{"id":4110,"date":"2025-06-24T08:21:51","date_gmt":"2025-06-24T05:21:51","guid":{"rendered":"https:\/\/www.defencemetal.com\/?p=4110"},"modified":"2026-09-17T23:07:42","modified_gmt":"2026-09-17T20:07:42","slug":"hastelloy-x-2-4665-uns-n06002-ams-5536-ams-5754-nickel-alloy","status":"publish","type":"post","link":"https:\/\/www.defencemetal.com\/index.php\/2025\/06\/24\/hastelloy-x-2-4665-uns-n06002-ams-5536-ams-5754-nickel-alloy\/","title":{"rendered":"Hastelloy X (2.4665 \/ UNS N06002) \u2014 AMS 5536 \/ AMS 5754 Nickel Alloy"},"content":{"rendered":"<p><!-- dm-urun-link --><\/p>\n<div style=\"border:1px solid #d7dfe4;border-left:3px solid #DD3333;background:#F7FAFB;padding:11px 15px;margin:0 0 20px;font-size:14px;line-height:1.55\"><strong style=\"color:#12303f\">We supply Hastelloy X.<\/strong> For dimensions, standard equivalents, stock and quotations, take a look at the <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/hastelloy-x\/\"><strong>Hastelloy X product page<\/strong><\/a>.<\/div>\n<p><!-- \/dm-urun-link --><\/p>\n<h3><b>Hastelloy X (UNS N06002): A Super Alloy Stable at High Temperatures<\/b><\/h3>\n<h3><b>Alloy Definition and Chemical Composition<\/b><\/h3>\n<p class=\"p3\"><span class=\"s2\">Hastelloy X<\/span> is known for its excellent <span class=\"s2\">oxidation resistance<\/span>, <span class=\"s2\">high temperature strength<\/span> and <span class=\"s2\">weldability<\/span> properties. It is a <span class=\"s2\"><a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/nickel-alloys\/\">nickel based<\/a> super alloy<\/span>. This material has been developed particularly in line with the demands of the aerospace, energy and petrochemical sectors.<\/p>\n<p class=\"p3\">Its chemical composition is approximately as follows:<\/p>\n<ul>\n<li class=\"p1\"><span class=\"s1\"><b>Nickel (Ni)<\/b><\/span>: 47.5 \u2013 61%<\/li>\n<li class=\"p1\"><span class=\"s1\"><b>Iron (Fe)<\/b><\/span>: 17 \u2013 20%<\/li>\n<li class=\"p1\"><span class=\"s1\"><b>Chromium (Cr)<\/b><\/span>: 20.5 \u2013 23%<\/li>\n<li class=\"p1\"><b>Molybdenum (Mo)<\/b><span class=\"s1\">: 8 \u2013 10%<\/span><\/li>\n<li class=\"p1\"><span class=\"s1\"><b>Cobalt (Co)<\/b><\/span>: Max. 1.0%<\/li>\n<li class=\"p1\"><b>Manganese, Silicon, Carbon, Aluminium, Titanium<\/b><span class=\"s1\">: In trace amounts<\/span><\/li>\n<\/ul>\n<p class=\"p3\">Thanks to this composition, at high temperatures <span class=\"s2\">up to 1100 \u00b0C<\/span> it can preserve its resistance to <span class=\"s2\">oxidation<\/span> and <span class=\"s2\">fracture<\/span>. In terms of microstructure it is <a href=\"https:\/\/en.wikipedia.org\/wiki\/%C3%96stenitik_paslanmaz_%C3%A7elik\"><span class=\"s2\">austenitic<\/span><\/a>, and grain boundary precipitation is at a minimum level. This in turn makes the alloy suitable for post-weld operations.<\/p>\n<hr>\n<h3><b>Hastelloy X <\/b><b>ASTM, AMS and International Standards<\/b><\/h3>\n<p class=\"p3\">The Hastelloy X alloy is made available commercially and industrially within the scope of the following specifications:<\/p>\n<ul>\n<li class=\"p1\"><span class=\"s1\"><b>ASTM B435<\/b><\/span> \u2013 Plate, sheet and strip<\/li>\n<li class=\"p1\"><span class=\"s1\"><b>ASTM B619 \/ B622<\/b><\/span> \u2013 Seamless and welded pipes<\/li>\n<li class=\"p1\"><span class=\"s1\"><b>ASTM B366<\/b><\/span> \u2013 Pipe fittings<\/li>\n<li class=\"p1\"><span class=\"s1\"><b>AMS 5536<\/b><\/span> \u2013 Aerospace grade sheet and plate<\/li>\n<li class=\"p1\"><span class=\"s1\"><b>AMS 5754<\/b><\/span> \u2013 Bar, forged and cast parts<\/li>\n<li class=\"p1\"><span class=\"s1\"><b>AMS 5587<\/b><\/span> \u2013 Pipes and piping systems<\/li>\n<li class=\"p1\"><span class=\"s1\"><b>UNS N06002<\/b><\/span> \u2013 Chemical composition designation<\/li>\n<li class=\"p1\"><span class=\"s1\"><b>Werkstoff Nr. 2.4665<\/b><\/span> \u2013 German DIN standard equivalent<\/li>\n<\/ul>\n<p class=\"p3\">Compliance with these standards is of importance especially in regulation-heavy sectors such as <span class=\"s2\"><b>aerospace and nuclear energy applications<\/b><\/span>.<\/p>\n<h3><b>Hastelloy X <\/b><b>Trade Names and Equivalent Materials<\/b><\/h3>\n<ul>\n<li class=\"p1\"><span class=\"s1\"><b>Hastelloy\u00ae X<\/b><\/span> \u2013 Registered by Haynes International<\/li>\n<li class=\"p1\"><span class=\"s1\"><b>Alloy X<\/b><\/span>, <span class=\"s1\"><b>Inconel HX<\/b><\/span>, <span class=\"s1\"><b>ATI HX<\/b><\/span> \u2013 Equivalent terms used in the technical literature<\/li>\n<li class=\"p1\"><span class=\"s1\"><b>UNS N06002<\/b><\/span>, <span class=\"s1\"><b>W.Nr. 2.4665<\/b><\/span> \u2013 International codings<\/li>\n<li class=\"p1\"><span class=\"s1\"><b>NiCr22Fe18Mo<\/b><\/span> \u2013 European EN chemical symbol<\/li>\n<\/ul>\n<p class=\"p3\">Among its equivalents there are also commercial variants such as <span class=\"s2\">Udimet Alloy 500<\/span>, <span class=\"s2\">Haynes HX<\/span> and <span class=\"s2\">Nicrofer 4722 Co<\/span>. All these materials, however, must be consistent with Hastelloy X at the level of the standards.<\/p>\n<hr>\n<h4><b>Areas of Use and Industrial Applications<\/b><\/h4>\n<p class=\"p3\"><span class=\"s2\"><b>Hastelloy X<\/b><\/span> is preferred especially in applications where high temperature, mechanical load and oxidative environments are present together:<\/p>\n<p class=\"p1\"><b>1.Aerospace Industry<\/b><b><\/b><\/p>\n<p class=\"p1\">*Jet engine combustion chambers<br \/>\n*Exhaust systems and combustion tubes<br \/>\n*Heat resistant fittings<\/p>\n<p class=\"p1\"><b>2.Gas Turbines and Power Generation<\/b><b><\/b><\/p>\n<p class=\"p1\">*Gas turbine components<br \/>\n*Heat exchangers and recuperators<br \/>\n*High temperature burner systems<\/p>\n<p class=\"p1\"><b>3.Petrochemical and Refinery Plants<\/b><b><\/b><\/p>\n<p class=\"p1\">*Reforming reactors<br \/>\n*Oxidising gas lines<br \/>\n*High temperature process pipes<\/p>\n<p class=\"p1\"><b>4.Nuclear Power Plant Components<\/b><b><\/b><\/p>\n<p class=\"p1\">*Internal components exposed to high radiation and temperature<br \/>\n*Heat transfer lines with a controlled atmosphere<\/p>\n<p class=\"p1\"><b>5.Heat Treatment Furnaces<\/b><b><\/b><\/p>\n<p class=\"p1\">*In-furnace parts, transport pallets, baskets<br \/>\n*Thermocouple protection tubes<\/p>\n<p class=\"p3\">Thanks to its mechanical and chemical stability under high temperature, <span class=\"s2\"><b>process efficiency and safety<\/b><\/span> are directly increased in these applications.<\/p>\n<hr>\n<h3><b>Advantages<\/b><\/h3>\n<ul>\n<li class=\"p1\"><b>Excellent Oxidation Resistance: <\/b>It remains stable in oxidising atmospheres up to 1200 \u00b0C. The high chromium and iron content contributes to this performance.<\/li>\n<li class=\"p1\"><b>Mechanical Stability at High Temperature: <\/b>It is strong in terms of creep strength and elongation at break. With this property it is ideal for parts operating under high temperature.<\/li>\n<li class=\"p1\"><b>Weldability: <\/b>It can be joined easily by the TIG, MIG and plasma arc welding methods. The risk of cracking after welding is low.<\/li>\n<li class=\"p1\"><b>Good Machinability: <\/b>It offers better chip removal capability compared with other nickel-based alloys.<\/li>\n<li class=\"p1\"><b>High Metallurgical Homogeneity: <\/b>The internal structure of the alloy has been developed so as to be durable against thermal cycles.<\/li>\n<\/ul>\n<hr>\n<h3><b>Disadvantages<\/b><\/h3>\n<ul>\n<li class=\"p1\"><b>Corrosion Resistance in Limited Environments: <\/b>Compared with alloys with a high molybdenum ratio such as C-22 or C-276, it may show lower performance in some acids (especially in reducing environments containing chloride).<\/li>\n<li class=\"p1\"><b>Cost: <\/b>It is costly because of the high nickel and molybdenum content. It is not economical for general structural applications.<\/li>\n<li class=\"p1\"><b>Carbide Precipitation in Welded Zones: <\/b>In cases of long-term exposure to high temperature, carbide precipitation may form at the grain boundaries. This situation may affect performance in some applications.<\/li>\n<\/ul>\n<hr>\n<h3><b>Conclusion and Engineering Evaluation<\/b><\/h3>\n<p class=\"p3\"><span class=\"s2\"><b>Hastelloy X<\/b><\/span> is a reliable super alloy for components operating at very high temperatures and at the same time exposed to oxidising and mechanical loading. It stands out especially in the field of <span class=\"s2\"><b>aerospace engines<\/b><\/span>, <span class=\"s2\"><b>gas turbines<\/b><\/span> and <span class=\"s2\"><b>high temperature process equipment<\/b><\/span> with its <span class=\"s2\"><b>metallurgical stability<\/b><\/span> and <span class=\"s2\"><b>weldability<\/b><\/span>.<\/p>\n<p class=\"p3\">Low maintenance costs and a long service life reduce the total cost of ownership and, despite the initial investment cost, make it a sustainable choice. For <span class=\"s2\"><b>precision engineering applications<\/b><\/span>, <span class=\"s2\"><b>industrial projects requiring certification<\/b><\/span> and <span class=\"s2\"><b>high safety processes<\/b><\/span>, Hastelloy X is a technically superior selection.<\/p>\n<p>&nbsp;<\/p>\n<h5><span class=\"s1\">#ASTMB435<br \/>\n<\/span><span class=\"s1\">#ASTMB619<br \/>\n#<\/span><span class=\"s1\">ASTMB366<\/span><br \/>\n<span class=\"s1\">#<\/span><span class=\"s1\">AMS5536<br \/>\n#<\/span><span class=\"s1\">AMS5754<br \/>\n#<\/span><span class=\"s1\">AMS5587<\/span><br \/>\n<span class=\"s1\">#<\/span><span class=\"s1\">UNSN06002<br \/>\n#<\/span><span class=\"s1\">2.4665<br \/>\n#<\/span><span class=\"s1\">Hastelloy\u00aeX<\/span><br \/>\n<span class=\"s1\">#<\/span><span class=\"s1\">AlloyX<br \/>\n#<\/span><span class=\"s1\">UNSN06002<br \/>\n#<\/span><span class=\"s1\">NiCr22Fe18Mo<\/span><\/h5>\n<p><!-- dm-ic-baglanti --><\/p>\n<div class=\"dm-ic-baglanti\" style=\"margin:28px 0 0;border:1px solid #e0e0e0;border-left:4px solid #DD3333;background:#FAFAFA;padding:16px 18px;\">\n<p style=\"font-size:12px;font-weight:700;letter-spacing:.06em;text-transform:uppercase;color:#DD3333;margin:0 0 6px;line-height:1.4;\">We supply this material<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.65;color:#333;\">We supply Hastelloy X (2.4665) \u2014 to the AMS 5536 standard, in the dimensions and forms required. Contact us for stock availability and pricing.<\/p>\n<p><a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/contact\/\" style=\"display:inline-block;color:#ffffff;background:#24BEE5;text-decoration:none;font-weight:600;font-size:14px;padding:10px 17px;line-height:1.2;\">Request a quotation \u2192<\/a>\n<\/div>\n<p><!-- \/dm-ic-baglanti --><\/p>\n<p><!-- dm-benzer --><\/p>\n<div class=\"dm-benzer\" style=\"margin:22px 0 0;padding:14px 16px;border:1px solid #e0e0e0;background:#FBFCFD;\">\n<p style=\"font-size:11px;font-weight:700;letter-spacing:.08em;text-transform:uppercase;color:#9aa3a8;margin:0 0 8px;line-height:1.4;\">Similar products<\/p>\n<p style=\"margin:0;font-size:15px;line-height:2;color:#333;\"><a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/monel-400\/\" style=\"color:#24BEE5;font-weight:600;text-decoration:none;\">Monel 400<\/a>  \u00b7  <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/monel-k500\/\" style=\"color:#24BEE5;font-weight:600;text-decoration:none;\">Monel K-500<\/a>  \u00b7  <a href=\"https:\/\/www.defencemetal.com\/index.php\/2025\/06\/24\/waspaloy-2-4654-uns-n07001-ams-5544-ams-5706-nickel-super-alloy\/\" style=\"color:#24BEE5;font-weight:600;text-decoration:none;\">Waspaloy<\/a>  \u00b7  <a href=\"https:\/\/www.defencemetal.com\/index.php\/2025\/06\/24\/nimonic-80a-uns-n07080-ams-4378-ams-5829-nickel-super-alloy\/\" style=\"color:#24BEE5;font-weight:600;text-decoration:none;\">Nimonic 80A<\/a>  \u00b7  <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/nickel-alloys\/\" style=\"color:#666;font-weight:600;text-decoration:none;\">All nickel alloys \u2192<\/a><\/p>\n<\/div>\n<p><!-- \/dm-benzer --><\/p>\n","protected":false},"excerpt":{"rendered":"<p>Hastelloy X (2.4665 \/ UNS N06002) is a nickel-chromium-iron-molybdenum super alloy with oxidation resistance and creep strength at high temperature. Chemical composition, ASTM B435 \/ B619 \/ B622 and AMS 5536, AMS 5754, AMS 5587 standards, trade names, jet engine, gas turbine and furnace applications.<\/p>\n","protected":false},"author":1,"featured_media":2132,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[8],"tags":[],"class_list":["post-4110","post","type-post","status-publish","format-standard","has-post-thumbnail","hentry","category-articles"],"yoast_head":"<!-- This site is optimized with the Yoast SEO plugin v28.5 - https:\/\/yoast.com\/product\/yoast-seo-wordpress\/ -->\n<title>Hastelloy X (2.4665 \/ UNS N06002) \u2014 AMS 5536 \/ AMS 5754 Nickel Alloy - Defence Metal<\/title>\n<meta name=\"description\" content=\"Hastelloy X (2.4665 \/ UNS N06002) is a nickel-chromium-iron-molybdenum super alloy with oxidation resistance and creep strength at high temperature.\" \/>\n<meta name=\"robots\" content=\"index, follow, max-snippet:-1, max-image-preview:large, max-video-preview:-1\" \/>\n<link rel=\"canonical\" href=\"https:\/\/www.defencemetal.com\/index.php\/2025\/06\/24\/hastelloy-x-2-4665-uns-n06002-ams-5536-ams-5754-nickel-alloy\/\" \/>\n<meta property=\"og:locale\" content=\"tr_TR\" \/>\n<meta property=\"og:type\" content=\"article\" \/>\n<meta property=\"og:title\" content=\"Hastelloy X (2.4665 \/ UNS N06002) \u2014 AMS 5536 \/ AMS 5754 Nickel Alloy - 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