{"id":561,"date":"2023-09-11T08:10:06","date_gmt":"2023-09-11T08:10:06","guid":{"rendered":"https:\/\/aerospace.technion.ac.il\/lab\/cdl\/?page_id=561"},"modified":"2025-03-27T14:26:34","modified_gmt":"2025-03-27T14:26:34","slug":"characterization-of-green-hypergolic-propellants-for-hybrid-rocket-applications","status":"publish","type":"page","link":"https:\/\/aerospace.technion.ac.il\/lab\/cdl\/characterization-of-green-hypergolic-propellants-for-hybrid-rocket-applications\/","title":{"rendered":"Characterization of Green Hypergolic Propellants for Hybrid Rocket Applications"},"content":{"rendered":"<p><span style=\"font-size: 18pt\">This project deals with the study of green, non-toxic hypergolic propellants for use in hybrid rockets. Before proceeding, an introduction to hybrid rocket motors and hypergolic propellants is needed.<\/span><\/p>\n<p><span style=\"font-size: 18pt\">Rockets run on combustion, which requires the presence of two classes of reactants: fuel and oxidizer. For rockets, the fuel and oxidizer are together called propellants. Based on the states of fuel and oxidizer, rockets are generally of three types. Solid rockets are those that use propellants in the solid state where they are intimately mixed and ignited together. Liquid rockets use propellants in the liquid states. And finally, hybrid rockets are those in which the fuel is in the solid state and the oxidizer is in the liquid state. Figure 1 below shows a schematic of a hybrid rocket engine.<\/span><\/p>\n","protected":false},"excerpt":{"rendered":"<p>This project deals with the study of green, non-toxic hypergolic propellants for use in hybrid rockets. Before proceeding, an introduction to hybrid rocket motors and hypergolic propellants is needed. Rockets run on combustion, which requires the presence of two classes of reactants: fuel and oxidizer. For rockets, the fuel and oxidizer are together called propellants. [&hellip;]<\/p>\n","protected":false},"author":3,"featured_media":0,"parent":0,"menu_order":0,"comment_status":"closed","ping_status":"closed","template":"page-flex.php","meta":{"_acf_changed":false,"inline_featured_image":false,"footnotes":""},"class_list":["post-561","page","type-page","status-publish","hentry"],"acf":[],"yoast_head":"<!-- This site is optimized with the Yoast SEO plugin v27.5 - https:\/\/yoast.com\/product\/yoast-seo-wordpress\/ -->\n<title>Characterization of Green Hypergolic Propellants for Hybrid Rocket Applications - Combustion and Diagnostics Laboratory<\/title>\n<meta name=\"robots\" content=\"index, follow, max-snippet:-1, max-image-preview:large, max-video-preview:-1\" \/>\n<link rel=\"canonical\" href=\"https:\/\/aerospace.technion.ac.il\/lab\/cdl\/characterization-of-green-hypergolic-propellants-for-hybrid-rocket-applications\/\" \/>\n<meta property=\"og:locale\" content=\"en_US\" \/>\n<meta property=\"og:type\" content=\"article\" \/>\n<meta property=\"og:title\" content=\"Characterization of Green Hypergolic Propellants for Hybrid Rocket Applications - Combustion and Diagnostics Laboratory\" \/>\n<meta property=\"og:description\" content=\"This project deals with the study of green, non-toxic hypergolic propellants for use in hybrid rockets. Before proceeding, an introduction to hybrid rocket motors and hypergolic propellants is needed. Rockets run on combustion, which requires the presence of two classes of reactants: fuel and oxidizer. For rockets, the fuel and oxidizer are together called propellants. 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