:\/\/public.ksc.nasa.gov\/kscsma\/wp-json\/wp\/v2\/pages\/499","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/public.ksc.nasa.gov\/kscsma\/wp-json\/wp\/v2\/pages"}],"about":[{"href":"https:\/\/public.ksc.nasa.gov\/kscsma\/wp-json\/wp\/v2\/types\/page"}],"author":[{"embeddable":true,"href":"https:\/\/public.ksc.nasa.gov\/kscsma\/wp-json\/wp\/v2\/users\/42"}],"replies":[{"embeddable":true,"href":"https:\/\/public.ksc.nasa.gov\/kscsma\/wp-json\/wp\/v2\/comments?post=499"}],"version-history":[{"count":4,"href":"https:\/\/public.ksc.nasa.gov\/kscsma\/wp-json\/wp\/v2\/pages\/499\/revisions"}],"predecessor-version":[{"id":660,"href":"https:\/\/public.ksc.nasa.gov\/kscsma\/wp-json\/wp\/v2\/pages\/499\/revisions\/660"}],"wp:attachment":[{"href":"https:\/\/public.ksc.nasa.gov\/kscsma\/wp-json\/wp\/v2\/media?parent=499"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}