{"id":2091,"date":"2017-01-12T12:00:00","date_gmt":"2017-01-12T12:00:00","guid":{"rendered":"http:\/\/wp.polot.net\/2024\/07\/13\/aircraft-engines-turbojets-in-france-part-21\/"},"modified":"2024-07-13T18:40:26","modified_gmt":"2024-07-13T16:40:26","slug":"aircraft-engines-turbojets-in-france-part-21","status":"publish","type":"post","link":"https:\/\/polot.net\/?p=2091&lang=en","title":{"rendered":"Aircraft Engines &#8211; Turbojets in France &#8211; Part 21"},"content":{"rendered":"<p>Krak\u00f3w 2017-01-12<\/p>\n<h2 id=\"Turbo-jets-in-France\"  >Turbo-jets in France<\/h2>\n<p><figure class=\"alignleft\">                    <img decoding=\"async\" data-src=\"https:\/\/images.polot.net\/a06a3a10338e9bddc1b3c9a9df17a0a58ba91eb3\" src=\"https:\/\/images.polot.net\/a06a3a10338e9bddc1b3c9a9df17a0a58ba91eb3\" alt=\"Atar 9. 2011 year. Photo by Karol Placha Hetman\" class=\"lazyload\" data-action=\"zoom\"><figcaption>Atar 9. 2011 year. Photo by Karol Placha Hetman<\/figcaption><\/figure>\n<h3 id=\"Snecma-Atar-9.-1955-year.\"  >Snecma Atar 9. 1955 year.<\/h3>\n<p>Work on the Atar 9 engine was successful. The engines powered several French-made combat aircraft: Etendard, Super Etendard, Mirage III, Mirage 5, Mirage 50, Mirage F1, Mirage IV.<\/p>\n<p>Atar 9 engine data: The single-flow, single-shaft motor received a 9-stage axial compressor. Compressor 5.2: 1 compression. Combustion chamber. 2-stage turbine. Afterburner. Length 5.90 m, diameter 1.00 m, weight 1,456 kg. 42.00 kN draft without afterburning and 58.90 kN with afterburning. Air flow through the engine 68 kg \/ s. fuel consumption 103 kg \/ (kN h) without afterburning and 207 kg \/ (kN h) with afterburning. The engine is started by compressed air generated by a starter (micro-turbine) located in a cone in front of the air inlet.<\/p>\n<p>Written by Karol Placha Hetman<\/p>\n","protected":false},"excerpt":{"rendered":"<p>Atar 9 engine data: The single-flow, single-shaft motor received a 9-stage axial compressor. Compressor 5.2: 1 compression. Combustion chamber. 2-stage turbine. Afterburner. Length 5.90 m, diameter 1.00 m, weight 1,456 kg. 42.00 kN draft without afterburning and 58.90 kN with afterburning. Air flow through the engine 68 kg \/ s. fuel consumption 103 kg \/ (kN h) without afterburning and 207 kg \/ (kN h) with afterburning. The engine is started by compressed air generated by a starter (micro-turbine) located in a cone in front of the air inlet.<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"closed","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[17],"tags":[],"class_list":["post-2091","post","type-post","status-publish","format-standard","hentry","category-articles"],"_links":{"self":[{"href":"https:\/\/polot.net\/index.php?rest_route=\/wp\/v2\/posts\/2091","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/polot.net\/index.php?rest_route=\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/polot.net\/index.php?rest_route=\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/polot.net\/index.php?rest_route=\/wp\/v2\/users\/2"}],"replies":[{"embeddable":true,"href":"https:\/\/polot.net\/index.php?rest_route=%2Fwp%2Fv2%2Fcomments&post=2091"}],"version-history":[{"count":1,"href":"https:\/\/polot.net\/index.php?rest_route=\/wp\/v2\/posts\/2091\/revisions"}],"predecessor-version":[{"id":2285,"href":"https:\/\/polot.net\/index.php?rest_route=\/wp\/v2\/posts\/2091\/revisions\/2285"}],"wp:attachment":[{"href":"https:\/\/polot.net\/index.php?rest_route=%2Fwp%2Fv2%2Fmedia&parent=2091"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/polot.net\/index.php?rest_route=%2Fwp%2Fv2%2Fcategories&post=2091"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/polot.net\/index.php?rest_route=%2Fwp%2Fv2%2Ftags&post=2091"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}