{"id":5722,"date":"2022-08-07T17:28:32","date_gmt":"2022-08-07T15:28:32","guid":{"rendered":"http:\/\/tst.minijets.org\/?page_id=5722"},"modified":"2022-10-26T16:46:08","modified_gmt":"2022-10-26T14:46:08","slug":"williams-fjx-2","status":"publish","type":"page","link":"https:\/\/minijets.org\/en\/300-500\/williams-fjx-2\/","title":{"rendered":"Williams FJX-2"},"content":{"rendered":"<p>The\u00a0Williams <strong>FJX-2<\/strong>\u00a0is a high-bypass-ratio turbofan engine that produces 700 pounds of thrust, yet weighs only 85-100 pounds, about one-fourth the weight of piston engine propulsion systems with similar capabilities.<\/p>\n\n\n\n<div class=\"wp-block-columns is-layout-flex wp-container-core-columns-is-layout-28f84493 wp-block-columns-is-layout-flex\">\n<div class=\"wp-block-column is-layout-flow wp-block-column-is-layout-flow\">\n<figure class=\"wp-block-image size-full\"><img loading=\"lazy\" decoding=\"async\" width=\"500\" height=\"354\" src=\"http:\/\/minijets.org\/wp-content\/uploads\/2022\/08\/Williams_FXJ2_01.jpg\" alt=\"Williams FJX-2\" class=\"wp-image-5725\" srcset=\"https:\/\/minijets.org\/wp-content\/uploads\/2022\/08\/Williams_FXJ2_01.jpg 500w, https:\/\/minijets.org\/wp-content\/uploads\/2022\/08\/Williams_FXJ2_01-300x212.jpg 300w, https:\/\/minijets.org\/wp-content\/uploads\/2022\/08\/Williams_FXJ2_01-18x12.jpg 18w\" sizes=\"auto, (max-width: 500px) 100vw, 500px\" \/><figcaption>Image Nasa : The FJX-2 turbofan engine in Glenn&#8217;s Propulsion Systems Lab (PSL) altitude test chamber.<\/figcaption><\/figure>\n<\/div>\n\n\n\n<div class=\"wp-block-column is-layout-flow wp-block-column-is-layout-flow\">\n<p>In 1996, Williams teamed with NASA to develop a smaller and lighte turbofan engine \u201dthe Williams FJX-2\u201d for general aviation. The General Aviation Propulsion (GAP) program is part of NASA&#8217;s Advanced General Aviation Transport Experiments (AGATE) program a joint NASA\/industry venture to revitalize general aviation. AGATE was born at the 1992 Oshkosh convention.<\/p>\n\n\n\n<p>To keep costs low, the FJX-2 team applied many lessons learned from research of automotive gas turbine engines. Emphasis was placed on simplifying design and reducing the number of parts. Low-cost design techniques and advanced automated manufacturing methods have led to the first turbine engine that is cost competitive with piston engines. While not as fuel efficient as today&#8217;s comparable piston-powered aircraft, new turbofan jets will have equivalent or lower takeoff-to-landing fuel consumption.<\/p>\n<\/div>\n<\/div>\n\n\n\n<p>The first FJX-2 turbofan engine was fully assembled on December 18, 1998, by Williams International in Walled Lake, Michigan, marking a major milestone in the GAP program. On&nbsp;<strong>December 22, 1998<\/strong>, the first operational test of the new FJX-2 engine was conducted in the Williams static test facility. The engine was then disassembled for inspection and found to be in excellent condition.<\/p>\n\n\n\n<div class=\"wp-block-columns is-layout-flex wp-container-core-columns-is-layout-28f84493 wp-block-columns-is-layout-flex\">\n<div class=\"wp-block-column is-layout-flow wp-block-column-is-layout-flow\">\n<figure class=\"wp-block-image size-full\"><img loading=\"lazy\" decoding=\"async\" width=\"500\" height=\"354\" src=\"http:\/\/minijets.org\/wp-content\/uploads\/2022\/08\/Williams_FXJ2_02.jpg\" alt=\"Williams FJX-2\" class=\"wp-image-5723\" srcset=\"https:\/\/minijets.org\/wp-content\/uploads\/2022\/08\/Williams_FXJ2_02.jpg 500w, https:\/\/minijets.org\/wp-content\/uploads\/2022\/08\/Williams_FXJ2_02-300x212.jpg 300w, https:\/\/minijets.org\/wp-content\/uploads\/2022\/08\/Williams_FXJ2_02-18x12.jpg 18w\" sizes=\"auto, (max-width: 500px) 100vw, 500px\" \/><figcaption>The FJX-2 Turbofan Engine Prior to the Initial test Run. Source : NASA\/CR\u20142008-215266<\/figcaption><\/figure>\n<\/div>\n\n\n\n<div class=\"wp-block-column is-layout-flow wp-block-column-is-layout-flow\">\n<figure class=\"wp-block-image size-full\"><img loading=\"lazy\" decoding=\"async\" width=\"500\" height=\"354\" src=\"http:\/\/minijets.org\/wp-content\/uploads\/2022\/08\/Williams_FXJ2_03.jpg\" alt=\"Williams FJX-2\" class=\"wp-image-5724\" srcset=\"https:\/\/minijets.org\/wp-content\/uploads\/2022\/08\/Williams_FXJ2_03.jpg 500w, https:\/\/minijets.org\/wp-content\/uploads\/2022\/08\/Williams_FXJ2_03-300x212.jpg 300w, https:\/\/minijets.org\/wp-content\/uploads\/2022\/08\/Williams_FXJ2_03-18x12.jpg 18w\" sizes=\"auto, (max-width: 500px) 100vw, 500px\" \/><figcaption>Mockup of the FJX-2 turbofan engine developed in the GAP program. Source : NASA<\/figcaption><\/figure>\n<\/div>\n<\/div>\n\n\n\n<h2 class=\"wp-block-heading\">Application<\/h2>\n\n\n        <div class=\"wp-block-getwid-custom-post-type custom-post-type-page has-layout-list\">\n            <div class=\"wp-block-getwid-custom-post-type__wrapper\">\n                \t\t\t\t\t\t\t\t<div class='wp-block-getwid-custom-post-type__post'>\n\t\t\t\t\t\t\t\t\t\n<div class=\"wp-block-getwid-custom-post-type__post-wrapper\">\n            <div class=\"wp-block-getwid-custom-post-type__post-thumbnail\">\n            <a href=\"https:\/\/minijets.org\/en\/300-500\/williams-fjx-2\/williams-v-jet-ii\/\"><img loading=\"lazy\" decoding=\"async\" width=\"2000\" height=\"1652\" src=\"https:\/\/minijets.org\/wp-content\/uploads\/2022\/08\/Williams_V-Jet_II_-_06.jpg\" class=\"attachment-post-thumbnail size-post-thumbnail wp-post-image\" alt=\"\" srcset=\"https:\/\/minijets.org\/wp-content\/uploads\/2022\/08\/Williams_V-Jet_II_-_06.jpg 2000w, https:\/\/minijets.org\/wp-content\/uploads\/2022\/08\/Williams_V-Jet_II_-_06-300x248.jpg 300w, https:\/\/minijets.org\/wp-content\/uploads\/2022\/08\/Williams_V-Jet_II_-_06-1024x846.jpg 1024w, https:\/\/minijets.org\/wp-content\/uploads\/2022\/08\/Williams_V-Jet_II_-_06-768x634.jpg 768w, https:\/\/minijets.org\/wp-content\/uploads\/2022\/08\/Williams_V-Jet_II_-_06-1536x1269.jpg 1536w, https:\/\/minijets.org\/wp-content\/uploads\/2022\/08\/Williams_V-Jet_II_-_06-15x12.jpg 15w\" sizes=\"auto, (max-width: 2000px) 100vw, 2000px\" \/><\/a>\n        <\/div>\n        <div class=\"wp-block-getwid-custom-post-type__content-wrapper\">\n        <div class=\"wp-block-getwid-custom-post-type__post-header\">\n            <h3 class=\"wp-block-getwid-custom-post-type__post-title\"><a href=\"https:\/\/minijets.org\/en\/300-500\/williams-fjx-2\/williams-v-jet-ii\/\">Williams V-Jet II<\/a><\/h3>        <\/div>\n        <div class=\"wp-block-getwid-custom-post-type__post-excerpt\"><p>Built by Scaled Composites under contract to William, the Williams V-JET II made its first flight on April 13, 1997 NASA&nbsp;has hard partnered with the general aviation industry in introducing the V-JET II, a turbofan-powered light aircraft designed for future flight testing. It was expected to revolutionize and revitalize general aviation with a safer, smoother, [&hellip;]<\/p>\n<\/div>\n    <\/div>\n<\/div>\n\t\t\t\t\t\t\t\t<\/div>\n\t\t\t\t\t\t\t            <\/div>\n\n                    <\/div>","protected":false},"excerpt":{"rendered":"<p>The\u00a0Williams FJX-2\u00a0is a high-bypass-ratio turbofan engine that produces 700 pounds of thrust, yet weighs only 85-100 pounds, about one-fourth the weight of piston engine propulsion systems with similar capabilities. In 1996, Williams teamed with NASA to develop a smaller and lighte turbofan engine \u201dthe Williams FJX-2\u201d for general aviation. The General Aviation Propulsion (GAP) program [&hellip;]<\/p>","protected":false},"author":1,"featured_media":5724,"parent":623,"menu_order":0,"comment_status":"closed","ping_status":"closed","template":"","meta":{"_acf_changed":false,"cybocfi_hide_featured_image":"","footnotes":""},"categories":[15],"tags":[],"planes-000-100":[],"class_list":["post-5722","page","type-page","status-publish","has-post-thumbnail","hentry","category-jet-engine-300-500"],"blocksy_meta":[],"acf":[],"_links":{"self":[{"href":"https:\/\/minijets.org\/en\/wp-json\/wp\/v2\/pages\/5722","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/minijets.org\/en\/wp-json\/wp\/v2\/pages"}],"about":[{"href":"https:\/\/minijets.org\/en\/wp-json\/wp\/v2\/types\/page"}],"author":[{"embeddable":true,"href":"https:\/\/minijets.org\/en\/wp-json\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/minijets.org\/en\/wp-json\/wp\/v2\/comments?post=5722"}],"version-history":[{"count":0,"href":"https:\/\/minijets.org\/en\/wp-json\/wp\/v2\/pages\/5722\/revisions"}],"up":[{"embeddable":true,"href":"https:\/\/minijets.org\/en\/wp-json\/wp\/v2\/pages\/623"}],"wp:featuredmedia":[{"embeddable":true,"href":"https:\/\/minijets.org\/en\/wp-json\/wp\/v2\/media\/5724"}],"wp:attachment":[{"href":"https:\/\/minijets.org\/en\/wp-json\/wp\/v2\/media?parent=5722"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/minijets.org\/en\/wp-json\/wp\/v2\/categories?post=5722"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/minijets.org\/en\/wp-json\/wp\/v2\/tags?post=5722"},{"taxonomy":"planes-000-100","embeddable":true,"href":"https:\/\/minijets.org\/en\/wp-json\/wp\/v2\/planes-000-100?post=5722"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}