{"id":3573,"date":"2026-09-16T11:01:47","date_gmt":"2026-09-16T08:01:47","guid":{"rendered":"https:\/\/www.defencemetal.com\/index.php\/en\/maraging-300\/"},"modified":"2026-09-25T16:25:20","modified_gmt":"2026-09-25T13:25:20","slug":"maraging-300","status":"publish","type":"page","link":"https:\/\/www.defencemetal.com\/index.php\/en\/maraging-300\/","title":{"rendered":"Maraging 300"},"content":{"rendered":"<p><!-- dm-hap --><\/p>\n<h1 class=\"dm-ust-baslik\" style=\"font-family:-apple-system,BlinkMacSystemFont,'Segoe UI',Helvetica,Arial,sans-serif !important;text-transform:none !important;font-size:27px;line-height:1.3;font-weight:800;color:#12303f;margin:0 0 10px;letter-spacing:-.01em;\">Maraging 300 \/ (1.6358) \/ UNS K93120 \/ AMS 6514 \/ AMS 6521<\/h1>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:0 0 22px;position:relative;overflow:hidden;\"><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<div style=\"background:#12303f;padding:14px 16px 12px;position:relative;z-index:2;\">\n<div style=\"font-size:22px;font-weight:700;color:#fff;line-height:1.25;\">Maraging 300<\/div>\n<div style=\"font-family:ui-monospace,Menlo,Consolas,monospace;font-size:12.5px;color:#b9cfdb;line-height:1.5;margin-top:5px;word-wrap:break-word;\">UNS K93120 \u00b7 W.Nr. 1.6358 (also 1.6354) \u00b7 X2NiCoMo18-9-5 \u00b7 18Ni(300) \/ C300 \u00b7 18.0-19.0% Ni \u2013 8.5-9.5% Co \u2013 4.6-5.2% Mo \u2013 0.50-0.80% Ti \u2013 0.05-0.15% Al \u2013 C \u2264 0.03%<\/div>\n<div data-dmkars-blok=\"1\" style=\"border-top:1px solid rgba(255,255,255,.16);margin-top:13px;padding-top:11px;\">\n<div style=\"font-size:10px;letter-spacing:.09em;text-transform:uppercase;color:#7f9fb0;font-weight:700;margin-bottom:8px;\">Not to be confused with<\/div>\n<p><a href=\"https:\/\/www.defencemetal.com\/index.php\/2026\/09\/15\/maraging-250-maraging-300-difference\/\" data-dmkars=\"1\" style=\"display:inline-block;padding:4px 11px;border:1px solid rgba(36,190,229,.45);background:rgba(36,190,229,.12);border-radius:99px;margin:0 6px 6px 0;font-size:12.5px;font-weight:600;color:#9fe2f7;text-decoration:none;\">Maraging 250<\/a><a href=\"https:\/\/www.defencemetal.com\/index.php\/2026\/09\/16\/maraging-300-maraging-350-difference\/\" data-dmkars=\"1\" style=\"display:inline-block;padding:4px 11px;border:1px solid rgba(36,190,229,.45);background:rgba(36,190,229,.12);border-radius:99px;margin:0 6px 6px 0;font-size:12.5px;font-weight:600;color:#9fe2f7;text-decoration:none;\">Maraging 350<\/a><\/div>\n<\/div>\n<div style=\"position:relative;z-index:2;\">\n<div style=\"display:flex;flex-wrap:wrap;border-top:1px solid #eceff1;\">\n<div style=\"flex:0 0 118px;padding:11px 14px;background:#F7FAFB;font-size:10.5px;letter-spacing:.09em;text-transform:uppercase;color:#6b8091;font-weight:600;line-height:1.5;\">For what<\/div>\n<div style=\"flex:1 1 230px;min-width:0;padding:11px 14px;font-size:14.5px;line-height:1.7;color:#3d5260;word-wrap:break-word;overflow-wrap:break-word;\">The most widely used grade of the maraging family. An essentially carbon-free iron-nickel martensitic precipitation-hardening steel that hardens by intermetallic precipitation, not carbides.<\/div>\n<\/div>\n<div style=\"display:flex;flex-wrap:wrap;border-top:1px solid #eceff1;\">\n<div style=\"flex:0 0 118px;padding:11px 14px;background:#F7FAFB;font-size:10.5px;letter-spacing:.09em;text-transform:uppercase;color:#6b8091;font-weight:600;line-height:1.5;\">Forms<\/div>\n<div style=\"flex:1 1 230px;min-width:0;padding:11px 14px;font-size:14.5px;line-height:1.7;color:#3d5260;word-wrap:break-word;overflow-wrap:break-word;\">Round bar \u00b7 Flat bar \u00b7 Plate \u00b7 Sheet \u00b7 Tube \u00b7 Forgings<\/div>\n<\/div>\n<div style=\"display:flex;flex-wrap:wrap;border-top:1px solid #eceff1;\">\n<div style=\"flex:0 0 118px;padding:11px 14px;background:#F7FAFB;font-size:10.5px;letter-spacing:.09em;text-transform:uppercase;color:#6b8091;font-weight:600;line-height:1.5;\">Standards<\/div>\n<div style=\"flex:1 1 230px;min-width:0;padding:11px 14px;font-size:14.5px;line-height:1.7;color:#3d5260;word-wrap:break-word;overflow-wrap:break-word;\"><b style=\"font-size:16.5px;font-weight:800;color:#12303f;\">AMS 6514<\/b> (bars, forgings, mechanical tubing, rings, forging stock \u2014 consumable electrode vacuum melted, annealed) \u00b7 <b style=\"font-size:16.5px;font-weight:800;color:#12303f;\">AMS 6521<\/b> (sheet, strip, plate \u2014 consumable electrode melted, solution heat treated) \u00b7 <b style=\"font-size:16.5px;font-weight:800;color:#12303f;\">AMS 6463<\/b> (welding wire, vacuum melted) \u00b7 MIL-S-46850 (300 ksi class; bar, plate, sheet, strip, forgings, extrusions) \u00b7 ASTM A538 Grade C (MAR-18-300, pressure vessel plate \u2014 the standard is no longer active) \u00b7 W.Nr. 1.6358 \/ X2NiCoMo18-9-5<br \/><span style=\"font-size:12.5px;color:#7b8f9b;line-height:1.6;display:inline-block;margin-top:6px;\">The AMS numbers have been verified against the grade, because they are frequently confused in the trade. The nominal compositions in the SAE title records are: AMS 6512 = 18Ni-7.8Co-4.9Mo-0.40Ti (Maraging 250), AMS 6514 = 18.5Ni-9.0Co-4.9Mo-0.65Ti (Maraging\u2026<\/span><\/div>\n<\/div>\n<div style=\"display:flex;flex-wrap:wrap;border-top:1px solid #eceff1;\">\n<div style=\"flex:0 0 118px;padding:11px 14px;background:#F7FAFB;font-size:10.5px;letter-spacing:.09em;text-transform:uppercase;color:#6b8091;font-weight:600;line-height:1.5;\">Advantage<\/div>\n<div style=\"flex:1 1 230px;min-width:0;padding:11px 14px;font-size:14.5px;line-height:1.7;color:#3d5260;word-wrap:break-word;overflow-wrap:break-word;\">The part is machined to finished size soft, then hardened, and its dimensions barely move. In the solution annealed condition it is 28-35 HRC and is machined in that state; 3-6 hours at 480-510 \u00b0C raises it to 50-55 HRC with no quench.<\/div>\n<\/div>\n<div style=\"display:flex;flex-wrap:wrap;border-top:1px solid #eceff1;\">\n<div style=\"flex:0 0 118px;padding:11px 14px;background:#F7FAFB;font-size:10.5px;letter-spacing:.09em;text-transform:uppercase;color:#6b8091;font-weight:600;line-height:1.5;\">Welding<\/div>\n<div style=\"flex:1 1 230px;min-width:0;padding:11px 14px;font-size:14.5px;line-height:1.7;color:#3d5260;word-wrap:break-word;overflow-wrap:break-word;\">Filler metal: maraging wire of approximately the same composition as the base metal; for Maraging 300 the verified AMS number is <b style=\"font-size:16.5px;font-weight:800;color:#12303f;\">AMS 6463<\/b> (18.5Ni-8.5Co-5.2Mo-0.72Ti-0.10Al, vacuum melted).<\/div>\n<\/div>\n<div style=\"display:flex;flex-wrap:wrap;border-top:1px solid #eceff1;\">\n<div style=\"flex:0 0 118px;padding:11px 14px;background:#fdeceb;font-size:10.5px;letter-spacing:.09em;text-transform:uppercase;color:#c0392b;font-weight:600;line-height:1.5;\">Limits<\/div>\n<div style=\"flex:1 1 230px;min-width:0;padding:11px 14px;font-size:14.5px;line-height:1.7;color:#3d5260;word-wrap:break-word;overflow-wrap:break-word;background:#fdeceb;\">It is not stainless. It contains no chromium and does not exhibit passive behaviour in 3% NaCl; it rusts like carbon steel in the atmosphere and in marine environments and must be protected (cadmium plating, phosphating, paint or similar). Carpenter data sheets classify its corrosion resistance as &#8216;Humidity Restricted&#8217;;<\/div>\n<\/div>\n<div style=\"padding:14px;border-top:1px solid #eceff1;\"><a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/contact\/\" style=\"display:inline-block;padding:11px 20px;font-size:14px;font-weight:700;text-decoration:none;margin:0 8px 6px 0;background:#dd3333;color:#ffffff;\">REQUEST A QUOTE<\/a><a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/alloy-steels\/\" style=\"display:inline-block;padding:11px 20px;font-size:14px;font-weight:700;text-decoration:none;margin:0 8px 6px 0;font-weight:600;border:1px solid #12303f;color:#12303f;\">All alloy steels &rarr;<\/a><span data-dm=\"dm-teknik\" style=\"cursor:pointer;display:inline-block;padding:11px 20px;font-size:14px;font-weight:700;text-decoration:none;margin:0 8px 6px 0;border:1px solid #dd3333;color:#dd3333;\">TECHNICAL DETAILS &darr;<\/span><\/div>\n<div style=\"padding:9px 14px;border-top:1px solid #eceff1;font-size:11.5px;color:#8a9aa4;line-height:1.5;\">Compiled from manufacturer data sheets \u00b7 confirm against the current specification before ordering<\/div>\n<\/div>\n<\/div>\n<p><!-- \/dm-hap --><!-- dm-nav --><\/p>\n<style>h4[id^=\"dm-b\"]{scroll-margin-top:120px}#dm-teknik{scroll-margin-top:120px}<\/style>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:0 0 22px;padding:12px 14px;\">\n<div style=\"font-size:10.5px;letter-spacing:.09em;text-transform:uppercase;color:#6b8091;font-weight:600;margin-bottom:9px;\">On this page &middot; click to jump<\/div>\n<div><span data-dm=\"dm-b0\" style=\"cursor:pointer;display:inline-block;padding:5px 11px;border:1px solid #dfe6ea;background:#F7FAFB;margin:0 6px 7px 0;font-size:13px;color:#12303f;\">Standards by Product Form<\/span><span data-dm=\"dm-b1\" style=\"cursor:pointer;display:inline-block;padding:5px 11px;border:1px solid #dfe6ea;background:#F7FAFB;margin:0 6px 7px 0;font-size:13px;color:#12303f;\">Mechanical Properties and Heat Treatment<\/span><span data-dm=\"dm-b2\" style=\"cursor:pointer;display:inline-block;padding:5px 11px;border:1px solid #dfe6ea;background:#F7FAFB;margin:0 6px 7px 0;font-size:13px;color:#12303f;\">Service Limits and Comparison<\/span><span data-dm=\"dm-b3\" style=\"cursor:pointer;display:inline-block;padding:5px 11px;border:1px solid #dfe6ea;background:#F7FAFB;margin:0 6px 7px 0;font-size:13px;color:#12303f;\">Frequently Asked Questions<\/span><\/div>\n<\/div>\n<p><script>(function(){function go(id){var e=document.getElementById(id);if(e){var s=document.scrollingElement||document.documentElement;var y=e.getBoundingClientRect().top+s.scrollTop-118;if(y-0-0-0-0!==y){y=0;}window.scrollTo(0,y);}}function bind(el){el.addEventListener(\"click\",function(ev){ev.preventDefault();go(el.getAttribute(\"data-dm\"));});}function init(){var l=document.querySelectorAll(\"[data-dm]\");Array.prototype.forEach.call(l,bind);if(location.hash){if(location.hash.indexOf(\"#dm-\")===0){try{history.replaceState(null,\"\",location.pathname+location.search);}catch(e){}window.scrollTo(0,0);setTimeout(function(){window.scrollTo(0,0);},80);}}}if(document.readyState===\"loading\"){document.addEventListener(\"DOMContentLoaded\",init);}else{init();}})();<\/script><!-- \/dm-nav --><br \/>\n<span id=\"dm-teknik\" style=\"display:block;height:0;overflow:hidden;\"><\/span><br \/>\nMaraging 300 (1.6358 &#8211; 1.6354), also widely known by its designation UNS K93120, is a special alloy steel formed essentially from nickel, molybdenum, cobalt and titanium. Grade 300 is the most widely used quality among the maraging materials. Including this one, there are four commonly known types of maraging steel: Maraging 200, 250, 300 and 350, and maraging steels are also known as 18Ni maraging steels. The numbers 200, 250 and 300 that follow the name indicate the ultimate tensile strength of the material in lbf\/in\u00b2, so the higher the number the stronger the material. Maraging materials contain little carbon, and that low carbon content is what makes them easy to machine. They can also, before ageing, be cold formed to a large degree without generating cracks. Maraging materials may undergo a small amount of dimensional change after heat treatment, so final precision dimensions on these materials are best machined after heat treatment. Thanks to their high alloy content, this material can be taken to high hardness after heat treatment. Maraging materials generally have moderate corrosion resistance, and where corrosion resistance has to be increased, cadmium plating or various other coatings can be used to raise it.<\/p>\n<p>The most widely used of the maraging materials, this is an alloy steel of very high mechanical strength and is generally chosen where very high mechanical strength is required. It is frequently used in aircraft landing gear parts, in aircraft gear components that have to carry mechanical load, and in structural applications that are permanently under load and need very high mechanical strength.<\/p>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Chemical Composition (Maraging 300 \u2013 X2NiCoMo19-9-5) \u00b7 Maraging 300 (1.6358)<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Ni<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">18.0-19.0%<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Fe<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">60.0-69.0% (typically around 67%)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Mo<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">4.60-5.20%<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">C<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">max 0.03%<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Mn<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">max 0.10%<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Si<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">max 0.10%<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">P<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">max 0.01%<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">S<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">max 0.01%<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Al<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">0.05-0.15%<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Co<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">8.00-9.50%<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Ti<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">0.55-0.80%<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Mechanical Properties at Room Temperature<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Density (specific gravity)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">8000 kg\/m\u00b3<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Melting Temperature<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Approx. 1413\u00b0C<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<div class=\"dm-std\" style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Standards and Equivalents \u00b7 Maraging 300<\/div>\n<div data-dmtw=\"1\" style=\"position:relative;overflow:hidden;\"><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<div style=\"position:relative;z-index:2;overflow-x:auto;\">\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Trade name<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Maraging 300<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">UNS<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">K93120<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">W.Nr (DIN\/EN)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">1.6358 \u00b7 1.6354<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">AMS<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">6514 \u00b7 6521<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Available forms<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Round bar \u00b7 Flat bar \u00b7 Plate \u00b7 Sheet \u00b7 Tube \u00b7 Forgings<br \/><span style=\"font-size:13px;color:#6b7a84;\">All forms are supplied to order.<\/span><\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<\/div>\n<\/div>\n<p><!-- dm-zengin --><\/p>\n<h4 id=\"dm-b0\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Standards by Product Form<\/h4>\n<p><!-- dm-diy-std --><\/p>\n<div style=\"border:1px solid #e3e9ec;margin:22px 0 26px;background:#fff;position:relative;overflow:hidden;\">\n<div style=\"background:#12303f;color:#fff;padding:9px 14px;font-size:14px;font-weight:700;letter-spacing:.3px;position:relative;z-index:2;\">STANDARDS BY PRODUCT FORM<\/div>\n<div style=\"position:relative;z-index:2;\">\n<div style=\"padding:12px 12px 2px;position:relative;overflow:hidden;\"><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<div style=\"overflow-x:auto;position:relative;z-index:2;\">\n<table style=\"width:100%;border-collapse:collapse;font-size:13.5px;min-width:430px;background:transparent;\">\n<tr>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Product form<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Standards<\/th>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;\">Round bar, flat bar, forging, mechanical tubing, rings<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\"><b style=\"font-size:16.5px;font-weight:800;color:#12303f;\">AMS 6514<\/b> \u00b7 MIL-S-46850 (300 ksi class)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;\">Plate, sheet, strip<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\"><b style=\"font-size:16.5px;font-weight:800;color:#12303f;\">AMS 6521<\/b> \u00b7 MIL-S-46850 (300 ksi class) \u00b7 ASTM A538 Grade C (inactive)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;\">Extrusion<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">MIL-S-46850 (300 ksi class)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;\">Welding wire<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\"><b style=\"font-size:16.5px;font-weight:800;color:#12303f;\">AMS 6463<\/b> (18.5Ni-8.5Co-5.2Mo-0.72Ti-0.10Al, vacuum melted)<\/td>\n<\/tr>\n<\/table>\n<\/div>\n<\/div>\n<\/div>\n<div style=\"padding:6px 14px 12px;font-size:12px;color:#5b7180;line-height:1.7;border-top:1px solid #f0f3f5;position:relative;z-index:2;\">AMS numbers are listed first, ASTM and military specifications after. Every AMS number has been checked against its grade using the nominal composition in the SAE title record. ASTM A538 is &#8216;Inactive&#8217; and ASTM A579 was withdrawn in 2024 with no replacement; neither should be relied on alone for new orders.<\/div>\n<\/div>\n<p><!-- \/dm-diy-std --><\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\">Maraging 300 (18Ni-300 \/ UNS K93120 \/ C300) is an iron-nickel alloy that hardens not through carbon but through <b>intermetallic precipitation<\/b>. The 300 in the name denotes the nominal <b>300 ksi (~2070 MPa) tensile class<\/b> in the aged condition. Two things must be understood from the outset: it is <b>not stainless<\/b>, and it is an <b>export-controlled dual-use material<\/b>.<\/p>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Standards by Product Form \u00b7 Maraging 300 (K93120)<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Bar \u00b7 Billet \u00b7 Forging stock<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>AMS 6514<\/b> (current revision K)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Forgings<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">AMS 6514 \u00b7 ASTM A579 (superstrength alloy steel forgings)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Plate \u00b7 Sheet \u00b7 Strip<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>AMS 6521<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">ASTM plate standard<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">ASTM A538 \/ A538M Grade C (&#8220;MAR-18-300&#8221;) \u2014 <b>a 1982 document that is now inactive\/withdrawn<\/b>; usable as a historical reference, not as the governing current standard<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">EN \/ Werkstoff number<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>1.6358<\/b> and <b>1.6354<\/b> \u2014 sources are not consistent about which applies to bar and which to plate; citing both is the safer practice<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Military<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">MIL-S-46850 (all grades, including fracture-toughness requirements). Reports that this specification has been cancelled in favour of AMS numbers <b>could not be confirmed against a primary record<\/b> \u2014 the AMS numbers are the safer current citation<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Pipe \u00b7 tube \u00b7 wire<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">\u2014 (no separate verified AMS number was found)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Welding wire<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">\u2014 (no separate verified AMS welding-wire specification was found; matching-composition wire is used)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Additive-manufacturing powder<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">There is no dedicated powder specification number; powder grades are qualified against <b>AMS 6514 \/ 6521<\/b> properties after solution treatment and ageing<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>WARNING \u2014 catalogue traps.<\/b> (1) <b>AMS 6514 and AMS 6521 must not be conflated:<\/b> 6514 covers bar, billet and forging stock; 6521 covers sheet, strip and plate. Many reseller pages list every product form under &#8220;AMS 6514&#8221;. (2) ASTM A538 should not be presented as an active standard. (3) Some supplier pages sell the product as <b>&#8220;Maraging 300 stainless steel&#8221;<\/b> \u2014 metallurgically wrong; the alloy contains no significant chromium. (4) The ageing cycle is frequently quoted <b>without the solution-treatment step<\/b>; a customer who applies ageing alone to non-annealed stock will not obtain the quoted properties.<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>Composition:<\/b> <b>C \u22640.03%<\/b> \u00b7 Ni 18.0\u201319.0% \u00b7 Co 8.0\u20139.5% \u00b7 Mo 4.6\u20135.2% \u00b7 Ti 0.50\u20130.80% \u00b7 Al 0.05\u20130.15% \u00b7 Si \u22640.10% \u00b7 Mn \u22640.10% \u00b7 S \u22640.010% \u00b7 P \u22640.010%. <b>Why the very low carbon matters:<\/b> strength does not come from the hardness of a carbon martensite as it does in conventional steels. Carbon is deliberately held below 0.03%, so the as-cooled structure is not a hard, brittle carbon martensite but a <b>soft, ductile iron-nickel martensite<\/b>. All of the strength is added afterwards, in a separate ageing step, by nanoscale <b>Ni\u2083Mo, Ni\u2083Ti and Fe\u2082Mo<\/b> intermetallic precipitates forming on dislocations.<\/p>\n<h4 id=\"dm-b1\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Mechanical Properties and Heat Treatment<\/h4>\n<p><!-- dm-diy-sert --><\/p>\n<div style=\"border:1px solid #e3e9ec;margin:22px 0 26px;background:#fff;position:relative;overflow:hidden;\">\n<div style=\"background:#12303f;color:#fff;padding:9px 14px;font-size:14px;font-weight:700;letter-spacing:.3px;position:relative;z-index:2;\">STRENGTH BY AGEING CONDITION<\/div>\n<div style=\"position:relative;z-index:2;\">\n<div style=\"padding:12px 10px 0;\"><svg viewBox=\"0 0 740 98\" style=\"width:100%;height:auto;display:block;\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\" role=\"img\"><rect x=\"16\" y=\"6\" width=\"12\" height=\"12\" fill=\"#12303f\"\/><text x=\"34\" y=\"16\" font-size=\"11.5\" fill=\"#12303f\" font-family=\"Arial,Helvetica,sans-serif\">Yield (MPa)<\/text><rect x=\"146\" y=\"6\" width=\"12\" height=\"12\" fill=\"#7fa8bd\"\/><text x=\"164\" y=\"16\" font-size=\"11.5\" fill=\"#12303f\" font-family=\"Arial,Helvetica,sans-serif\">Tensile (MPa)<\/text><text x=\"16\" y=\"44\" font-size=\"12.5\" font-weight=\"bold\" fill=\"#12303f\" font-family=\"Arial,Helvetica,sans-serif\">Solution annealed + aged (480-510 \u00b0C \/ 3-6 h \/ air)<\/text><rect x=\"16\" y=\"50\" width=\"652.0\" height=\"15\" fill=\"#7fa8bd\"\/><text x=\"675.0\" y=\"62\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">2000<\/text><rect x=\"16\" y=\"68\" width=\"629.2\" height=\"15\" fill=\"#12303f\"\/><text x=\"652.2\" y=\"80\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">1930<\/text><\/svg><\/div>\n<div style=\"padding:12px 12px 2px;position:relative;overflow:hidden;\"><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<div style=\"overflow-x:auto;position:relative;z-index:2;\">\n<table style=\"width:100%;border-collapse:collapse;font-size:13.5px;min-width:430px;background:transparent;\">\n<tr>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Condition<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Hardness<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Yield MPa<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Tensile MPa<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Elongation<\/th>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;\">Solution annealed (815-820 \u00b0C \/ air) \u2014 as-delivered<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">36 max<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">\u2014<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">\u2014<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">\u2014<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;\">Solution annealed + aged (480-510 \u00b0C \/ 3-6 h \/ air)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">50-55<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">1930-2135<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">2000-2170<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">7-11%<\/td>\n<\/tr>\n<\/table>\n<\/div>\n<\/div>\n<\/div>\n<div style=\"padding:6px 14px 12px;font-size:12px;color:#5b7180;line-height:1.7;border-top:1px solid #f0f3f5;position:relative;z-index:2;\"><b style=\"color:#12303f;\">The rows are NOT the minimums of a single specification. They are the enclosing range of values published by several independent sources (producer data sheets, specification title records, government laboratory reports) for the same heat treatment condition. Order to the specification minimum.<\/b> In the chart, a value given as a range is drawn at its lower bound; the full range is in the table. The hardness and strength band shifts within itself with aging temperature and time; the order specification must state the aging condition. No strength values are given for the solution annealed condition: a common yield\/tensile band confirmed by 4 independent sources could not be established for that condition, only the hardness band.<\/div>\n<\/div>\n<p><!-- \/dm-diy-sert --><!-- dm-diy-isil --><\/p>\n<div style=\"border:1px solid #e3e9ec;margin:22px 0 26px;background:#fff;position:relative;overflow:hidden;\">\n<div style=\"background:#12303f;color:#fff;padding:9px 14px;font-size:14px;font-weight:700;letter-spacing:.3px;position:relative;z-index:2;\">HEAT TREATMENT \u2014 SCHEMATIC<\/div>\n<div style=\"position:relative;z-index:2;\">\n<div style=\"padding:14px 12px 4px;display:flex;flex-wrap:wrap;gap:10px;align-items:stretch;\">\n<div style=\"flex:1 1 180px;min-width:150px;background:#12303f;color:#fff;padding:12px 14px;\">\n<div style=\"font-size:12.5px;font-weight:700;letter-spacing:.06em;line-height:1.35;\">1 \u00b7 SOLUTION TREATMENT<\/div>\n<div style=\"font-size:12.5px;line-height:1.5;margin-top:4px;opacity:.88;\">815-820 \u00b0C (1500 \u00b0F)<br \/>1 hour (depending on section thickness; producer data sheets state a minimum of 30 minutes)<\/div>\n<\/div>\n<div style=\"flex:1 1 180px;min-width:150px;background:#c0392b;color:#fff;padding:12px 14px;\">\n<div style=\"font-size:12.5px;font-weight:700;letter-spacing:.06em;line-height:1.35;\">2 \u00b7 COOL<\/div>\n<div style=\"font-size:12.5px;line-height:1.5;margin-top:4px;opacity:.88;\">air cool to room temperature<\/div>\n<\/div>\n<div style=\"flex:1 1 180px;min-width:150px;background:#1b7f4b;color:#fff;padding:12px 14px;\">\n<div style=\"font-size:12.5px;font-weight:700;letter-spacing:.06em;line-height:1.35;\">3 \u00b7 AGEING<\/div>\n<div style=\"font-size:12.5px;line-height:1.5;margin-top:4px;opacity:.88;\">see the table below<\/div>\n<\/div>\n<\/div>\n<div style=\"padding:6px 10px 0;\"><svg viewBox=\"0 0 740 148\" style=\"width:100%;height:auto;display:block;\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\" role=\"img\"><line x1=\"70\" y1=\"68\" x2=\"690\" y2=\"68\" stroke=\"#9fb0ba\" stroke-width=\"2\"\/><line x1=\"70.0\" y1=\"68\" x2=\"70.0\" y2=\"42\" stroke=\"#c7d2d9\" stroke-width=\"1.5\"\/><circle cx=\"70.0\" cy=\"68\" r=\"5\" fill=\"#12303f\"\/><text x=\"70.0\" y=\"34\" text-anchor=\"middle\" font-size=\"12.5\" font-weight=\"bold\" fill=\"#12303f\" font-family=\"Arial,Helvetica,sans-serif\">Aging<\/text><text x=\"70.0\" y=\"19\" text-anchor=\"middle\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">480 \u00b0C<\/text><line x1=\"670.0\" y1=\"68\" x2=\"670.0\" y2=\"42\" stroke=\"#c7d2d9\" stroke-width=\"1.5\"\/><circle cx=\"670.0\" cy=\"68\" r=\"5\" fill=\"#12303f\"\/><text x=\"670.0\" y=\"34\" text-anchor=\"middle\" font-size=\"12.5\" font-weight=\"bold\" fill=\"#12303f\" font-family=\"Arial,Helvetica,sans-serif\">Aging<\/text><text x=\"670.0\" y=\"19\" text-anchor=\"middle\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">510 \u00b0C<\/text><text x=\"370\" y=\"142\" text-anchor=\"middle\" font-size=\"11.5\" font-weight=\"bold\" fill=\"#12303f\" font-family=\"Arial,Helvetica,sans-serif\">Ageing temperature (\u00b0C)<\/text><\/svg><\/div>\n<div style=\"padding:10px 12px 2px;position:relative;overflow:hidden;\"><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<div style=\"position:relative;z-index:2;\">\n<div style=\"font-size:13.5px;font-weight:700;color:#12303f;margin:6px 0 6px;\">Solution treatment<\/div>\n<table style=\"width:100%;border-collapse:collapse;font-size:13.5px;background:transparent;\">\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Step<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">Solution anneal \u2014 soft martensite<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Temperature<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">815-820 \u00b0C (1500 \u00b0F)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Time<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">1 hour (depending on section thickness; producer data sheets state a minimum of 30 minutes)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Cooling<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">air cool to room temperature<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Resulting hardness<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">28-35 HRC (soft, heavily dislocated Fe-Ni lath martensite; machining is done in this condition)<\/td>\n<\/tr>\n<\/table>\n<\/div>\n<\/div>\n<div style=\"padding:10px 12px 2px;position:relative;overflow:hidden;\"><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<div style=\"position:relative;z-index:2;\">\n<div style=\"font-size:13.5px;font-weight:700;color:#12303f;margin:6px 0 6px;\">Aging \u2014 common practice<\/div>\n<table style=\"width:100%;border-collapse:collapse;font-size:13.5px;background:transparent;\">\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Step<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">Aging \u2014 common practice<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Temperature<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">480 \u00b0C (900 \u00b0F)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Time<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">3-6 hours<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Cooling<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">air<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Resulting hardness<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">52-55 HRC<\/td>\n<\/tr>\n<\/table>\n<\/div>\n<\/div>\n<div style=\"padding:10px 12px 2px;position:relative;overflow:hidden;\"><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<div style=\"position:relative;z-index:2;\">\n<div style=\"font-size:13.5px;font-weight:700;color:#12303f;margin:6px 0 6px;\">Aging \u2014 full published band<\/div>\n<table style=\"width:100%;border-collapse:collapse;font-size:13.5px;background:transparent;\">\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Step<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">Aging \u2014 full published band<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Temperature<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">480-510 \u00b0C (900-950 \u00b0F)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Time<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">3-6 hours<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Cooling<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">air<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Resulting hardness<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">50-55 HRC<\/td>\n<\/tr>\n<\/table>\n<\/div>\n<\/div>\n<\/div>\n<div style=\"padding:6px 14px 12px;font-size:12px;color:#5b7180;line-height:1.7;border-top:1px solid #f0f3f5;position:relative;z-index:2;\">The diagram is schematic; the time axis is not to scale. No published TTT or CCT curve was used for Maraging 250\/300\/350. Hardening is not by carbide precipitation but by intermetallic precipitation: aging forms Ni3Mo, eta-Ni3Ti and, at long times, Fe2Mo \/ Fe7Mo6 nanoprecipitates. Carbon is held to 0.03% max, and this is deliberate: carbon would form TiC with the titanium and reduce impact strength, ductility and toughness. There is no quench in the solution treatment. Air cooling gives soft martensite directly; there is no critical cooling rate for hardening, so heavy sections take the same structure right through. The aging temperature also fixes the upper service temperature: a part aged at 480-510 \u00b0C will continue to age, and then overage, at service temperatures approaching that band. Dimensional change on aging is small: sources give a uniform contraction of roughly 0.05% to 0.10% on all dimensions, and because there is no quench no distortion is reported. For the numerical value see the &#8216;celiskiler&#8217; section.<\/div>\n<\/div>\n<p><!-- \/dm-diy-isil --><\/p>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Maraging 300 \u00b7 Two Conditions<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Solution annealed (as delivered)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Yield ~830 MPa \u00b7 Tensile ~1030 MPa \u00b7 Elongation ~16% \u00b7 Reduction of area ~70% \u00b7 <b>~30\u201335 HRC<\/b> \u2014 soft and readily machined<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Aged (482 \u00b0C)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Yield 1930\u20132000 MPa \u00b7 Tensile 2000\u20132035 MPa \u00b7 Elongation 8\u201312% \u00b7 Reduction of area 40\u201346% \u00b7 <b>50\u201355 HRC<\/b> (nominally ~52 HRC)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Fracture toughness<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">\u2014 (the only numeric K<sub>Ic<\/sub> figure found for C300 is single-sourced and is not published here as a catalogue value)<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">Heat treatment<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\">The mechanism is <b>age hardening of a low-carbon iron-nickel martensite<\/b>, with the strength coming from Ni\u2083Mo \/ Ni\u2083Ti \/ Fe\u2082Mo intermetallics rather than carbides. <b>Solution annealing:<\/b> about 816 \u00b0C (1500 \u00b0F), typically 1 hour (roughly 1 hour per inch for heavy sections), air cool \u2192 ~30\u201335 HRC. <b>Ageing:<\/b> <b>482 \u00b0C (900 \u00b0F)<\/b> for 3\u20136 hours (sources give 3 or 6 hours depending on section size), air cool \u2192 ~52 HRC and ~2000 MPa tensile. <b>Modified cycle for die-casting tooling:<\/b> anneal at 816\u2013829 \u00b0C for 1 hour per inch, then age at 527\u2013538 \u00b0C for 6 hours. <b>Dimensional stability:<\/b> ageing produces roughly <b>0.05% linear contraction<\/b> \u2014 with no quench involved, distortion is far below that of conventionally hardened steels, so parts can be machined close to final size and aged afterwards. <b>Standard delivery is the solution-annealed condition.<\/b><\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">Welding<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\">Weldability is good for the strength class. The common statement in mill and service-centre datasheets is that <b>no preheat or pre-heating is required<\/b> \u2014 a genuine distinguishing feature against conventional high-strength alloy steels, and a direct consequence of the very low carbon (no brittle carbon martensite and no hydrogen-cracking risk in the HAZ). Repair weldability is also good. <b>Post-weld ageing is required<\/b>: welding is normally done in the soft, solution-annealed condition and the whole part is aged afterwards. Welding already-aged material still requires ageing, and the HAZ toughness will not fully match the base metal. <b>Note:<\/b> one general materials database states that preheat and post-weld heat treatment are required, which conflicts with the mill-datasheet consensus \u2014 for critical work your welding engineer should confirm this against the specific mill&#8217;s WPS.<\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">Machining<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\">In the annealed condition, machinability is comparable to <b><a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/aisi-4340\/\">AISI 4340<\/a><\/b> at the same hardness level. The standard practice is to <b>rough and usually finish machine in the soft, solution-annealed condition and age afterwards<\/b> \u2014 because distortion on ageing is so small, most finish machining can be completed before hardening, which is the alloy&#8217;s principal commercial advantage over conventional tool steels that distort and need post-hardening grinding. Machining in the aged condition (52+ HRC) requires <b>rigid equipment, very sharp (usually carbide) tooling and abundant coolant<\/b>. <b>Nitriding<\/b> can be applied for wear resistance (single-sourced).<\/p>\n<h4 id=\"dm-b2\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Service Limits and Comparison<\/h4>\n<p><!-- dm-diy-kars --><\/p>\n<div style=\"border:1px solid #e3e9ec;margin:22px 0 26px;background:#fff;position:relative;overflow:hidden;\">\n<div style=\"background:#12303f;color:#fff;padding:9px 14px;font-size:14px;font-weight:700;letter-spacing:.3px;position:relative;z-index:2;\">COMPARISON<\/div>\n<div style=\"position:relative;z-index:2;\">\n<div style=\"padding:10px 14px 0;font-size:12.5px;color:#5b7180;line-height:1.7;\">The three grades are compared along one heat treatment route: solution annealing at 815-820 \u00b0C with air cooling, followed by aging at 480-510 \u00b0C with air cooling. Composition bands are taken from the nominal compositions in the AMS 6512 \/ 6514 \/ 6515 title records together with producer and specification bands; aged strength and hardness are given as the enclosing range of the values published by several independent sources for the same condition (solution annealed plus aged). No single producer&#8217;s typical table is used on its own, and the scatter between sources is left visible as a range. The molybdenum band is the same in all three grades; what changes is cobalt and titanium.<\/div>\n<div style=\"padding:12px 12px 2px;position:relative;overflow:hidden;\"><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<div style=\"overflow-x:auto;position:relative;z-index:2;\">\n<table style=\"width:100%;border-collapse:collapse;font-size:13.5px;min-width:430px;background:transparent;\">\n<tr>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Grade<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">AMS<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Cobalt<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Molybdenum<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Titanium<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Carbon<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Melting practice<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Aged yield MPa<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Aged tensile MPa<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Hardness HRC<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Elongation<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Note<\/th>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;\">Maraging 250 (18Ni-250 \u00b7 UNS K92890 \u00b7 1.6359)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">AMS 6512 (bars, forgings, mechanical tubing, rings) \u00b7 AMS 6520 (sheet, strip, plate)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">7.0-8.5% (AMS nominal 7.8%)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">4.6-5.2% (AMS nominal 4.9%)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">0.30-0.50% (AMS nominal 0.40%)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">0.03% max<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">Consumable electrode vacuum melted (VIM + VAR)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">1700-1760<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">1760-1860<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">48-52<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">6-11%<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">The toughest of the three grades; highest fracture toughness and best stress corrosion behaviour.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;\">Maraging 300 (18Ni-300 \u00b7 UNS K93120 \u00b7 1.6358)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">AMS 6514 (bars, forgings, mechanical tubing, rings) \u00b7 AMS 6521 (sheet, strip, plate) \u00b7 AMS 6463 (welding wire)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">8.5-9.5% (AMS nominal 9.0%)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">4.6-5.2% (AMS nominal 4.9%)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">0.50-0.80% (AMS nominal 0.65%)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">0.03% max<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">Consumable electrode vacuum melted (VIM + VAR)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">1930-2135<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">2000-2170<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">50-55<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">7-11%<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">Cobalt and titanium are raised relative to grade 250; yield strength rises by roughly 300 MPa while elongation falls.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;\">Maraging 350 (18Ni-350 \u00b7 UNS K93160)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">AMS 6515 (bars, forgings, tubing, rings \u2014 double vacuum melted)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">11.5-12.5% (AMS nominal 12.0%)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">4.6-5.2% (AMS nominal 4.9%)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">1.30-1.60% (AMS nominal 1.40%)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">0.03% max<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">Double vacuum melted (required by AMS 6515)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">2275-2320<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">2310-2415<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">53-58<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">6-8%<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">Titanium is about 3.5 times that of grade 250. It is the grade most susceptible to stress corrosion cracking (NASA report); there is no verified AMS number for sheet or plate.<\/td>\n<\/tr>\n<\/table>\n<\/div>\n<\/div>\n<\/div>\n<div style=\"padding:6px 14px 12px;font-size:12px;color:#5b7180;line-height:1.7;border-top:1px solid #f0f3f5;position:relative;z-index:2;\">Raising cobalt from 7.8% to 12.0% and titanium from 0.40% to 1.40% lifts the aged yield strength from about 1700 MPa to over 2300 MPa and hardness from 48 HRC to around 55 HRC. The molybdenum band is 4.6-5.2% in all three grades; what raises strength is not the molybdenum level but the density of intermetallic precipitates produced by the higher cobalt and titanium. The cost: elongation falls from about 11% to 6%, reduction of area for grade 350 is quoted as low as 25%, susceptibility to stress corrosion cracking rises with strength (the NASA report ranks grade 350 as the most susceptible), and the alloy cost rises with cobalt content. The strength and hardness figures in a row are not the minimums of a single specification; they are the enclosing range of values published by independent sources for the same heat treatment condition. Order to the specification minimum. Sources give the aged hardness of grade 350 between 53 HRC (Dynamic Metals) and 55-60 HRC (SSA Corp); the table therefore shows a range rather than a single number.<\/div>\n<\/div>\n<p><!-- \/dm-diy-kars --><\/p>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Maraging 300 \u00b7 Properties and Neighbouring Grades<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Service temperature<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Useful strength retained to about 450 \u00b0C (840 \u00b0F); above that overageing and loss of strength begin<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Corrosion \u2014 IMPORTANT<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>It is not stainless.<\/b> There is no significant chromium; corrosion resistance is broadly comparable to a conventional low-alloy martensitic steel. Conventional protection \u2014 <b>plating, phosphating, paint or an oil film<\/b> \u2014 is required in humid or marine service<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Magnetic<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Ferromagnetic, as a martensitic ferrous alloy<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Defining property<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Toughness and ductility retained at very high strength (8\u201312% elongation and 40\u201346% reduction of area in the aged condition) \u2014 conventional steels tempered to the same hardness are effectively without ductility<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/maraging-250\/\">Maraging 250<\/a><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Lower Co (~7.5\u20138.5%) and Ti (~0.4%); aged tensile ~1720\u20131760 MPa, ~48\u201350 HRC. The tougher, lower-strength option<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/maraging-350\/\">Maraging 350<\/a><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Higher Co (~12%) and Ti (~1.4%); aged tensile ~2340\u20132410 MPa, ~55\u201360 HRC. Highest strength, lowest toughness<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/aermet-100\/\">AerMet 100<\/a><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">A carbide-bearing (not carbon-free) secondary-hardening steel, tensile ~1930\u20131965 MPa. Fracture toughness and stress-corrosion resistance are excellent, but the carbide content makes it harder to machine than maraging steel, and conventional quench and temper means more distortion<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/aisi-4340\/\">AISI 4340<\/a><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Can be heat-treated to similar tensile levels, but with far lower ductility and toughness and much greater quench distortion<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Export control<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>A dual-use, export-controlled material<\/b> under multilateral non-proliferation regimes. End-use statements, export licences and\/or destination-country documentation are normally required for international shipment<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<h4 id=\"dm-b3\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Frequently Asked Questions<\/h4>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">What does &#8220;maraging&#8221; mean, and why is there almost no carbon?<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\">&#8220;Maraging&#8221; is a contraction of <b>martensitic ageing<\/b>. Conventional alloy steels take their hardness from carbon locked into a martensitic structure by quenching. Maraging steel instead keeps carbon deliberately very low (\u22640.03%). The result, straight from the mill or after a simple air-cooled solution anneal, is a <b>soft, tough iron-nickel martensite<\/b> at around 30\u201335 HRC, easily machined or formed. All of the strength is added afterwards in a separate low-temperature ageing step (roughly 482 \u00b0C for a few hours), during which nanoscale nickel-molybdenum and nickel-titanium intermetallics precipitate throughout the matrix, raising hardness to 50\u201355 HRC and tensile strength to roughly 2000 MPa. Because none of this depends on carbon, the alloy avoids the brittleness and cracking risk that high-carbon steels show at equivalent strength.<\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">Why are parts machined before ageing, and how much do they move?<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\">Maraging 300 is normally supplied and machined in its soft, solution-annealed condition (~30\u201335 HRC), where it cuts much like a mild alloy steel. The ageing treatment that follows is a simple, low-temperature (~482 \u00b0C) air-cooled cycle with <b>no quench<\/b>, so it produces only a very small, predictable dimensional change \u2014 mill data for C300 puts it at roughly <b>0.05% linear contraction<\/b>. That is far less movement than a conventional tool steel sees during a hardening quench, so shops routinely finish-machine tight-tolerance features <b>before<\/b> ageing, cutting or eliminating the post-hardening grinding pass that other high-strength steels need. This is the material&#8217;s main commercial advantage for precision tooling and aerospace hardware.<\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">Is Maraging 300 stainless, and does it need corrosion protection?<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\">No \u2014 despite the name, and despite some catalogues mislabelling it, Maraging 300 is <b>not a stainless steel<\/b>. It contains essentially no chromium; its corrosion resistance comes only incidentally from its nickel content and is broadly similar to an ordinary low-alloy martensitic steel, not to a 400- or 300-series stainless. Bare parts will rust in humid, marine or chemically aggressive environments. For any service outside a dry, controlled environment, plan on conventional protection \u2014 plating, phosphating, paint or an oil or grease film \u2014 the same as you would specify for <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/aisi-4340\/\">4340<\/a> or a comparable alloy steel. Confirm plating and coating compatibility with the customer&#8217;s ageing cycle, since some coatings must be applied after the final age.<\/p>\n<p><!-- \/dm-zengin --><\/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;\">Related grades<\/p>\n<p style=\"margin:0;font-size:15px;line-height:2;color:#333;\"><a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/aisi-4340\/\" style=\"color:#24BEE5;font-weight:600;text-decoration:none;\">4340 VAR<\/a> &nbsp;\u00b7&nbsp; <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/maraging-350\/\" style=\"color:#24BEE5;font-weight:600;text-decoration:none;\">Maraging 350<\/a> &nbsp;\u00b7&nbsp; <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/aermet-100\/\" style=\"color:#24BEE5;font-weight:600;text-decoration:none;\">AerMet 100<\/a> &nbsp;\u00b7&nbsp; <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/aisi-8740\/\" style=\"color:#24BEE5;font-weight:600;text-decoration:none;\">AISI 8740<\/a> &nbsp;\u00b7&nbsp; <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-ld --><script type=\"application\/ld+json\">{\"@context\":\"https:\/\/schema.org\",\"@type\":\"WebPage\",\"name\":\"Maraging 300\",\"url\":\"https:\/\/www.defencemetal.com\/index.php\/en\/maraging-300\/\",\"inLanguage\":\"en\",\"description\":\"Maraging 300 (18Ni-300 \/ UNS K93120 \/ C300) is an iron-nickel alloy that hardens not through carbon but through intermetallic precipitation. The 300 in the name denotes the nominal 300 ksi (~2070 MPa) tensile class in the aged condition.\",\"isPartOf\":{\"@type\":\"WebSite\",\"name\":\"Defence Metal\",\"url\":\"https:\/\/www.defencemetal.com\/\"},\"publisher\":{\"@type\":\"Organization\",\"name\":\"Defence Metal\",\"url\":\"https:\/\/www.defencemetal.com\/\"},\"mainEntity\":{\"@type\":\"DefinedTerm\",\"name\":\"Maraging 300\",\"description\":\"Maraging 300 (18Ni-300 \/ UNS K93120 \/ C300) is an iron-nickel alloy that hardens not through carbon but through intermetallic precipitation. 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The most widely used maraging grade; low carbon, machinable soft, hardened by ageing.","inspiro_hide_title":false,"inspiro_hide_featured_image":false,"footnotes":""},"dm_sektor":[10,9],"class_list":["post-3573","page","type-page","status-publish","hentry"],"yoast_head":"<!-- This site is optimized with the Yoast SEO plugin v28.5 - https:\/\/yoast.com\/product\/yoast-seo-wordpress\/ -->\n<title>MARAGING 300 \/ (1.6358) \/ UNS K93120 \/ AMS 6514 \/ AMS 6521 | Defence Metal<\/title>\n<meta name=\"description\" content=\"Maraging 300 (UNS K93120, 1.6358) \u2014 AMS 6514 \/ AMS 6521. 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