{"id":2353,"date":"2026-01-09T14:26:30","date_gmt":"2026-01-09T13:26:30","guid":{"rendered":"https:\/\/www.nickelcasting.com\/?page_id=2353"},"modified":"2026-03-28T16:00:52","modified_gmt":"2026-03-28T15:00:52","slug":"rene-41","status":"publish","type":"page","link":"https:\/\/www.nickelcasting.com\/es\/aleaciones-de-niquel\/rene-41\/","title":{"rendered":"Ren\u00e9 41"},"content":{"rendered":"<div data-elementor-type=\"wp-page\" data-elementor-id=\"2353\" class=\"elementor elementor-2353\" data-elementor-post-type=\"page\">\n\t\t\t\t<div class=\"elementor-element elementor-element-98f3dde e-flex e-con-boxed e-con e-parent\" data-id=\"98f3dde\" data-element_type=\"container\">\n\t\t\t\t\t<div class=\"e-con-inner\">\n\t\t\t\t<div class=\"elementor-element elementor-element-f0e5801 elementor-widget elementor-widget-html\" data-id=\"f0e5801\" data-element_type=\"widget\" data-widget_type=\"html.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t<link rel=\"stylesheet\" href=\"\/zicss\/nickel6.css\">\n\n<div class=\"product-detail-wrapper\">\n\n    <div class=\"breadcrumbs\">\n        <a href=\"\/es\/\">Inicio<\/a> \n        <span class=\"separator\">\/<\/span> \n        <a href=\"\/es\/aleaciones-de-niquel\/\">Aleaciones de n\u00edquel<\/a>\n        <span class=\"separator\">\/<\/span> \n        Ren\u00e9 41\n    <\/div>\n\n    <div class=\"prod-hero\">\n        <div class=\"prod-image-box\">\n            <img decoding=\"async\" src=\"http:\/\/www.nickelcasting.com\/wp-content\/uploads\/2026\/01\/nickel33.jpg\" alt=\"Superaleaci\u00f3n de n\u00edquel Rene 41\">\n        <\/div>\n        \n        <div class=\"prod-info-box\">\n            <h1>Ren\u00e9 41<\/h1>\n            <div class=\"prod-subtitle\">UNS N07041 | W.Nr. 2.4973 | Aleaci\u00f3n R-41<\/div>\n            \n            <p>\n                Ren\u00e9 41 es una superaleaci\u00f3n a base de n\u00edquel endurecible por envejecimiento capaz de mantener una resistencia excepcionalmente alta en el intervalo de temperaturas de 650\u00b0C a 980\u00b0C (1200\u00b0F a 1800\u00b0F). Ofrece una de las relaciones resistencia-peso m\u00e1s elevadas de todas las superaleaciones disponibles en esta gama de funcionamiento.\n            <\/p>\n\n            <ul class=\"key-specs-list\">\n                <li><strong>Formas comunes:<\/strong> Chapa, fleje, placa, barra redonda, alambre.<\/li>\n                <li><strong>Caracter\u00edstica clave:<\/strong> Resistencia extrema hasta 1800\u00b0F.<\/li>\n                <li><strong>Endurecimiento:<\/strong> Endurecido mediante titanio y aluminio.<\/li>\n                <li><strong>Corrosi\u00f3n:<\/strong> Excelente resistencia a la oxidaci\u00f3n a altas temperaturas.<\/li>\n            <\/ul>\n\n            <div class=\"action-area\">\n                <a href=\"\/es\/pongase-en-contacto-con\/\" class=\"quote-btn\">Solicitar presupuesto<\/a>\n                <a href=\"#\" class=\"download-btn\">Descargar hoja de datos<\/a>\n            <\/div>\n        <\/div>\n    <\/div>\n\n    <div class=\"section-head\">\u00bfPor qu\u00e9 elegir Ren\u00e9 41?<\/div>\n    <p>\n        Ren\u00e9 41 es el material de elecci\u00f3n cuando las superaleaciones est\u00e1ndar como <a href=\"https:\/\/www.nickelcasting.com\/ko\/%eb%8b%88%ec%bc%88-%ed%95%a9%ea%b8%88\/%ec%9d%b8%ec%bd%94%eb%84%ac-%eb%8b%88%ec%bc%88-%ed%95%a9%ea%b8%88\/inconel-718\/\">Inconel 718<\/a> o <a href=\"https:\/\/www.nickelcasting.com\/ko\/%eb%8b%88%ec%bc%88-%ed%95%a9%ea%b8%88\/waspaloy\/\">Waspaloy<\/a> alcanzan sus l\u00edmites de temperatura. Desarrollado originalmente por General Electric, est\u00e1 dise\u00f1ado para componentes que requieren la m\u00e1xima resistencia a la tracci\u00f3n y a la rotura por fluencia en las secciones m\u00e1s calientes de motores a reacci\u00f3n y sistemas de misiles.\n    <\/p>\n\n    <div class=\"feature-grid\">\n        <div class=\"feature-col\">\n            <h4>Resistencia a temperaturas extremas<\/h4>\n            <p>Retiene propiedades mec\u00e1nicas ultra-altas hasta 980\u00b0C (1800\u00b0F), haci\u00e9ndola superior a muchas otras aleaciones endurecidas por precipitaci\u00f3n.<\/p>\n        <\/div>\n        <div class=\"feature-col\">\n            <h4>Resistencia a la rotura por fluencia<\/h4>\n            <p>Excelente resistencia a la deformaci\u00f3n bajo carga a lo largo del tiempo a altas temperaturas, cr\u00edtica para los componentes giratorios de las turbinas.<\/p>\n        <\/div>\n        <div class=\"feature-col\">\n            <h4>Resistencia a la oxidaci\u00f3n<\/h4>\n            <p>El alto contenido en cromo y cobalto proporciona una buena resistencia a la oxidaci\u00f3n y a la corrosi\u00f3n en caliente en entornos de combusti\u00f3n.<\/p>\n        <\/div>\n    <\/div>\n\n    <div class=\"section-head\">Composici\u00f3n qu\u00edmica (%)<\/div>\n    <div class=\"data-table-wrap\">\n        <table class=\"tech-table\">\n            <thead>\n                <tr>\n                    <th>Elemento<\/th>\n                    <th>Contenido (%)<\/th>\n                <\/tr>\n            <\/thead>\n            <tbody>\n                <tr>\n                    <td><strong>N\u00edquel (Ni)<\/strong><\/td>\n                    <td>Saldo<\/td>\n                <\/tr>\n                <tr>\n                    <td><strong>Cromo (Cr)<\/strong><\/td>\n                    <td>18.0 - 20.0<\/td>\n                <\/tr>\n                <tr>\n                    <td><strong>Cobalto (Co)<\/strong><\/td>\n                    <td><strong>10.0 - 12.0<\/strong><\/td>\n                <\/tr>\n                <tr>\n                    <td><strong>Molibdeno (Mo)<\/strong><\/td>\n                    <td><strong>9.0 - 10.5<\/strong><\/td>\n                <\/tr>\n                <tr>\n                    <td><strong>Titanio (Ti)<\/strong><\/td>\n                    <td><strong>3.0 - 3.3<\/strong><\/td>\n                <\/tr>\n                <tr>\n                    <td><strong>Aluminio (Al)<\/strong><\/td>\n                    <td>1.4 - 1.6<\/td>\n                <\/tr>\n                 <tr>\n                    <td><strong>Hierro (Fe)<\/strong><\/td>\n                    <td>5,0 m\u00e1x.<\/td>\n                <\/tr>\n            <\/tbody>\n        <\/table>\n        <p style=\"font-size:0.85rem; color:#666; margin-top:10px;\">*Nota: El alto contenido de Ti\/Al proporciona un endurecimiento por envejecimiento agresivo.<\/p>\n    <\/div>\n\n    <div class=\"section-head\">Especificaciones est\u00e1ndar<\/div>\n    <div class=\"data-table-wrap\">\n        <table class=\"tech-table\">\n            <thead>\n                <tr>\n                    <th width=\"30%\">Forma del producto<\/th>\n                    <th>Normas (AMS)<\/th>\n                <\/tr>\n            <\/thead>\n            <tbody>\n                <tr>\n                    <td><strong>Chapa, tira, placa<\/strong><\/td>\n                    <td>AMS 5545<\/td>\n                <\/tr>\n                <tr>\n                    <td><strong>Barras, piezas forjadas, anillos<\/strong><\/td>\n                    <td>AMS 5712, AMS 5713<\/td>\n                <\/tr>\n                <tr>\n                    <td><strong>Alambre (soldadura)<\/strong><\/td>\n                    <td>AMS 5800<\/td>\n                <\/tr>\n            <\/tbody>\n        <\/table>\n    <\/div>\n\n    \n    \n    <div class=\"section-head\">Formularios disponibles para Ren\u00e9 41<\/div>\n    <p style=\"margin-bottom: 25px;\">\n        Para satisfacer las exigencias operativas extremas de los sectores aeroespacial y de defensa, suministramos Ren\u00e9 41 en formas de molino totalmente certificadas, dise\u00f1adas para fabricar piezas de motores rotativos y fuselajes estructurales de alta temperatura.\n    <\/p>\n\n    <div class=\"forms-grid\">\n        <a href=\"\/es\/product-forms\/plate-and-sheet\/\" class=\"form-card-link\">\n            <div class=\"form-card-icon\">\ud83d\udd32<\/div>\n            <div class=\"form-card-content\">\n                <h4>Chapa, fleje y placa<\/h4>\n                <p>Material laminado plano de alta resistencia esencial para la fabricaci\u00f3n de escudos t\u00e9rmicos, componentes de postcombusti\u00f3n y revestimientos estructurales de misiles y cohetes.<\/p>\n            <\/div>\n        <\/a>\n\n        <a href=\"\/es\/product-forms\/bar\/\" class=\"form-card-link\">\n            <div class=\"form-card-icon\">\ud83d\udccf<\/div>\n            <div class=\"form-card-content\">\n                <h4>Bar &amp; Rod<\/h4>\n                <p>Se suministra para el mecanizado CNC de precisi\u00f3n de fijaciones cr\u00edticas de turbinas de gas, atornillado estructural y hardware especializado de motores de alta temperatura.<\/p>\n            <\/div>\n        <\/a>\n\n        <a href=\"\/es\/product-forms\/forgings\/\" class=\"form-card-link\">\n            <div class=\"form-card-icon\">\ud83d\udd28<\/div>\n            <div class=\"form-card-content\">\n                <h4>Forjas y anillos<\/h4>\n                <p>Bloques forjados a medida y anillos laminados sin soldadura que sirven de base para ruedas de turbina sometidas a grandes esfuerzos y tabiques de secci\u00f3n caliente.<\/p>\n            <\/div>\n        <\/a>\n\n        <a href=\"\/es\/product-forms\/wire\/\" class=\"form-card-link\">\n            <div class=\"form-card-icon\">\ud83e\uddf5<\/div>\n            <div class=\"form-card-content\">\n                <h4>Alambre<\/h4>\n                <p>Material de alambre especializado utilizado para fabricar muelles de alta temperatura extrema que funcionan en entornos que superan los l\u00edmites del Inconel X-750.<\/p>\n            <\/div>\n        <\/a>\n    <\/div>\n    <div class=\"section-head\">Propiedades mec\u00e1nicas (envejecimiento t\u00edpico)<\/div>\n    <div class=\"data-table-wrap\">\n        <table class=\"tech-table\">\n            <thead>\n                <tr>\n                    <th>Propiedad<\/th>\n                    <th>Temperatura ambiente<\/th>\n                    <th>A 760\u00b0C (1400\u00b0F)<\/th>\n                <\/tr>\n            <\/thead>\n            <tbody>\n                <tr>\n                    <td><strong>Resistencia a la tracci\u00f3n<\/strong><\/td>\n                    <td>206 ksi (1420 MPa)<\/td>\n                    <td>165 ksi (1135 MPa)<\/td>\n                <\/tr>\n                <tr>\n                    <td><strong>L\u00edmite el\u00e1stico (0,2%)<\/strong><\/td>\n                    <td>154 ksi (1060 MPa)<\/td>\n                    <td>135 ksi (930 MPa)<\/td>\n                <\/tr>\n                <tr>\n                    <td><strong>Alargamiento<\/strong><\/td>\n                    <td>14%<\/td>\n                    <td>16%<\/td>\n                <\/tr>\n                 <tr>\n                    <td><strong>Dureza (Rockwell C)<\/strong><\/td>\n                    <td>35 - 45 HRC<\/td>\n                    <td>--<\/td>\n                <\/tr>\n            <\/tbody>\n        <\/table>\n        <p style=\"font-size:0.85rem; color:#666; margin-top:10px;\">*Nota: Las propiedades indicadas son las t\u00edpicas de un material tratado por disoluci\u00f3n y envejecido.<\/p>\n    <\/div>\n\n    <div class=\"section-head\">Aplicaciones t\u00edpicas<\/div>\n    <div class=\"app-list\">\n        <div class=\"app-card\">\n            <h4>Componentes de motores a reacci\u00f3n<\/h4>\n            <p>\u00c1labes de turbina, ruedas, piezas de postcombusti\u00f3n y tabiques de tobera expuestos a combusti\u00f3n directa.<\/p>\n        <\/div>\n        <div class=\"app-card\">\n            <h4>Estructuras de misiles<\/h4>\n            <p>Componentes aerodin\u00e1micos en caliente y revestimientos estructurales para misiles y cohetes de alta velocidad.<\/p>\n        <\/div>\n        <div class=\"app-card\">\n            <h4>Nave espacial<\/h4>\n            <p>Escudos t\u00e9rmicos de reentrada y pernos para c\u00e1psulas espaciales tripuladas (uso hist\u00f3rico en el Proyecto Mercury).<\/p>\n        <\/div>\n        <div class=\"app-card\">\n            <h4>Muelles<\/h4>\n            <p>Resortes de alta temperatura que funcionan en entornos demasiado calientes para <a href=\"https:\/\/www.nickelcasting.com\/ko\/%eb%8b%88%ec%bc%88-%ed%95%a9%ea%b8%88\/%ec%9d%b8%ec%bd%94%eb%84%ac-%eb%8b%88%ec%bc%88-%ed%95%a9%ea%b8%88\/inconel-x-750\/\">Inconel X-750<\/a>.<\/p>\n        <\/div>\n    <\/div>\n\n    <div id=\"quote-form\" style=\"margin-top: 60px; background: #f1f4f6; padding: 40px; border-radius: 5px; text-align: center;\">\n        <h3 style=\"color: var(--prod-primary); margin-top: 0;\">\u00bfNecesita Ren\u00e9 41 Hoja o Barra?<\/h3>\n        <p style=\"max-width: 600px; margin: 0 auto 20px;\">\n            Suministramos Ren\u00e9 41 de alto rendimiento en chapa, placa y barra.\n            Incluye certificaci\u00f3n aeroespacial completa (AMS 5545 \/ 5712).\n        <\/p>\n        <a href=\"\/es\/pongase-en-contacto-con\/\" class=\"quote-btn\">Presupuesto r\u00e1pido<\/a>\n    <\/div>\n\n<\/div>\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<\/div>","protected":false},"excerpt":{"rendered":"<p>Home \/ Nickel Alloys \/ Ren\u00e9 41 Ren\u00e9 41 UNS N07041 | W.Nr. 2.4973 | Alloy R-41 Ren\u00e9 41 is an age-hardenable nickel-based superalloy capable of maintaining exceptionally high strength in the temperature range of 1200\u00b0F to 1800\u00b0F (650\u00b0C to 980\u00b0C). It offers one of the highest strength-to-weight ratios of any superalloy available in this [&hellip;]<\/p>","protected":false},"author":1,"featured_media":0,"parent":1831,"menu_order":0,"comment_status":"closed","ping_status":"closed","template":"elementor_theme","meta":{"_uag_custom_page_level_css":"","site-sidebar-layout":"no-sidebar","site-content-layout":"page-builder","ast-site-content-layout":"full-width-container","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":"","ast-breadcrumbs-content":"","ast-featured-img":"disabled","footer-sml-layout":"","theme-transparent-header-meta":"default","adv-header-id-meta":"","stick-header-meta":"","header-above-stick-meta":"","header-main-stick-meta":"","header-below-stick-meta":"","astra-migrate-meta-layouts":"set","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 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center","background-size":"auto","background-attachment":"scroll","background-type":"","background-media":"","overlay-type":"","overlay-color":"","overlay-opacity":"","overlay-gradient":""}},"footnotes":""},"class_list":["post-2353","page","type-page","status-publish","hentry"],"spectra_custom_meta":{"_edit_lock":["1774710052:1"],"_edit_last":["1"],"rank_math_internal_links_processed":["1"],"rank_math_seo_score":["82"],"rank_math_description":["Rene 41 is a high-strength, heat-resistant superalloy used in aerospace and turbine engine components."],"rank_math_focus_keyword":["rene 41"],"_wp_page_template":["elementor_theme"],"site-sidebar-layout":["no-sidebar"],"ast-site-content-layout":["full-width-container"],"site-content-style":["default"],"site-sidebar-style":["default"],"theme-transparent-header-meta":["default"],"_elementor_edit_mode":["builder"],"_astra_content_layout_flag":["disabled"],"ast-title-bar-display":["disabled"],"ast-featured-img":["disabled"],"site-content-layout":["page-builder"],"_elementor_template_type":["wp-page"],"_elementor_version":["3.33.2"],"_elementor_pro_version":["3.32.3"],"_elementor_data":["[{\"id\":\"98f3dde\",\"elType\":\"container\",\"settings\":{\"flex_direction\":\"column\",\"display_condition_list\":[{\"display_condition_login_status\":\"subscriber\",\"_id\":\"e9a33d6\"}]},\"elements\":[{\"id\":\"f0e5801\",\"elType\":\"widget\",\"settings\":{\"html\":\"<link rel=\\\"stylesheet\\\" href=\\\"\\\/zicss\\\/nickel6.css\\\">\\n\\n<div class=\\\"product-detail-wrapper\\\">\\n\\n    <div class=\\\"breadcrumbs\\\">\\n        <a href=\\\"\\\/\\\">Home<\\\/a> \\n        <span class=\\\"separator\\\">\\\/<\\\/span> \\n        <a href=\\\"\\\/nickel-alloys\\\/\\\">Nickel Alloys<\\\/a>\\n        <span class=\\\"separator\\\">\\\/<\\\/span> \\n        Ren\\u00e9 41\\n    <\\\/div>\\n\\n    <div class=\\\"prod-hero\\\">\\n        <div class=\\\"prod-image-box\\\">\\n            <img src=\\\"http:\\\/\\\/www.nickelcasting.com\\\/wp-content\\\/uploads\\\/2026\\\/01\\\/nickel33.jpg\\\" alt=\\\"Rene 41 Nickel Superalloy\\\">\\n        <\\\/div>\\n        \\n        <div class=\\\"prod-info-box\\\">\\n            <h1>Ren\\u00e9 41<\\\/h1>\\n            <div class=\\\"prod-subtitle\\\">UNS N07041 | W.Nr. 2.4973 | Alloy R-41<\\\/div>\\n            \\n            <p>\\n                Ren\\u00e9 41 is an age-hardenable nickel-based superalloy capable of maintaining exceptionally high strength in the temperature range of 1200\\u00b0F to 1800\\u00b0F (650\\u00b0C to 980\\u00b0C). It offers one of the highest strength-to-weight ratios of any superalloy available in this operating range.\\n            <\\\/p>\\n\\n            <ul class=\\\"key-specs-list\\\">\\n                <li><strong>Common Forms:<\\\/strong> Sheet, Strip, Plate, Round Bar, Wire.<\\\/li>\\n                <li><strong>Key Feature:<\\\/strong> Extreme strength up to 1800\\u00b0F.<\\\/li>\\n                <li><strong>Hardening:<\\\/strong> Age-hardened via Titanium and Aluminum.<\\\/li>\\n                <li><strong>Corrosion:<\\\/strong> Excellent oxidation resistance at high heat.<\\\/li>\\n            <\\\/ul>\\n\\n            <div class=\\\"action-area\\\">\\n                <a href=\\\"\\\/contact\\\/\\\" class=\\\"quote-btn\\\">Request a Quote<\\\/a>\\n                <a href=\\\"#\\\" class=\\\"download-btn\\\">Download Datasheet<\\\/a>\\n            <\\\/div>\\n        <\\\/div>\\n    <\\\/div>\\n\\n    <div class=\\\"section-head\\\">Why Choose Ren\\u00e9 41?<\\\/div>\\n    <p>\\n        Ren\\u00e9 41 is the material of choice when standard superalloys like Inconel 718 or Waspaloy reach their temperature limits. Originally developed by General Electric, it is designed for components that require maximum tensile strength and creep-rupture resistance in the hottest sections of jet engines and missile systems.\\n    <\\\/p>\\n\\n    <div class=\\\"feature-grid\\\">\\n        <div class=\\\"feature-col\\\">\\n            <h4>Extreme Temp Strength<\\\/h4>\\n            <p>Retains ultra-high mechanical properties up to 1800\\u00b0F (980\\u00b0C), making it superior to many other precipitation-hardened alloys.<\\\/p>\\n        <\\\/div>\\n        <div class=\\\"feature-col\\\">\\n            <h4>Creep-Rupture Resistance<\\\/h4>\\n            <p>Excellent resistance to deformation under load over time at high temperatures, critical for rotating turbine components.<\\\/p>\\n        <\\\/div>\\n        <div class=\\\"feature-col\\\">\\n            <h4>Oxidation Resistance<\\\/h4>\\n            <p>The high Chromium and Cobalt content provides good resistance to oxidation and hot corrosion in combustion environments.<\\\/p>\\n        <\\\/div>\\n    <\\\/div>\\n\\n    <div class=\\\"section-head\\\">Chemical Composition (%)<\\\/div>\\n    <div class=\\\"data-table-wrap\\\">\\n        <table class=\\\"tech-table\\\">\\n            <thead>\\n                <tr>\\n                    <th>Element<\\\/th>\\n                    <th>Content (%)<\\\/th>\\n                <\\\/tr>\\n            <\\\/thead>\\n            <tbody>\\n                <tr>\\n                    <td><strong>Nickel (Ni)<\\\/strong><\\\/td>\\n                    <td>Balance<\\\/td>\\n                <\\\/tr>\\n                <tr>\\n                    <td><strong>Chromium (Cr)<\\\/strong><\\\/td>\\n                    <td>18.0 - 20.0<\\\/td>\\n                <\\\/tr>\\n                <tr>\\n                    <td><strong>Cobalt (Co)<\\\/strong><\\\/td>\\n                    <td><strong>10.0 - 12.0<\\\/strong><\\\/td>\\n                <\\\/tr>\\n                <tr>\\n                    <td><strong>Molybdenum (Mo)<\\\/strong><\\\/td>\\n                    <td><strong>9.0 - 10.5<\\\/strong><\\\/td>\\n                <\\\/tr>\\n                <tr>\\n                    <td><strong>Titanium (Ti)<\\\/strong><\\\/td>\\n                    <td><strong>3.0 - 3.3<\\\/strong><\\\/td>\\n                <\\\/tr>\\n                <tr>\\n                    <td><strong>Aluminum (Al)<\\\/strong><\\\/td>\\n                    <td>1.4 - 1.6<\\\/td>\\n                <\\\/tr>\\n                 <tr>\\n                    <td><strong>Iron (Fe)<\\\/strong><\\\/td>\\n                    <td>5.0 max<\\\/td>\\n                <\\\/tr>\\n            <\\\/tbody>\\n        <\\\/table>\\n        <p style=\\\"font-size:0.85rem; color:#666; margin-top:10px;\\\">*Note: High Ti\\\/Al content provides aggressive age hardening.<\\\/p>\\n    <\\\/div>\\n\\n    <div class=\\\"section-head\\\">Standard Specifications<\\\/div>\\n    <div class=\\\"data-table-wrap\\\">\\n        <table class=\\\"tech-table\\\">\\n            <thead>\\n                <tr>\\n                    <th width=\\\"30%\\\">Product Form<\\\/th>\\n                    <th>Standards (AMS)<\\\/th>\\n                <\\\/tr>\\n            <\\\/thead>\\n            <tbody>\\n                <tr>\\n                    <td><strong>Sheet, Strip, Plate<\\\/strong><\\\/td>\\n                    <td>AMS 5545<\\\/td>\\n                <\\\/tr>\\n                <tr>\\n                    <td><strong>Bar, Forgings, Rings<\\\/strong><\\\/td>\\n                    <td>AMS 5712, AMS 5713<\\\/td>\\n                <\\\/tr>\\n                <tr>\\n                    <td><strong>Wire (Welding)<\\\/strong><\\\/td>\\n                    <td>AMS 5800<\\\/td>\\n                <\\\/tr>\\n            <\\\/tbody>\\n        <\\\/table>\\n    <\\\/div>\\n\\n    \\n    \\n    <div class=\\\"section-head\\\">Available Forms for Ren\\u00e9 41<\\\/div>\\n    <p style=\\\"margin-bottom: 25px;\\\">\\n        To meet the extreme operational demands of the aerospace and defense sectors, we supply Ren\\u00e9 41 in fully certified mill forms designed for fabricating high-temperature rotating engine parts and structural airframes.\\n    <\\\/p>\\n\\n    <div class=\\\"forms-grid\\\">\\n        <a href=\\\"\\\/product-forms\\\/plate-and-sheet\\\/\\\" class=\\\"form-card-link\\\">\\n            <div class=\\\"form-card-icon\\\">\\ud83d\\udd32<\\\/div>\\n            <div class=\\\"form-card-content\\\">\\n                <h4>Sheet, Strip & Plate<\\\/h4>\\n                <p>High-strength flat rolled stock essential for manufacturing heat shields, afterburner components, and structural skins for missiles and rockets.<\\\/p>\\n            <\\\/div>\\n        <\\\/a>\\n\\n        <a href=\\\"\\\/product-forms\\\/bar\\\/\\\" class=\\\"form-card-link\\\">\\n            <div class=\\\"form-card-icon\\\">\\ud83d\\udccf<\\\/div>\\n            <div class=\\\"form-card-content\\\">\\n                <h4>Bar & Rod<\\\/h4>\\n                <p>Supplied for precision CNC machining of critical gas turbine fasteners, structural bolting, and specialized high-temperature engine hardware.<\\\/p>\\n            <\\\/div>\\n        <\\\/a>\\n\\n        <a href=\\\"\\\/product-forms\\\/forgings\\\/\\\" class=\\\"form-card-link\\\">\\n            <div class=\\\"form-card-icon\\\">\\ud83d\\udd28<\\\/div>\\n            <div class=\\\"form-card-content\\\">\\n                <h4>Forgings & Rings<\\\/h4>\\n                <p>Custom forged blocks and seamless rolled rings serving as the foundation for highly stressed turbine wheels and hot-section partitions.<\\\/p>\\n            <\\\/div>\\n        <\\\/a>\\n\\n        <a href=\\\"\\\/product-forms\\\/wire\\\/\\\" class=\\\"form-card-link\\\">\\n            <div class=\\\"form-card-icon\\\">\\ud83e\\uddf5<\\\/div>\\n            <div class=\\\"form-card-content\\\">\\n                <h4>Wire<\\\/h4>\\n                <p>Specialized wire stock utilized for fabricating extreme high-temperature springs operating in environments that exceed the limits of Inconel X-750.<\\\/p>\\n            <\\\/div>\\n        <\\\/a>\\n    <\\\/div>\\n    <div class=\\\"section-head\\\">Mechanical Properties (Typical Aged)<\\\/div>\\n    <div class=\\\"data-table-wrap\\\">\\n        <table class=\\\"tech-table\\\">\\n            <thead>\\n                <tr>\\n                    <th>Property<\\\/th>\\n                    <th>Room Temp<\\\/th>\\n                    <th>At 1400\\u00b0F (760\\u00b0C)<\\\/th>\\n                <\\\/tr>\\n            <\\\/thead>\\n            <tbody>\\n                <tr>\\n                    <td><strong>Tensile Strength<\\\/strong><\\\/td>\\n                    <td>206 ksi (1420 MPa)<\\\/td>\\n                    <td>165 ksi (1135 MPa)<\\\/td>\\n                <\\\/tr>\\n                <tr>\\n                    <td><strong>Yield Strength (0.2%)<\\\/strong><\\\/td>\\n                    <td>154 ksi (1060 MPa)<\\\/td>\\n                    <td>135 ksi (930 MPa)<\\\/td>\\n                <\\\/tr>\\n                <tr>\\n                    <td><strong>Elongation<\\\/strong><\\\/td>\\n                    <td>14%<\\\/td>\\n                    <td>16%<\\\/td>\\n                <\\\/tr>\\n                 <tr>\\n                    <td><strong>Hardness (Rockwell C)<\\\/strong><\\\/td>\\n                    <td>35 - 45 HRC<\\\/td>\\n                    <td>--<\\\/td>\\n                <\\\/tr>\\n            <\\\/tbody>\\n        <\\\/table>\\n        <p style=\\\"font-size:0.85rem; color:#666; margin-top:10px;\\\">*Note: Properties shown are typical for solution treated and aged material.<\\\/p>\\n    <\\\/div>\\n\\n    <div class=\\\"section-head\\\">Typical Applications<\\\/div>\\n    <div class=\\\"app-list\\\">\\n        <div class=\\\"app-card\\\">\\n            <h4>Jet Engine Components<\\\/h4>\\n            <p>Turbine blades, wheels, afterburner parts, and nozzle partitions exposed to direct combustion.<\\\/p>\\n        <\\\/div>\\n        <div class=\\\"app-card\\\">\\n            <h4>Missile Structures<\\\/h4>\\n            <p>Hot airframe components and structural skins for high-speed missiles and rockets.<\\\/p>\\n        <\\\/div>\\n        <div class=\\\"app-card\\\">\\n            <h4>Spacecraft<\\\/h4>\\n            <p>Re-entry heat shields and bolting for manned space capsules (historical use in Project Mercury).<\\\/p>\\n        <\\\/div>\\n        <div class=\\\"app-card\\\">\\n            <h4>Springs<\\\/h4>\\n            <p>High-temperature springs operating in environments too hot for Inconel X-750.<\\\/p>\\n        <\\\/div>\\n    <\\\/div>\\n\\n    <div id=\\\"quote-form\\\" style=\\\"margin-top: 60px; background: #f1f4f6; padding: 40px; border-radius: 5px; text-align: center;\\\">\\n        <h3 style=\\\"color: var(--prod-primary); margin-top: 0;\\\">Need Ren\\u00e9 41 Sheet or Bar?<\\\/h3>\\n        <p style=\\\"max-width: 600px; margin: 0 auto 20px;\\\">\\n            We supply high-performance Ren\\u00e9 41 in sheet, plate, and bar.\\n            Full aerospace certification (AMS 5545 \\\/ 5712) included.\\n        <\\\/p>\\n        <a href=\\\"\\\/contact\\\/\\\" class=\\\"quote-btn\\\">Get a Quick Quote<\\\/a>\\n    <\\\/div>\\n\\n<\\\/div>\",\"display_condition_list\":[{\"display_condition_login_status\":\"subscriber\",\"_id\":\"e8ef6a1\"}]},\"elements\":[],\"widgetType\":\"html\"}],\"isInner\":false}]"],"rank_math_og_content_image":["a:2:{s:5:\"check\";s:32:\"fbf0d61b83bf3dfe7d2ae5d5b11df8db\";s:6:\"images\";a:1:{i:0;i:2343;}}"],"ilj_blacklistdefinition":["a:0:{}"],"ilj_linkdefinition":["a:1:{i:0;s:7:\"Rene 41\";}"],"astra-migrate-meta-layouts":["set"],"_elementor_page_settings":["a:0:{}"],"_elementor_controls_usage":["a:2:{s:4:\"html\";a:3:{s:5:\"count\";i:1;s:15:\"control_percent\";i:0;s:8:\"controls\";a:2:{s:7:\"content\";a:1:{s:13:\"section_title\";a:1:{s:4:\"html\";i:1;}}s:8:\"advanced\";a:1:{s:26:\"display_conditions_section\";a:1:{s:22:\"display_condition_list\";i:1;}}}}s:9:\"container\";a:3:{s:5:\"count\";i:1;s:15:\"control_percent\";i:0;s:8:\"controls\";a:2:{s:6:\"layout\";a:1:{s:24:\"section_layout_container\";a:1:{s:14:\"flex_direction\";i:1;}}s:8:\"advanced\";a:1:{s:26:\"display_conditions_section\";a:1:{s:22:\"display_condition_list\";i:1;}}}}}"],"_uag_page_assets":["a:9:{s:3:\"css\";s:263:\".uag-blocks-common-selector{z-index:var(--z-index-desktop) !important}@media (max-width: 976px){.uag-blocks-common-selector{z-index:var(--z-index-tablet) !important}}@media (max-width: 767px){.uag-blocks-common-selector{z-index:var(--z-index-mobile) !important}}\n\";s:2:\"js\";s:0:\"\";s:18:\"current_block_list\";a:8:{i:0;s:11:\"core\/search\";i:1;s:10:\"core\/group\";i:2;s:12:\"core\/heading\";i:3;s:17:\"core\/latest-posts\";i:4;s:20:\"core\/latest-comments\";i:5;s:13:\"core\/archives\";i:6;s:15:\"core\/categories\";i:7;s:10:\"core\/image\";}s:8:\"uag_flag\";b:0;s:11:\"uag_version\";s:10:\"1776419131\";s:6:\"gfonts\";a:0:{}s:10:\"gfonts_url\";s:0:\"\";s:12:\"gfonts_files\";a:0:{}s:14:\"uag_faq_layout\";b:0;}"],"_uag_css_file_name":["uag-css-2353.css"],"_elementor_page_assets":["a:1:{s:7:\"scripts\";a:1:{i:0;s:18:\"elementor-frontend\";}}"],"_elementor_css":["a:6:{s:4:\"time\";i:1776528732;s:5:\"fonts\";a:0:{}s:5:\"icons\";a:0:{}s:20:\"dynamic_elements_ids\";a:0:{}s:6:\"status\";s:4:\"file\";i:0;s:0:\"\";}"],"_elementor_element_cache":["{\"timeout\":1776618732,\"value\":{\"content\":\"<div class=\\\"elementor-element elementor-element-98f3dde e-flex e-con-boxed e-con e-parent\\\" data-id=\\\"98f3dde\\\" data-element_type=\\\"container\\\">\\n\\t\\t\\t\\t\\t<div class=\\\"e-con-inner\\\">\\n\\t\\t\\t\\t<div class=\\\"elementor-element elementor-element-f0e5801 elementor-widget elementor-widget-html\\\" data-id=\\\"f0e5801\\\" data-element_type=\\\"widget\\\" data-widget_type=\\\"html.default\\\">\\n\\t\\t\\t\\t<div class=\\\"elementor-widget-container\\\">\\n\\t\\t\\t\\t\\t<link rel=\\\"stylesheet\\\" href=\\\"\\\/zicss\\\/nickel6.css\\\">\\n\\n<div class=\\\"product-detail-wrapper\\\">\\n\\n    <div class=\\\"breadcrumbs\\\">\\n        <a href=\\\"\\\/\\\">Home<\\\/a> \\n        <span class=\\\"separator\\\">\\\/<\\\/span> \\n        <a href=\\\"\\\/nickel-alloys\\\/\\\">Nickel Alloys<\\\/a>\\n        <span class=\\\"separator\\\">\\\/<\\\/span> \\n        Ren\\u00e9 41\\n    <\\\/div>\\n\\n    <div class=\\\"prod-hero\\\">\\n        <div class=\\\"prod-image-box\\\">\\n            <img src=\\\"http:\\\/\\\/www.nickelcasting.com\\\/wp-content\\\/uploads\\\/2026\\\/01\\\/nickel33.jpg\\\" alt=\\\"Rene 41 Nickel Superalloy\\\">\\n        <\\\/div>\\n        \\n        <div class=\\\"prod-info-box\\\">\\n            <h1>Ren\\u00e9 41<\\\/h1>\\n            <div class=\\\"prod-subtitle\\\">UNS N07041 | W.Nr. 2.4973 | Alloy R-41<\\\/div>\\n            \\n            <p>\\n                Ren\\u00e9 41 is an age-hardenable nickel-based superalloy capable of maintaining exceptionally high strength in the temperature range of 1200\\u00b0F to 1800\\u00b0F (650\\u00b0C to 980\\u00b0C). It offers one of the highest strength-to-weight ratios of any superalloy available in this operating range.\\n            <\\\/p>\\n\\n            <ul class=\\\"key-specs-list\\\">\\n                <li><strong>Common Forms:<\\\/strong> Sheet, Strip, Plate, Round Bar, Wire.<\\\/li>\\n                <li><strong>Key Feature:<\\\/strong> Extreme strength up to 1800\\u00b0F.<\\\/li>\\n                <li><strong>Hardening:<\\\/strong> Age-hardened via Titanium and Aluminum.<\\\/li>\\n                <li><strong>Corrosion:<\\\/strong> Excellent oxidation resistance at high heat.<\\\/li>\\n            <\\\/ul>\\n\\n            <div class=\\\"action-area\\\">\\n                <a href=\\\"\\\/contact\\\/\\\" class=\\\"quote-btn\\\">Request a Quote<\\\/a>\\n                <a href=\\\"#\\\" class=\\\"download-btn\\\">Download Datasheet<\\\/a>\\n            <\\\/div>\\n        <\\\/div>\\n    <\\\/div>\\n\\n    <div class=\\\"section-head\\\">Why Choose Ren\\u00e9 41?<\\\/div>\\n    <p>\\n        Ren\\u00e9 41 is the material of choice when standard superalloys like Inconel 718 or Waspaloy reach their temperature limits. Originally developed by General Electric, it is designed for components that require maximum tensile strength and creep-rupture resistance in the hottest sections of jet engines and missile systems.\\n    <\\\/p>\\n\\n    <div class=\\\"feature-grid\\\">\\n        <div class=\\\"feature-col\\\">\\n            <h4>Extreme Temp Strength<\\\/h4>\\n            <p>Retains ultra-high mechanical properties up to 1800\\u00b0F (980\\u00b0C), making it superior to many other precipitation-hardened alloys.<\\\/p>\\n        <\\\/div>\\n        <div class=\\\"feature-col\\\">\\n            <h4>Creep-Rupture Resistance<\\\/h4>\\n            <p>Excellent resistance to deformation under load over time at high temperatures, critical for rotating turbine components.<\\\/p>\\n        <\\\/div>\\n        <div class=\\\"feature-col\\\">\\n            <h4>Oxidation Resistance<\\\/h4>\\n            <p>The high Chromium and Cobalt content provides good resistance to oxidation and hot corrosion in combustion environments.<\\\/p>\\n        <\\\/div>\\n    <\\\/div>\\n\\n    <div class=\\\"section-head\\\">Chemical Composition (%)<\\\/div>\\n    <div class=\\\"data-table-wrap\\\">\\n        <table class=\\\"tech-table\\\">\\n            <thead>\\n                <tr>\\n                    <th>Element<\\\/th>\\n                    <th>Content (%)<\\\/th>\\n                <\\\/tr>\\n            <\\\/thead>\\n            <tbody>\\n                <tr>\\n                    <td><strong>Nickel (Ni)<\\\/strong><\\\/td>\\n                    <td>Balance<\\\/td>\\n                <\\\/tr>\\n                <tr>\\n                    <td><strong>Chromium (Cr)<\\\/strong><\\\/td>\\n                    <td>18.0 - 20.0<\\\/td>\\n                <\\\/tr>\\n                <tr>\\n                    <td><strong>Cobalt (Co)<\\\/strong><\\\/td>\\n                    <td><strong>10.0 - 12.0<\\\/strong><\\\/td>\\n                <\\\/tr>\\n                <tr>\\n                    <td><strong>Molybdenum (Mo)<\\\/strong><\\\/td>\\n                    <td><strong>9.0 - 10.5<\\\/strong><\\\/td>\\n                <\\\/tr>\\n                <tr>\\n                    <td><strong>Titanium (Ti)<\\\/strong><\\\/td>\\n                    <td><strong>3.0 - 3.3<\\\/strong><\\\/td>\\n                <\\\/tr>\\n                <tr>\\n                    <td><strong>Aluminum (Al)<\\\/strong><\\\/td>\\n                    <td>1.4 - 1.6<\\\/td>\\n                <\\\/tr>\\n                 <tr>\\n                    <td><strong>Iron (Fe)<\\\/strong><\\\/td>\\n                    <td>5.0 max<\\\/td>\\n                <\\\/tr>\\n            <\\\/tbody>\\n        <\\\/table>\\n        <p style=\\\"font-size:0.85rem; color:#666; margin-top:10px;\\\">*Note: High Ti\\\/Al content provides aggressive age hardening.<\\\/p>\\n    <\\\/div>\\n\\n    <div class=\\\"section-head\\\">Standard Specifications<\\\/div>\\n    <div class=\\\"data-table-wrap\\\">\\n        <table class=\\\"tech-table\\\">\\n            <thead>\\n                <tr>\\n                    <th width=\\\"30%\\\">Product Form<\\\/th>\\n                    <th>Standards (AMS)<\\\/th>\\n                <\\\/tr>\\n            <\\\/thead>\\n            <tbody>\\n                <tr>\\n                    <td><strong>Sheet, Strip, Plate<\\\/strong><\\\/td>\\n                    <td>AMS 5545<\\\/td>\\n                <\\\/tr>\\n                <tr>\\n                    <td><strong>Bar, Forgings, Rings<\\\/strong><\\\/td>\\n                    <td>AMS 5712, AMS 5713<\\\/td>\\n                <\\\/tr>\\n                <tr>\\n                    <td><strong>Wire (Welding)<\\\/strong><\\\/td>\\n                    <td>AMS 5800<\\\/td>\\n                <\\\/tr>\\n            <\\\/tbody>\\n        <\\\/table>\\n    <\\\/div>\\n\\n    \\n    \\n    <div class=\\\"section-head\\\">Available Forms for Ren\\u00e9 41<\\\/div>\\n    <p style=\\\"margin-bottom: 25px;\\\">\\n        To meet the extreme operational demands of the aerospace and defense sectors, we supply Ren\\u00e9 41 in fully certified mill forms designed for fabricating high-temperature rotating engine parts and structural airframes.\\n    <\\\/p>\\n\\n    <div class=\\\"forms-grid\\\">\\n        <a href=\\\"\\\/product-forms\\\/plate-and-sheet\\\/\\\" class=\\\"form-card-link\\\">\\n            <div class=\\\"form-card-icon\\\">\\ud83d\\udd32<\\\/div>\\n            <div class=\\\"form-card-content\\\">\\n                <h4>Sheet, Strip & Plate<\\\/h4>\\n                <p>High-strength flat rolled stock essential for manufacturing heat shields, afterburner components, and structural skins for missiles and rockets.<\\\/p>\\n            <\\\/div>\\n        <\\\/a>\\n\\n        <a href=\\\"\\\/product-forms\\\/bar\\\/\\\" class=\\\"form-card-link\\\">\\n            <div class=\\\"form-card-icon\\\">\\ud83d\\udccf<\\\/div>\\n            <div class=\\\"form-card-content\\\">\\n                <h4>Bar & Rod<\\\/h4>\\n                <p>Supplied for precision CNC machining of critical gas turbine fasteners, structural bolting, and specialized high-temperature engine hardware.<\\\/p>\\n            <\\\/div>\\n        <\\\/a>\\n\\n        <a href=\\\"\\\/product-forms\\\/forgings\\\/\\\" class=\\\"form-card-link\\\">\\n            <div class=\\\"form-card-icon\\\">\\ud83d\\udd28<\\\/div>\\n            <div class=\\\"form-card-content\\\">\\n                <h4>Forgings & Rings<\\\/h4>\\n                <p>Custom forged blocks and seamless rolled rings serving as the foundation for highly stressed turbine wheels and hot-section partitions.<\\\/p>\\n            <\\\/div>\\n        <\\\/a>\\n\\n        <a href=\\\"\\\/product-forms\\\/wire\\\/\\\" class=\\\"form-card-link\\\">\\n            <div class=\\\"form-card-icon\\\">\\ud83e\\uddf5<\\\/div>\\n            <div class=\\\"form-card-content\\\">\\n                <h4>Wire<\\\/h4>\\n                <p>Specialized wire stock utilized for fabricating extreme high-temperature springs operating in environments that exceed the limits of Inconel X-750.<\\\/p>\\n            <\\\/div>\\n        <\\\/a>\\n    <\\\/div>\\n    <div class=\\\"section-head\\\">Mechanical Properties (Typical Aged)<\\\/div>\\n    <div class=\\\"data-table-wrap\\\">\\n        <table class=\\\"tech-table\\\">\\n            <thead>\\n                <tr>\\n                    <th>Property<\\\/th>\\n                    <th>Room Temp<\\\/th>\\n                    <th>At 1400\\u00b0F (760\\u00b0C)<\\\/th>\\n                <\\\/tr>\\n            <\\\/thead>\\n            <tbody>\\n                <tr>\\n                    <td><strong>Tensile Strength<\\\/strong><\\\/td>\\n                    <td>206 ksi (1420 MPa)<\\\/td>\\n                    <td>165 ksi (1135 MPa)<\\\/td>\\n                <\\\/tr>\\n                <tr>\\n                    <td><strong>Yield Strength (0.2%)<\\\/strong><\\\/td>\\n                    <td>154 ksi (1060 MPa)<\\\/td>\\n                    <td>135 ksi (930 MPa)<\\\/td>\\n                <\\\/tr>\\n                <tr>\\n                    <td><strong>Elongation<\\\/strong><\\\/td>\\n                    <td>14%<\\\/td>\\n                    <td>16%<\\\/td>\\n                <\\\/tr>\\n                 <tr>\\n                    <td><strong>Hardness (Rockwell C)<\\\/strong><\\\/td>\\n                    <td>35 - 45 HRC<\\\/td>\\n                    <td>--<\\\/td>\\n                <\\\/tr>\\n            <\\\/tbody>\\n        <\\\/table>\\n        <p style=\\\"font-size:0.85rem; color:#666; margin-top:10px;\\\">*Note: Properties shown are typical for solution treated and aged material.<\\\/p>\\n    <\\\/div>\\n\\n    <div class=\\\"section-head\\\">Typical Applications<\\\/div>\\n    <div class=\\\"app-list\\\">\\n        <div class=\\\"app-card\\\">\\n            <h4>Jet Engine Components<\\\/h4>\\n            <p>Turbine blades, wheels, afterburner parts, and nozzle partitions exposed to direct combustion.<\\\/p>\\n        <\\\/div>\\n        <div class=\\\"app-card\\\">\\n            <h4>Missile Structures<\\\/h4>\\n            <p>Hot airframe components and structural skins for high-speed missiles and rockets.<\\\/p>\\n        <\\\/div>\\n        <div class=\\\"app-card\\\">\\n            <h4>Spacecraft<\\\/h4>\\n            <p>Re-entry heat shields and bolting for manned space capsules (historical use in Project Mercury).<\\\/p>\\n        <\\\/div>\\n        <div class=\\\"app-card\\\">\\n            <h4>Springs<\\\/h4>\\n            <p>High-temperature springs operating in environments too hot for Inconel X-750.<\\\/p>\\n        <\\\/div>\\n    <\\\/div>\\n\\n    <div id=\\\"quote-form\\\" style=\\\"margin-top: 60px; background: #f1f4f6; padding: 40px; border-radius: 5px; text-align: center;\\\">\\n        <h3 style=\\\"color: var(--prod-primary); margin-top: 0;\\\">Need Ren\\u00e9 41 Sheet or Bar?<\\\/h3>\\n        <p style=\\\"max-width: 600px; margin: 0 auto 20px;\\\">\\n            We supply high-performance Ren\\u00e9 41 in sheet, plate, and bar.\\n            Full aerospace certification (AMS 5545 \\\/ 5712) included.\\n        <\\\/p>\\n        <a href=\\\"\\\/contact\\\/\\\" class=\\\"quote-btn\\\">Get a Quick Quote<\\\/a>\\n    <\\\/div>\\n\\n<\\\/div>\\t\\t\\t\\t<\\\/div>\\n\\t\\t\\t\\t<\\\/div>\\n\\t\\t\\t\\t\\t<\\\/div>\\n\\t\\t\\t\\t<\\\/div>\\n\\t\\t\",\"scripts\":[],\"styles\":[]}}"]},"uagb_featured_image_src":{"full":false,"thumbnail":false,"medium":false,"medium_large":false,"large":false,"1536x1536":false,"2048x2048":false,"trp-custom-language-flag":false},"uagb_author_info":{"display_name":"nickel","author_link":"https:\/\/www.nickelcasting.com\/es\/author\/nickel\/"},"uagb_comment_info":0,"uagb_excerpt":"Home \/ Nickel Alloys \/ Ren\u00e9 41 Ren\u00e9 41 UNS N07041 | W.Nr. 2.4973 | Alloy R-41 Ren\u00e9 41 is an age-hardenable nickel-based superalloy capable of maintaining exceptionally high strength in the temperature range of 1200\u00b0F to 1800\u00b0F (650\u00b0C to 980\u00b0C). It offers one of the highest strength-to-weight ratios of any superalloy available in this&hellip;","_links":{"self":[{"href":"https:\/\/www.nickelcasting.com\/es\/wp-json\/wp\/v2\/pages\/2353","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/www.nickelcasting.com\/es\/wp-json\/wp\/v2\/pages"}],"about":[{"href":"https:\/\/www.nickelcasting.com\/es\/wp-json\/wp\/v2\/types\/page"}],"author":[{"embeddable":true,"href":"https:\/\/www.nickelcasting.com\/es\/wp-json\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/www.nickelcasting.com\/es\/wp-json\/wp\/v2\/comments?post=2353"}],"version-history":[{"count":11,"href":"https:\/\/www.nickelcasting.com\/es\/wp-json\/wp\/v2\/pages\/2353\/revisions"}],"predecessor-version":[{"id":3461,"href":"https:\/\/www.nickelcasting.com\/es\/wp-json\/wp\/v2\/pages\/2353\/revisions\/3461"}],"up":[{"embeddable":true,"href":"https:\/\/www.nickelcasting.com\/es\/wp-json\/wp\/v2\/pages\/1831"}],"wp:attachment":[{"href":"https:\/\/www.nickelcasting.com\/es\/wp-json\/wp\/v2\/media?parent=2353"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}