{"id":3541,"date":"2026-09-16T10:57:54","date_gmt":"2026-09-16T07:57:54","guid":{"rendered":"https:\/\/www.defencemetal.com\/index.php\/en\/maraging-350\/"},"modified":"2026-09-25T16:25:25","modified_gmt":"2026-09-25T13:25:25","slug":"maraging-350","status":"publish","type":"page","link":"https:\/\/www.defencemetal.com\/index.php\/en\/maraging-350\/","title":{"rendered":"Maraging 350 \/ AMS 6515"},"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 350 \/ AMS 6515<\/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 350<\/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 K93160 \u00b7 18Ni(350) \/ C350 \u00b7 18.0-19.0% Ni \u2013 11.5-12.5% Co \u2013 4.6-5.2% Mo \u2013 1.30-1.60% 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\/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 300<\/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 highest-strength grade of the maraging family. Cobalt is raised to 12% and titanium to 1.4%; carbon is still 0.03% max and hardening is again by intermetallic precipitation.<\/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 6515<\/b> (bars, forgings, tubing, rings \u2014 double vacuum melted, annealed) \u00b7 MIL-S-46850 (350 ksi class; bar, plate, sheet, strip, forgings, extrusions; fracture toughness requirements apply) \u00b7 UNS K93160<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 53-58 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;\">What Maraging 350 Is<\/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;\">Standards by Product Form<\/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;\">ASME Code Acceptance and Pressure-Equipment Status<\/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;\">Product Forms With NO Standard<\/span><span data-dm=\"dm-b4\" 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;\">Chemical Composition<\/span><span data-dm=\"dm-b5\" 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<\/span><span data-dm=\"dm-b6\" 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;\">Physical Properties<\/span><span data-dm=\"dm-b7\" 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;\">Heat Treatment and Thermal Stability<\/span><span data-dm=\"dm-b8\" 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;\">Welding<\/span><span data-dm=\"dm-b9\" 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;\">Machining<\/span><span data-dm=\"dm-b10\" 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;\">Corrosion<\/span><span data-dm=\"dm-b11\" 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><span data-dm=\"dm-b12\" 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;\">Common Datasheet Errors and Traps<\/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 350 is a special high-alloy steel with low carbon and a high nickel and cobalt content. It is the highest strength member of the maraging family within the nickel alloy group, one step above the 250 and 300 grades.<\/p>\n<p>What separates maraging steels from other high strength steels is that they take their hardness from intermetallic precipitates rather than from carbon. The carbon content is held below 0.03%, and strength comes from precipitation hardening in the nickel-molybdenum-titanium system.<\/p>\n<p>The practical consequence is this: the material is easily machined in the soft martensitic condition and is then aged at a low temperature of around 480-510 \u00b0C. That low temperature reduces post-machining distortion to almost nothing, which is the decisive advantage for complex parts held to tight tolerances. Weldability is also very good for a steel in this strength class.<\/p>\n<p>It is used in aerospace and defence for rocket motor cases, landing gear parts and critical fasteners; in tooling for injection and die casting moulds working under high load; and in motorsport for shafts and drivetrain components.<\/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 \u00b7 Maraging 350<\/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 \u2014 Nickel<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">18.5% (nominal)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Co \u2014 Cobalt<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">12.0% (nominal)<\/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 \u2014 Molybdenum<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">4.8% (nominal)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Ti \u2014 Titanium<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">1.40% (nominal)<\/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 \u2014 Aluminium<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">0.05 \u2013 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%;\">C \u2014 Carbon<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">0.03% max<\/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;\">Fe \u2014 Iron<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Balance<\/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;\">Heat Treatment and Mechanical Properties \u00b7 Maraging 350<\/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 annealing<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">820 \u2013 860 \u00b0C<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Ageing<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">480 \u2013 510 \u00b0C<\/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;\">Tensile strength (R<sub>m<\/sub>)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">2415 MPa (350 ksi)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Yield strength (R<sub>p0.2<\/sub>)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">2275 MPa (330 ksi)<\/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;\">Hardness<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">55 \u2013 60 HRC<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Elongation<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">8% (4D)<\/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 350<\/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 350<\/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;\">6515<\/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<div style=\"margin:28px 0 0;padding:14px 16px;border:1px solid #e0e0e0;background:#FBFCFD;font-size:15px;line-height:1.7;\">\n<p style=\"margin:0 0 10px;\"><span style=\"color:#DD3333;font-weight:700;\">\u2192<\/span> Contact us for Maraging 350 stock availability, sizes and AMS 6515 certified supply.<\/p>\n<p style=\"margin:0;\"><a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/contact\/\" style=\"display:inline-block;background:#DD3333;color:#ffffff;font-weight:700;font-size:14px;padding:9px 16px;text-decoration:none;\">Request a quote<\/a><\/p>\n<\/div>\n<div 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\/maraging-300\/\" style=\"color:#24BEE5;font-weight:600;text-decoration:none;\">Maraging 300<\/a> &nbsp;\u00b7&nbsp; <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/maraging-250\/\" style=\"color:#24BEE5;font-weight:600;text-decoration:none;\">Maraging 250<\/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\/300m\/\" style=\"color:#24BEE5;font-weight:600;text-decoration:none;\">300M<\/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-zengin --><\/p>\n<h4 id=\"dm-b0\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">What Maraging 350 Is \u2014 and Why It Is the Extreme End of the Family<\/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\">2310<\/text><rect x=\"16\" y=\"68\" width=\"642.1\" height=\"15\" fill=\"#12303f\"\/><text x=\"665.1\" y=\"80\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">2275<\/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;\">30-35<\/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;\">53-58<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">2275-2320<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">2310-2415<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">6-8%<\/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=\"70.0\" y1=\"68\" x2=\"70.0\" y2=\"94\" stroke=\"#c7d2d9\" stroke-width=\"1.5\"\/><circle cx=\"70.0\" cy=\"68\" r=\"5\" fill=\"#12303f\"\/><text x=\"70.0\" y=\"102\" 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=\"117\" 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><line x1=\"670.0\" y1=\"68\" x2=\"670.0\" y2=\"94\" stroke=\"#c7d2d9\" stroke-width=\"1.5\"\/><circle cx=\"670.0\" cy=\"68\" r=\"5\" fill=\"#12303f\"\/><text x=\"670.0\" y=\"102\" 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=\"117\" 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;\">53-58 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;\">53-60 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 long cycle (specific to grade 350)<\/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 long cycle (specific to grade 350)<\/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;\">12 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 (argon atmosphere recommended)<\/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;\">53-58 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 short \/ high-temperature cycle<\/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 short \/ high-temperature cycle<\/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;\">510 \u00b0C (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 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;\">56-60 HRC (SSA Corp)<\/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. For grade 350 the LIGO specification gives 12 hours at 480 \u00b0C while SSA Corp gives 6 hours at 482-496 \u00b0C or 3 hours at 510 \u00b0C. All three cycles are shown as separate rows; confirm from the order specification.<\/div>\n<\/div>\n<p><!-- \/dm-diy-isil --><\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\">Maraging 350 (18Ni-350 \/ C350 \/ Vascomax C350 \/ ATI C-350) is the <b>highest-strength and lowest-toughness<\/b> step of the 18Ni maraging family. The 350 in the name denotes the nominal <b>350 ksi (2413 MPa) tensile class<\/b> in the aged condition; the measured <b>0.2% yield strength lies in the 2275\u20132365 MPa band<\/b>. It hardens not through carbon but through <b>intermetallic precipitation<\/b>; the low carbon that defines the family (<b>C \u22640.03%<\/b>), quench-free hardening and freedom from distortion all apply here too. But <b>this grade is a toughness bargain, and we are obliged to say so plainly.<\/b><\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\">The distinguishing property in one sentence: <b>Maraging 350 exists for duties where the absolute ceiling of tensile strength is what matters, where crack tolerance does not govern the design, and where the environment is dry.<\/b> Put in the wrong place, it does not forgive what the other grades in the family forgive.<\/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;\">Identity \u00b7 Maraging 350<\/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;\">Family designation<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>18Ni-350<\/b> \u00b7 <b>C350<\/b> \u00b7 Vascomax C350 \u00b7 ATI C-350<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>UNS number<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>CONFLICT \u2014 published here honestly.<\/b> Supplier sources give <b>K93160<\/b> and <b>K93540<\/b>; some pages give <b>K93120<\/b>, which <b>belongs to Maraging 300 and is wrong<\/b>. On orders and certificates, rely on <b>AMS 6515 plus the chemistry<\/b>, not on the UNS number<\/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;\">AMS<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>AMS 6515<\/b> \u2014 titled: <i>&#8220;Steel, Maraging, Bars, Forgings, Tubing, and Rings, 18.5Ni 12.0Co 4.9Mo 1.40Ti 0.10Al, Double Vacuum Melted, Annealed&#8221;<\/i><\/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;\"><b>MIL-S-46850<\/b>, 350 ksi class (including fracture-toughness requirements)<\/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;\"><b>EN \/ Werkstoff<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>\u2014 no confirmed W.Nr. or EN designation was found.<\/b> The 250 grade has <b>1.6359 \/ X2NiCoMo18-8-5<\/b>; no comparable European designation could be confirmed for the 350. <b>Do not invent a W.Nr.<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Melt route<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>Double vacuum: VIM + VAR.<\/b> &#8220;Double Vacuum Melted&#8221; appears in the AMS 6515 title itself \u2014 <b>here the melt route is part of the specification, not an option<\/b><\/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;\">Delivery condition<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>Annealed (solution treated)<\/b>, <b>30\u201335 HRC<\/b>. <b>NOT stainless<\/b> \u2014 no significant chromium, no passive film<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Export control<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>Yes, and beyond argument at this grade.<\/b> The aged tensile strength (~2350\u20132430 MPa) is <b>well above<\/b> the <b>&#8220;1.95 GPa or more&#8221;<\/b> threshold in the gas-centrifuge control text<\/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;\">Where it sits in the family: cobalt and titanium jump here<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\">The design logic of the 18Ni family is visible in one line: <b>cobalt and titanium rise together, molybdenum stays nearly constant, nickel and carbon never change.<\/b> Titanium is the direct fuel for the <b>Ni\u2083Ti<\/b> precipitate; cobalt forms no precipitate of its own but lowers the solubility of molybdenum in the matrix and thereby <b>forces Mo to precipitate as Ni\u2083Mo and Fe\u2082Mo<\/b>. In the 350 grade both elements jump \u2014 and the bill is paid directly out of toughness.<\/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;\">The 18Ni Maraging Family \u00b7 Where 350 Sits<\/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;\">18Ni-200<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Co 8\u20139% \u00b7 Ti 0.15\u20130.25% \u00b7 Mo 3.0\u20133.5% \u00b7 yield <b>~1379 MPa<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">18Ni-250<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Co 7.0\u20138.5% \u00b7 Ti 0.30\u20130.50% \u00b7 Mo 4.6\u20135.2% \u00b7 yield <b>~1724 MPa<\/b>. Detail: <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/maraging-250\/\">Maraging 250<\/a><\/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;\">18Ni-300<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Co 8.0\u20139.5% \u00b7 Ti 0.50\u20130.80% \u00b7 Mo 4.6\u20135.2% \u00b7 yield <b>~2068 MPa<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>18Ni-350<\/b><br \/>(this page)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Co <b>11.5\u201312.5%<\/b> \u00b7 Ti <b>1.30\u20131.60%<\/b> \u00b7 Mo 4.6\u20135.2% \u00b7 yield <b>~2275\u20132365 MPa<\/b>, tensile <b>~2350\u20132430 MPa<\/b>. <b>Cobalt rises about 30% over the 300 grade and titanium roughly doubles; molybdenum does not change.<\/b> All of the extra strength comes from Co + Ti<\/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;\"><b>What never changes<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Ni <b>17\u201319%<\/b>, <b>C \u22640.03%<\/b> and Al 0.05\u20130.15% are identical across all four steps. The family is four settings of one metallurgical idea<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Additions unique to 350<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Datasheets show <b>zirconium ~0.01%<\/b> and <b>boron ~0.003%<\/b> in the 350 composition \u2014 two trace additions absent from the standard listings of the other grades. They are typically added as <b>grain refiners<\/b>, but that function could not be explicitly confirmed in a mill document<\/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;\">THE TOUGHNESS PENALTY \u2014 the most important section on this page<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>Showing the strength table when selling Maraging 350 is easy; the engineering responsibility is to show the toughness table at the same size.<\/b> The values below come from a single defence report in which all four grades were measured <b>in the same laboratory, in the same programme<\/b>, so they are directly comparable. (They are <b>K<sub>Q<\/sub><\/b> values, i.e. provisional fracture-toughness results whose validity conditions were not separately confirmed \u2014 read them as a <b>ratio between grades<\/b>, not as absolute design values.)<\/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;\">Toughness Ladder Measured in One Programme \u2014 THE HONEST TABLE<\/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;\">18Ni-200<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">K<sub>Q<\/sub> <b>130.9 ksi\u221ain \u2248 144 MPa\u221am<\/b> \u00b7 Charpy <b>60.9 ft-lb \u2248 83 J<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">18Ni-250<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">K<sub>Q<\/sub> <b>104.4\u2013112.5 ksi\u221ain \u2248 115\u2013124 MPa\u221am<\/b> \u00b7 Charpy <b>24.7\u201330.2 ft-lb \u2248 33\u201341 J<\/b><\/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;\">18Ni-300<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">K<sub>Q<\/sub> <b>~70 ksi\u221ain \u2248 77 MPa\u221am<\/b> \u00b7 Charpy <b>17.5\u201318.1 ft-lb \u2248 24 J<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>18Ni-350<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">K<sub>Q<\/sub> <b>35.2 ksi\u221ain \u2248 39 MPa\u221am<\/b> \u00b7 Charpy <b>8.6 ft-lb \u2248 12 J<\/b><\/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;\"><b>What it means<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Going from 250 to 350 raises yield by <b>35%<\/b> while fracture toughness falls to <b>one third<\/b> and Charpy energy to <b>one quarter<\/b>. Even from 300 to 350, yield rises about <b>12%<\/b> while toughness <b>halves<\/b>. <b>This is not a fine adjustment, it is a change of regime<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>The specification side<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">MIL-S-46850B requires a minimum fracture toughness of <b>50 ksi\u221ain (\u224855 MPa\u221am)<\/b> for the 300 class; <b>the measured 350 value (35.2 ksi\u221ain) is below that<\/b>. One grade&#8217;s minimum cannot be applied to another \u2014 read the minimum that actually applies to 350 <b>from your own specification revision<\/b><\/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;\"><b>Critical flaw size<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">As toughness falls, so does the flaw size that drives unstable crack growth at design stress. <b>At around 39 MPa\u221am that size approaches the limit of what routine non-destructive inspection can reliably find<\/b><\/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;\">Why there is no carbon, and how the mechanism is pushed in the 350<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\">A conventional alloy steel takes its hardness from <b>carbon<\/b> trapped in the martensite lattice by quenching, and pays for it in brittleness, quench cracking and hydrogen cracking. In maraging steel carbon is deliberately held at <b>\u22640.03%<\/b>; the structure that air cools from high temperature is not a hard carbon martensite but a <b>soft, ductile iron-nickel martensite<\/b> at <b>30\u201335 HRC<\/b>. All of the strength is added afterwards, during ageing, by nanoscale <b>Ni\u2083Mo<\/b>, <b>Ni\u2083Ti<\/b> and <b>Fe\u2082Mo<\/b> intermetallics precipitating on the high dislocation density of the martensite itself.<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>In the 350 grade this mechanism is pushed to its limit.<\/b> Raising titanium to 1.30\u20131.60% markedly increases the volume fraction of Ni\u2083Ti precipitates; raising cobalt to 12% leaves even less molybdenum dissolved in the matrix. The result is a <b>very dense, very fine precipitate distribution<\/b> in which dislocation motion is almost completely locked. What is gained is a yield strength of order 2300 MPa; <b>what is lost is the ability to absorb energy by plastic deformation at a crack tip<\/b> \u2014 and that is exactly what the collapse in fracture toughness and Charpy energy measures. <b>High titanium also increases the tendency to form coarse Ti-rich particles at grain boundaries<\/b>, which act as crack initiators \u2014 that is why double-vacuum melting is written into the specification for this grade.<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>Overageing and reverted austenite.<\/b> If the ageing temperature or time is exceeded, the precipitates coarsen and <b>austenite re-forms (reverted austenite)<\/b> in nickel-rich regions. Academic work on 18Ni-350 has measured this behaviour in detail: <b>during overageing at 640 \u00b0C the volume fraction of austenite rises with time<\/b>; yield and tensile strength fall while tensile ductility rises. Impact toughness behaves <b>in two stages<\/b>: in the early stages of overageing a small amount of reverted austenite appears <b>beneficial<\/b>, but with prolonged overageing the coarsened <b>titanium-nickel intermetallics initiate cracks and produce severe embrittlement<\/b>. <b>The practical consequence: at this grade, temperature control of the ageing furnace is a quality record.<\/b><\/p>\n<h4 id=\"dm-b1\" 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, 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 6515<\/b> \u00b7 MIL-S-46850 (350 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;\">MIL-S-46850 (350 ksi class) \u2014 there is no verified AMS sheet or plate number for this grade; ASTM A538 covers only the 200\/250\/300 classes<\/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 (350 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 consumables<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">No verified AMS welding wire number was found for this grade<\/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;\"><b>The standards landscape for Maraging 350 is NARROWER than for the other grades in the family, and that is a commercial fact the sales side needs to know.<\/b> The 250 grade has a dedicated AMS number for sheet and plate (AMS 6520); so does the 300 grade (AMS 6521). <b>For the 350 grade, none was found.<\/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 350<\/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;\"><b>Bar \u00b7 forgings \u00b7 TUBING \u00b7 rings<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>AMS 6515<\/b> \u2014 the title reads exactly <i>&#8220;Bars, Forgings, Tubing, and Rings&#8221;<\/i>, <b>double vacuum melted, supplied annealed<\/b>. Note: <b>tubing IS within this specification<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Sheet \u00b7 strip \u00b7 plate<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>\u2014 NO SEPARATE AMS NUMBER WAS FOUND.<\/b> AMS 6520 exists for the 250 and AMS 6521 for the 300; <b>no counterpart for the 350 could be confirmed<\/b>. For plate and sheet the only verified route is <b>MIL-S-46850<\/b><\/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;\">Military (all forms)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>MIL-S-46850<\/b>, 350 ksi class. Titled <i>&#8220;Steel: Bar, Plate, Sheet, Strip, Forgings, and Extrusions, 18 Percent Nickel Alloy, Maraging, 200 ksi, 250 ksi, 300 ksi, and 350 ksi&#8221;<\/i>. <b>It is the ONLY verified document covering plate, sheet, strip and extrusions<\/b>, and it <b>carries fracture-toughness requirements<\/b> \u2014 particularly valuable at this grade<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Pressure-vessel plate<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>\u2014 NONE.<\/b> ASTM A538 \/ A538M contains only <b>Grade A (MAR-18-200), Grade B (MAR-18-250) and Grade C (MAR-18-300)<\/b>. <b>There is no A538 grade for the 350<\/b> (and A538 is in any case an old, no longer active document)<\/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;\">Forgings (ASTM route)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">ASTM <b>A579 \/ A579M<\/b> covered the maraging grades in the range <b>Grades 71\u201375<\/b>. <b>IMPORTANT: A579 was WITHDRAWN by ASTM in May 2024 with no replacement.<\/b> In addition, <b>which grade number corresponds to the 350 could not be independently confirmed<\/b>. Do not use A579 in new contracts<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>EN \/ Werkstoff<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>\u2014 no confirmed equivalent was found.<\/b> If a European customer asks for a W.Nr., the honest answer is: <b>&#8220;This grade has no confirmed Werkstoff number; we work from the AMS 6515 chemistry and mechanicals.&#8221;<\/b><\/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;\">ASME Section IX P\/F-No<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>\u2014 could not be confirmed;<\/b> no published ASME P-number exists for the 18Ni maraging steels<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">NACE MR0175 \/ ISO 15156<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>\u2014 NOT listed.<\/b> Never offer it for H\u2082S service<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<h4 id=\"dm-b2\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">ASME Code Acceptance and Pressure-Equipment Status<\/h4>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>The short answer: Maraging 350 is not an ASME pressure-vessel code material<\/b> \u2014 and at this grade that is not merely a missing document, it is also the engineering-correct outcome. Code design rests on assumptions of ductility and damage tolerance; <b>a fracture toughness of order 39 MPa\u221am is far below the behaviour the code expects of pressure-boundary materials.<\/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;\">Code and Vessel Status \u00b7 Maraging 350<\/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;\"><b>ASME Section VIII Div. 1 \/ Div. 2<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>NO confirmed acceptance.<\/b> No SA-\/SB- numbered material specification and no allowable-stress table 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%;\"><b>ASME Section I \/ B31.1 \/ B31.3<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>NO confirmed acceptance<\/b><\/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;\"><b>No A538 route either<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Even the old pressure-vessel plate standard covering the family <b>excludes the 350 grade<\/b> (only 200\/250\/300) \u2014 historically it was not regarded as a vessel material either<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>What is actually done<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">The 350 grade is used not as a pressure vessel but as a structural and tooling material under <b>aerospace and military specification regimes<\/b> (AMS 6515 + MIL-S-46850 + customer drawing)<\/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;\"><b>Wording for a quotation<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">If the customer asks for &#8220;ASME code Maraging 350&#8221;, the honest answer is: <b>&#8220;This material is not listed in the ASME BPVC; if code coverage is required, a code case or a different material is needed \u2014 and at this strength class we would recommend considering a lower grade on toughness grounds.&#8221;<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Europe (PED)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">No harmonised EN product standard was found and <b>not even a confirmed W.Nr. exists<\/b>. Use under the PED requires a <b>Particular Material Appraisal (PMA)<\/b> and will be difficult on toughness grounds<\/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;\">Product Forms With NO Standard \u2014 the Commercially Valuable Section<\/h4>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>This is the section your sales engineers should memorise.<\/b> The list of forms that can honestly be sold &#8220;to a standard&#8221; for Maraging 350 is short: <b>bar, forgings, rings, tubing<\/b> (AMS 6515) and <b>plate, sheet, strip, extrusions<\/b> (via the MIL-S-46850 route only). Everything else is sold <b>to a mill specification and a customer drawing<\/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;\">Specification Gaps for Maraging 350<\/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;\"><b>AMS for sheet \u00b7 plate \u00b7 strip<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>NONE.<\/b> It exists for the 250 (AMS 6520) and the 300 (AMS 6521); <b>none was found for the 350<\/b>. If an aerospace customer asks for &#8220;350 plate to AMS&#8221;, the honest answer is: <b>&#8220;There is no AMS number; it is MIL-S-46850 350 ksi class, or a mill specification plus customer acceptance criteria.&#8221;<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Cold-drawn wire \u00b7 spring wire<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>NO verified ASTM\/AMS\/EN wire product specification.<\/b> Maraging wire is produced and sold, but <b>to a mill specification<\/b>. <b>Additional warning:<\/b> at this toughness level the tolerance for surface defects in drawn wire is very narrow \u2014 put the acceptance criteria in the contract<\/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;\"><b>Castings<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>NO verified casting product specification for 18Ni-350.<\/b> <b>And it is not recommended on engineering grounds either:<\/b> the unavoidable segregation and coarse grain of a cast structure would further reduce a toughness that is already 39 MPa\u221am. <b>Machine from forging<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Welded pipe \u00b7 fittings \u00b7 flanges<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>NO verified specification.<\/b> AMS 6515 covers <b>seamless tubing<\/b> only<\/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;\"><b>Bolts \u00b7 nuts \u00b7 fasteners<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>NO dedicated bolting specification.<\/b> Parts are made <b>from AMS 6515 bar, to the buyer&#8217;s drawing<\/b>. <b>At this grade the thread root, radii and surface finish are critical design parameters<\/b> \u2014 notch sensitivity is high<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Welding wire \u00b7 covered electrodes<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>NO verified AWS consumable classification.<\/b> The practice is <b>matching-composition wire<\/b><\/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;\"><b>Additive-manufacturing powder<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>No dedicated powder specification number was found for the 350 grade.<\/b> The common maraging powder on the market is <b>1.2709 \/ X3NiCoMoTi18-9-5 (MS1)<\/b>, and that composition is <b>roughly the 300 grade, not the 350<\/b><\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<h4 id=\"dm-b4\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Chemical Composition<\/h4>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>The nominal mill composition is 18.5Ni \u2013 12.0Co \u2013 4.8Mo \u2013 1.40Ti \u2013 0.10Al, balance iron.<\/b> The AMS 6515 title carries these nominal values directly. The band values are compiled from supplier specification tables.<\/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 \u00b7 Maraging 350, weight %<\/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;\"><b>Carbon (C)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>\u22640.03<\/b> \u2014 the defining limit of the family. <b>It matters even more at this grade:<\/b> with high titanium it forms carbonitrides at grain boundaries and further reduces an already low toughness<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Nickel (Ni)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>18.00\u201319.00<\/b> (nominal 18.50) \u2014 same band in all four grades<\/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;\"><b>Cobalt (Co)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>11.50\u201312.50<\/b> (nominal 12.00) \u2014 <b>about 30% more than the 300 grade.<\/b> It forms no precipitate of its own; it lowers molybdenum solubility and forces Mo out of solution<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Molybdenum (Mo)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>4.60\u20135.20<\/b> (nominal 4.80\u20134.90) \u2014 <b>IDENTICAL to the 250 and 300.<\/b> The strength of the 350 does not come from molybdenum<\/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;\"><b>Titanium (Ti)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>1.30\u20131.60<\/b> (nominal 1.40) \u2014 <b>roughly twice the 300 grade and three to four times the 250.<\/b> It is the direct fuel for the <b>Ni\u2083Ti<\/b> precipitate and the single element that makes the 350 what it is<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Al \u00b7 Si \u00b7 Mn \u00b7 P \u00b7 S<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Al <b>0.05\u20130.15<\/b> (nominal 0.10, deoxidiser) \u00b7 Si \u22640.10 \u00b7 Mn \u22640.10 \u00b7 P \u22640.01 \u00b7 S \u22640.01<\/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;\"><b>Zirconium (Zr)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>~0.01<\/b> \u2014 listed in the 350 composition on datasheets and absent from the standard listings of the other grades. Its typical function is <b>grain refinement<\/b>; that function could not be explicitly confirmed in a mill document<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Boron (B)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>~0.003<\/b> \u2014 likewise listed only in the 350 composition; a grain-boundary effect is expected but <b>not independently confirmed<\/b><\/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;\">Cr \u00b7 Cu \u00b7 Fe<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Cr and Cu at residual level \u2014 <b>chromium confers no passivity<\/b>; Fe balance<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>Three lines that actually matter on a certificate.<\/b> (1) <b>Titanium.<\/b> The difference between 1.30% and 1.60% is not small at this grade: the top of the band means higher strength, the bottom means higher toughness. <b>If toughness is critical, narrow the band and write it into the order.<\/b> (2) <b>Carbon and nitrogen.<\/b> Working together with high titanium, these two form coarse TiC\/TiN particles at grain boundaries, and in the 350 those are crack initiation sites. (3) <b>Melt route.<\/b> AMS 6515 requires <b>double vacuum (VIM + VAR)<\/b>. <b>That is not negotiable at this grade<\/b> \u2014 the link between inclusion cleanliness and measured toughness is far tighter here than in the other grades of the family.<\/p>\n<h4 id=\"dm-b5\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Mechanical Properties<\/h4>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>Three separate sets of numbers circulate in this section and must not be mixed:<\/b> specification minima, typical mill values and independent laboratory measurements. <b>And the sources diverge badly on elongation<\/b> \u2014 all of them are given below exactly as published.<\/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;\">Aged Condition \u00b7 Values by Source<\/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;\"><b>Minimum values<\/b><br \/>(supplier specification table)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Tensile <b>\u22652344 MPa<\/b> \u00b7 Yield <b>\u22652275 MPa<\/b> \u00b7 Elongation <b>\u22652.8%<\/b> \u00b7 <b>\u226556 HRC<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Aerospace datasheet<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Yield <b>330 ksi = 2275 MPa<\/b> \u00b7 Tensile <b>350 ksi = 2413 MPa<\/b> \u00b7 Elongation <b>8% (4D)<\/b><\/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;\"><b>Typical mill value<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Hardness <b>57 HRC<\/b> \u00b7 Tensile <b>342 ksi = 2358 MPa<\/b> \u00b7 Yield <b>336 ksi = 2317 MPa<\/b> \u00b7 Elongation <b>6.2%<\/b> \u00b7 Reduction of area <b>28%<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Independent measurement (NASA)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Yield <b>2365 MPa<\/b> \u00b7 Tensile <b>2432 MPa<\/b> \u00b7 Elongation <b>4.0%<\/b><\/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;\"><b>Independent measurement (defence report)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Yield <b>321 ksi = 2213 MPa<\/b> \u00b7 Tensile <b>329 ksi = 2268 MPa<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>ELONGATION \u2014 OPEN CONFLICT<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Published values scatter across four separate figures: <b>2.8% \u00b7 4.0% \u00b7 6.2% \u00b7 8.0%<\/b>. This comes from differences in gauge length (4D\/5D), orientation (longitudinal\/transverse), section size and ageing cycle. <b>Publishing a single elongation figure is misleading; state in the contract which gauge length acceptance is based on<\/b><\/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;\">Solution annealed (as delivered)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Hardness <b>30\u201335 HRC<\/b> \u2014 &#8220;very tough, relatively soft, readily machined or formed&#8221; (mill wording). <b>No verified annealed tensile or yield figure was found for the 350<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Fracture toughness K<sub>Q<\/sub><\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>35.2 ksi\u221ain \u2248 39 MPa\u221am<\/b> \u2014 in the same programme 115\u2013124 MPa\u221am was measured for the 250 and ~77 MPa\u221am for the 300<\/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;\"><b>Charpy impact<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>8.6 ft-lb \u2248 12 J<\/b> \u2014 <b>less than one third<\/b> of the 250 grade<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">High temperature<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>Tensile retained to about 450 \u00b0C<\/b>; above that overageing begins<\/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;\">Low temperature<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>Notch impact toughness is retained at \u221250 \u00b0C<\/b> (mill wording) \u2014 but the room-temperature value is already low<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>The commercial conclusion to draw from this table.<\/b> In Maraging 350 <b>the gap between minimum and typical is narrow and the margin is small<\/b>: minimum yield 2275 MPa against a typical 2317 MPa. The alloy <b>runs at the edge of its own specification<\/b>. The same is even more marked in elongation \u2014 a 2.8% minimum against a 6.2% typical. <b>A small deviation in the ageing cycle can put a part outside specification.<\/b> At this grade, manage heat treatment with furnace records, thermocouple calibration and witness coupons.<\/p>\n<h4 id=\"dm-b6\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Physical Properties<\/h4>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>The physical properties of the 350 grade differ measurably from the 250<\/b>, and the difference is real \u2014 12% cobalt raises both density and elastic modulus. The values below come from the same mill datasheet family and are therefore <b>directly comparable with the 250<\/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;\">Physical Properties \u00b7 Maraging 350 (compared with the 250)<\/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<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>0.292 lb\/in\u00b3 \u2248 8.08 g\/cm\u00b3<\/b> \u00b7 <b>Maraging 250: 0.289\u20130.290 lb\/in\u00b3 \u2248 8.0 g\/cm\u00b3<\/b>. <b>The 350 is heavier<\/b> \u2014 do not ignore this in specific-strength calculations<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Modulus of elasticity<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>29.0 \u00d7 10\u2076 psi \u2248 200 GPa<\/b> \u00b7 <b>Maraging 250: 27.0 \u00d7 10\u2076 psi \u2248 186 GPa<\/b>. <b>The 350 is markedly stiffer<\/b><\/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;\">Coefficient of thermal expansion<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>6.3 \u00d7 10\u207b\u2076 \/\u00b0F \u2248 11.3 \u00d7 10\u207b\u2076 \/\u00b0C<\/b> \u00b7 <b>Maraging 250: 5.6 \u00d7 10\u207b\u2076 \/\u00b0F \u2248 10.1 \u00d7 10\u207b\u2076 \/\u00b0C<\/b>. <b>The 350 expands more<\/b> \u2014 allow for it in tooling and rigid joint design<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Thermal conductivity<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>\u2014 no verified value was found for the 350 grade.<\/b> The figures circulating for the family (19.6\u201325.6 W\/m\u00b7K) belong to <b>the 250 grade<\/b> and even those conflict with one another. <b>Do not publish a number for the 350<\/b><\/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;\"><b>Specific heat \u00b7 resistivity \u00b7 melting range<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>\u2014 no verified values were found for the 350 grade.<\/b> It is known across the family that ageing lowers resistivity markedly (for the 250: 60 \u03bc\u03a9\u00b7cm annealed \u2192 38 \u03bc\u03a9\u00b7cm aged)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Magnetic behaviour<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>Ferromagnetic<\/b> \u2014 a martensitic ferrous alloy; <b>unusable where non-magnetic material is required<\/b><\/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;\">Service temperature<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Tensile retained to ~450 \u00b0C; the practical continuous-service limit is <b>~400\u2013450 \u00b0C<\/b>, above which it overages<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<h4 id=\"dm-b7\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Heat Treatment and Thermal Stability<\/h4>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>A common misconception needs correcting here: Maraging 350 is not aged LONGER than the 250 \u2014 it may be aged HOTTER.<\/b> Mill datasheets publish two alternative cycles, and the higher-temperature one is the <b>SHORTER<\/b> of the two. In the same defence programme the 250 grade was aged at <b>900 \u00b0F for 3 hours<\/b> and the 350 grade at <b>950 \u00b0F for 3 hours<\/b> \u2014 same time, different temperature.<\/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;\">Heat Treatment Route \u00b7 Maraging 350<\/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;\"><b>1. Solution anneal<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>815\u2013830 \u00b0C (1500\u20131525 \u00b0F)<\/b>, <b>1 hour per inch<\/b> (about 1 hour per 25 mm), then <b>air cool<\/b>. Result: <b>30\u201335 HRC<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>2a. Ageing \u2014 standard<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>482\u2013496 \u00b0C (900\u2013925 \u00b0F) for 6 hours<\/b>, air cool \u2192 <b>55\u201360 HRC<\/b><\/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;\"><b>2b. Ageing \u2014 hotter \/ shorter<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>510 \u00b0C (950 \u00b0F) for 3 hours<\/b>, air cool \u2192 <b>56\u201360 HRC<\/b>. The mechanical values measured in the defence programme were obtained with this cycle<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Which cycle to use<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>Whatever the customer specification says.<\/b> The two are not &#8220;equivalent&#8221;; even where the hardness band is similar, the precipitate distribution and therefore the toughness differ. <b>Do not substitute a cycle of your own<\/b><\/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;\"><b>Modified cycle for tooling<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Die-casting dies: <b>anneal at 815\u2013830 \u00b0C for 1 hour per inch, then age at 527\u2013538 \u00b0C (980\u20131000 \u00b0F) for 6 hours<\/b>, after finish machining. The higher ageing temperature trades strength for <b>thermal-fatigue resistance<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Quenching \u00b7 atmosphere<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>There is NO quench<\/b>; air cooling suffices and the alloy <b>through-hardens<\/b> regardless of section thickness. With essentially no carbon there is <b>no decarburisation risk<\/b> either<\/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;\"><b>Dimensional change<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>No separate, verified contraction figure was found for the 350 grade.<\/b> The same mill datasheet gives <b>0.0009 in\/in (\u22480.09%)<\/b> for the 250 and <b>0.001 in\/in (\u22480.10%)<\/b> for the 300; a European mill states <b>~0.05%<\/b> for the 250. <b>Run a trial piece from your own material for the 350<\/b> \u2014 the trend is for contraction to rise with titanium, but that could not be independently confirmed<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Overageing<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">If temperature or time is exceeded the precipitates coarsen and <b>reverted austenite<\/b> forms. Measurements on 18Ni-350: <b>during overageing at 640 \u00b0C the austenite volume fraction rises with time<\/b>, yield and tensile fall and tensile ductility rises; impact toughness improves at first, but with prolonged overageing the coarsened <b>Ti-Ni intermetallics initiate cracks and cause severe embrittlement<\/b><\/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;\">Re-ageing<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Re-ageing an already aged part is <b>a route into overageing<\/b>. The only reset is a <b>fresh solution anneal plus a fresh age<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Process control<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>At this grade heat treatment is a quality record.<\/b> Because the margin between minimum and typical is narrow, calibrated thermocouples, furnace surveys, witness coupons and furnace records are <b>a requirement, not a recommendation<\/b><\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<h4 id=\"dm-b8\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Welding<\/h4>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>The family&#8217;s greatest advantage \u2014 needing no preheat \u2014 applies to the 350 grade too, but here we must be honest: being weldable is not the same as being reliable in the welded condition.<\/b> With carbon at \u22640.03% no hard carbon martensite forms in the HAZ, the risk of hydrogen cracking is practically absent, and mill datasheets state <b>&#8220;good weldability without preheating or post heating&#8221;<\/b> and <b>&#8220;good repair weldability&#8221;<\/b>. But when the parent metal&#8217;s fracture toughness is already <b>~39 MPa\u221am<\/b>, every loss of toughness in the HAZ has proportionally far heavier consequences.<\/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;\">Welding \u00b7 Maraging 350<\/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;\"><b>Preheat<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>NOT REQUIRED<\/b> \u2014 the common statement across mill and service-centre datasheets. The reason is directly the very low carbon<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Condition for welding<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>The solution-annealed (soft) condition.<\/b> The part is welded, then <b>the whole structure is aged together<\/b><\/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;\"><b>Post-weld treatment<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>Ageing is mandatory.<\/b> The weld bead hardens on the same cycle as the parent metal with no separate solution treatment of the assembly \u2014 <b>this is the maraging family&#8217;s greatest manufacturing advantage<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Filler metal<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>Matching-composition wire.<\/b> No verified AWS classification<\/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;\">Processes<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>TIG (GTAW), MIG (GMAW), electron beam and laser<\/b> are all used in this family. <b>At the 350 grade the low-heat-input processes (EB, laser) should be preferred<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Heat input<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>Keep it as low as possible.<\/b> High heat input and slow cooling produce <b>reverted austenite<\/b> and a coarsened structure in the HAZ, and that zone does not fully recover on ageing<\/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;\"><b>HAZ toughness \u2014 CRITICAL<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>After post-weld ageing the HAZ toughness does not fully match the parent metal.<\/b> Because the parent toughness is already <b>~39 MPa\u221am<\/b>, <b>at this grade that gap directly threatens the design<\/b>. Where fracture toughness is contractual, take the specimen <b>from the weld zone without exception<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Honest recommendation<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>If you are designing a welded structure in which crack tolerance is critical, seriously consider <\/b><a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/maraging-250\/\">Maraging 250<\/a><b> or the 300 grade instead of the 350.<\/b> The natural home of the 350 is not welded structure but <b>solid machined parts and tooling<\/b><\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<h4 id=\"dm-b9\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Machining<\/h4>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>The rule is the same and matters even more here:<\/b> do the roughing and every possible finishing operation in the <b>solution-annealed (soft, 30\u201335 HRC) condition<\/b>, then age. After ageing the material is at <b>55\u201360 HRC<\/b>, the hardest state in the family to machine. The parameters below are the mill datasheet&#8217;s <b>annealed-condition<\/b> starting points, given for the family generally.<\/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;\">Starting Parameters \u00b7 SOLUTION-ANNEALED condition (mill data)<\/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;\">Turning \u00b7 HSS (M2 \/ T-15)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>24 m\/min (80 sfm)<\/b> \u00b7 feed <b>0.23 mm\/rev<\/b> \u00b7 depth of cut <b>1.5 mm<\/b> \u00b7 <b>soluble oil 1:20<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Turning \u00b7 carbide (C3)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>145 m\/min (475 sfm)<\/b> \u00b7 feed <b>0.23 mm\/rev<\/b> \u00b7 <b>soluble oil 1:20<\/b><\/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;\">Face milling \u00b7 HSS (M2 \/ M-7)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>43 m\/min (140 sfm)<\/b> \u00b7 <b>0.13 mm\/tooth<\/b> \u00b7 depth <b>1.5 mm<\/b> \u00b7 <b>highly chlorinated oil<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Face milling \u00b7 carbide (C2)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>101 m\/min (330 sfm)<\/b> \u00b7 <b>0.13 mm\/tooth<\/b> \u00b7 depth <b>1.5 mm<\/b> \u00b7 <b>dry<\/b><\/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;\">Peripheral end milling \u00b7 HSS (M2)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>69 m\/min (225 sfm)<\/b> \u00b7 <b>0.10 mm\/tooth<\/b> \u00b7 depth <b>6.4 mm<\/b> \u00b7 <b>soluble oil 1:20<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">End-mill slotting \u00b7 HSS (M2)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>43 m\/min (140 sfm)<\/b> \u00b7 <b>0.05 mm\/tooth<\/b> \u00b7 depth <b>6.4 mm<\/b> \u00b7 <b>highly chlorinated oil<\/b><\/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;\">Drilling \u00b7 HSS (M1)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>30 m\/min (100 sfm)<\/b> \u00b7 <b>0.13 mm\/rev<\/b> \u00b7 \u00d812.7 mm \u00b7 <b>highly sulphurised oil<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Reaming \u00b7 HSS (M2)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>18 m\/min (60 sfm)<\/b> \u00b7 <b>0.23 mm\/rev<\/b> \u00b7 \u00d812.7 mm \u00b7 <b>highly sulphurised oil<\/b><\/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;\">Tapping \u00b7 HSS (M1)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>46 m\/min (150 sfm)<\/b> \u00b7 \u00d812.7 mm \u00b7 <b>highly sulphurised oil<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Machining in the aged condition<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>55\u201360 HRC<\/b> \u2014 the hardest in the family. <b>Carbide or CBN is essential<\/b>, cutting speeds drop markedly, rigidity and coolant are critical. In practice <b>grinding and EDM<\/b> take over<\/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;\"><b>EDM warning \u2014 critical at 350<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">The <b>recast layer<\/b> left by EDM must be removed. It contains microcracks and, <b>in a material with 39 MPa\u221am toughness, it is a direct fatigue and fracture initiator<\/b>. Remove it by grinding, polishing or chemical etching and write that into the acceptance criteria<\/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;\">Nitriding<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\">Maraging steels <b>can be nitrided<\/b>, and this is used in tooling applications that need wear resistance. <b>The metallurgically convenient point:<\/b> nitriding temperatures overlap the alloy&#8217;s ageing band, so <b>nitriding and ageing can be combined in a single cycle<\/b>. <b>Honest limits:<\/b> (1) no verified <b>case hardness or case depth<\/b> value specific to the 350 grade was found that could be published here \u2014 the available academic work is mainly on <b>18Ni-250 and 18Ni-300<\/b>. (2) <b>Adding a hard, brittle nitride case to a material whose core toughness is already low can raise notch sensitivity<\/b>; do not skip that assessment on fatigue-loaded parts. <b>Case data must be obtained from the treatment house on a part-by-part basis.<\/b><\/p>\n<h4 id=\"dm-b10\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Corrosion \u2014 Where It Is Good, WHERE IT FAILS<\/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<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>This section must be published at least as prominently as the strength section. Maraging 350 is the family member MOST susceptible to stress-corrosion cracking, and that is not a laboratory curiosity but a measured failure mode.<\/b><\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">The basic fact: it is not stainless<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\">Maraging 350 is <b>not a stainless steel<\/b>. Chromium is a residual, not an alloying addition; <b>there is no passive oxide film<\/b>. Its corrosion resistance is comparable to that of an ordinary low-alloy martensitic steel. Bare parts will rust in humid, marine and industrial atmospheres. <b>For any service outside a dry, controlled environment, plan on conventional protection:<\/b> plating, phosphating, paint, dry-film lubricant or an oil or grease film. Suppliers selling the product as <b>&#8220;maraging 350 stainless steel&#8221;<\/b> \u2014 some of them carrying that phrase in their page addresses \u2014 are metallurgically wrong.<\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">Where it is relatively good: general corrosion rate and polishability<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\">Despite carrying no chromium, mill documents report <b>better pitting and corrosion resistance than common tool steels<\/b> and an <b>excellent polish<\/b>. General rusting advances uniformly; localised penetrating attack is not typical \u2014 commercially meaningful for tooling surfaces.<\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">WHERE IT FAILS \u2014 stress-corrosion cracking<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>The sentence &#8220;maraging steels resist stress corrosion and hydrogen embrittlement&#8221; is not merely misleading when applied to the 350 grade \u2014 it is dangerous.<\/b> An independent NASA study tested all four grades side by side and the result is unambiguous: <b>the lowest-strength grade (200) was the least susceptible and the highest-strength grade (350) the MOST susceptible.<\/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;\">Stress-Corrosion Cracking \u00b7 Four Grades Side by Side<\/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;\">18Ni-200<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>Did not fail<\/b> in salt water at stresses up to <b>90%<\/b> of yield<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">18Ni-250<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>Did not fail<\/b> in salt water at stresses up to <b>90%<\/b> of yield<\/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;\">18Ni-300<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>Failed<\/b> in salt water at <b>75%<\/b> of yield after extended exposure<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>18Ni-350<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>Failed in UNDER TWO DAYS in salt water at only 55% of yield strength.<\/b> <b>This is the single most important number on this page<\/b><\/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;\"><b>For comparison<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">K<sub>ISCC<\/sub> for the 250 grade was measured at <b>\u224844 MPa\u221am<\/b>, i.e. <b>40%<\/b> of its toughness in air. <b>No verified K<sub>ISCC<\/sub> value was found for the 350<\/b>, but applying the same ratio to a 39 MPa\u221am air toughness makes it clear <b>how little would remain<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>The harshest test medium<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">The surprising finding of the same study: <b>98% relative humidity at 35 \u00b0C<\/b> was <b>more aggressive<\/b> than alternate immersion in 3.5% NaCl or synthetic seawater. <b>&#8220;It passed the salt-water test&#8221; is not enough \u2014 humid air is enough to cause it<\/b><\/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;\"><b>Design consequence<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>Do not use the 350 grade under sustained tensile stress in a humid or salt environment.<\/b> If you must: keep the stress far below yield, plate it, relieve residual stresses and <b>define an inspection interval<\/b><\/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;\">Hydrogen embrittlement<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\">Maraging 350 <b>is susceptible to hydrogen embrittlement<\/b>, and \u2014 as in every steel at a 2300 MPa yield \u2014 that susceptibility <b>rises sharply with strength<\/b>. The practical consequences bear directly on your manufacturing route: <b>acid pickling, electroplating (cadmium and zinc especially), electropolishing and cathodic protection<\/b> all charge hydrogen into the part. For plated parts a <b>post-plating hydrogen bake-out must be treated as mandatory<\/b>, planned at a temperature that does not disturb the aged condition (the classical 190\u2013200 \u00b0C range sits far below the 482\u2013510 \u00b0C ageing temperature). <b>No verified numerical hydrogen threshold was found for the 350 grade in this research<\/b> \u2014 the plating and bake-out specification should be written jointly with the customer, and <b>mechanical plating or a plating-free solution should be preferred where possible<\/b>.<\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">Where it must not be used<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>(1) Any acid or chemical-process service<\/b> \u2014 there is no chromium. <b>(2) Under tensile stress in permanent salt-spray, marine immersion or high-humidity service<\/b> \u2014 the measured SCC behaviour forbids it. <b>(3) H\u2082S (sour) service<\/b> \u2014 it is not listed under NACE MR0175 \/ ISO 15156. <b>(4) In damage-tolerant structures where crack tolerance governs the design<\/b> \u2014 39 MPa\u221am is too low for that job. <b>(5) In welded primary structural members<\/b> \u2014 the HAZ toughness gap creates unacceptable risk at this grade. <b>(6) Anywhere that must be non-magnetic.<\/b> <b>(7) In continuous service above ~450 \u00b0C.<\/b><\/p>\n<h4 id=\"dm-b11\" 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;\">Do we really need 350, or will 300 or 250 do?<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>This is the most important question on this page, and the honest answer is usually &#8220;you do not need 350&#8221;.<\/b><br \/>The strength difference is real but smaller than you might think: the 300 grade gives <b>~2068 MPa yield<\/b> and the 350 grade <b>~2275\u20132365 MPa yield<\/b> \u2014 a difference of about <b>12\u201314%<\/b>. Against the 250 the difference is <b>35%<\/b>.<br \/><b>What you pay for it is disproportionately large.<\/b> Measured in the same laboratory: fracture toughness <b>115\u2013124 MPa\u221am for the 250, ~77 for the 300, ~39 for the 350<\/b>; Charpy energy <b>41 J \u2192 24 J \u2192 12 J<\/b>. In other words, going from 300 to 350 you give up <b>half the toughness for 12% more strength<\/b>.<br \/><b>And on the corrosion side the difference is not a step but a change of class.<\/b> In the NASA study the 250 did not fail in salt water up to 90% of yield; the 300 failed at <b>75%<\/b>; and the <b>350 failed at 55%, in under two days<\/b>.<br \/><b>Decision rule:<\/b> if your design is <b>purely stress-limited<\/b>, the part is <b>solid and machined<\/b>, the environment is <b>dry and protected<\/b>, crack tolerance does not govern, and <b>weight genuinely is critical<\/b> \u2014 the 350 is the right choice. If any one of those does not hold, <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/maraging-250\/\">Maraging 250<\/a> or the 300 grade is <b>better engineering and cheaper<\/b>. <b>A bigger number is not automatically an improvement.<\/b><\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">Is ageing longer for 350 than for 250? How should we write the cycle?<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>Contrary to the common belief, it is not longer \u2014 it is HOTTER.<\/b><br \/>Mill datasheets give two alternatives for the 350: <b>6 hours at 482\u2013496 \u00b0C (900\u2013925 \u00b0F)<\/b> (\u2192 55\u201360 HRC) or <b>3 hours at 510 \u00b0C (950 \u00b0F)<\/b> (\u2192 56\u201360 HRC). The second cycle is <b>hotter and shorter<\/b>. In the same defence programme the 250 grade was aged at <b>900 \u00b0F for 3 hours<\/b> and the 350 at <b>950 \u00b0F for 3 hours<\/b> \u2014 <b>same time, different temperature<\/b>.<br \/><b>Why:<\/b> the very high titanium of the 350 starts Ni\u2083Ti precipitation earlier and faster; holding too long coarsens the precipitates and moves the material towards the <b>reverted austenite<\/b> window. A shorter hold at a higher temperature completes the reaction while limiting coarsening.<br \/><b>How to write the cycle:<\/b> (1) <b>Never omit the solution anneal<\/b> \u2014 815\u2013830 \u00b0C, 1 hour per inch, air cool. (2) <b>Read from the customer specification which of the two ageing cycles applies<\/b>; they are not equivalent, and even where the hardness band is similar the precipitate distribution and toughness differ. (3) <b>Use witness coupons.<\/b> At this grade the margin between minimum and typical is narrow (minimum yield 2275 MPa, typical 2317 MPa) and a small furnace deviation can put the part out of specification. (4) <b>Do not re-age an already aged part<\/b>; that is a route into overageing. Resetting requires a fresh solution anneal followed by a fresh age.<\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">Is 350 stainless, and how should corrosion protection be planned?<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>No \u2014 and at this grade the corrosion plan is a design requirement, not a preference.<\/b><br \/>In Maraging 350 chromium is not an alloying addition; <b>there is no passive oxide film<\/b>. Its corrosion resistance is comparable to an ordinary low-alloy martensitic steel, not to a 300- or 400-series stainless. That some suppliers carry <b>&#8220;maraging stainless steel&#8221;<\/b> in their page titles and even in their page addresses is metallurgically wrong.<br \/><b>The real issue is not general rusting but stress-corrosion cracking.<\/b> Independent measurement: the 350 grade <b>failed in salt water at only 55% of its yield strength, in under two days<\/b>. Another finding of the same study is more disturbing still: <b>air at 98% relative humidity proved more aggressive than salt-water immersion<\/b>. You do not need to be at the coast \u2014 <b>a humid warehouse is enough<\/b>.<br \/><b>Practical plan:<\/b> (1) <b>Do not leave the part under sustained tensile stress<\/b>; account for assembly preloads and residual stresses. (2) <b>Plate it<\/b> \u2014 but <b>electroplating carries a hydrogen-embrittlement risk<\/b>; make the post-plating bake-out mandatory, or prefer routes that do not charge hydrogen, such as mechanical plating, paint or dry-film lubricant. (3) <b>Write a handling and storage specification<\/b>: humidity control, oil film, VCI packaging. (4) <b>Define an inspection interval.<\/b> (5) If the environment really is humid or salt-laden, <b>consider changing material<\/b> \u2014 <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/aermet-100\/\">AerMet 100<\/a> is markedly better in that duty.<\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">How should we compare Maraging 350 with AerMet 100 and 300M?<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>These three sit on the same shelf but do not do the same job. The dividing line is not strength \u2014 it is toughness and stress-corrosion behaviour.<\/b><br \/><b>Maraging 350<\/b> is by a clear margin <b>the strongest<\/b>: yield ~2275\u20132365 MPa, tensile ~2350\u20132430 MPa, 55\u201360 HRC. In return: <b>K<sub>Q<\/sub> ~39 MPa\u221am, Charpy ~12 J<\/b>, and cracking in salt water at <b>55%<\/b> of yield. Its advantages: <b>quench-free hardening, freedom from distortion, welding without preheat, simple heat treatment, easy machining in the annealed condition.<\/b><br \/><b>AerMet 100<\/b> (0.23C \u2013 13.4Co \u2013 11.1Ni \u2013 3.1Cr \u2013 1.2Mo) is a <b>carbon-bearing<\/b> secondary-hardening steel: yield <b>1724 MPa<\/b>, tensile <b>1965 MPa<\/b>, elongation <b>14%<\/b>, reduction of area <b>65%<\/b>, <b>K<sub>Ic<\/sub> 126 MPa\u221am<\/b>, <b>K<sub>ISCC<\/sub> 88 MPa\u221am<\/b>. It delivers about <b>75% of the 350&#8217;s yield<\/b> with <b>more than three times the fracture toughness<\/b>. The price: quench plus deep freeze (\u221273 \u00b0C) plus 5 hours at 482 \u00b0C, so it <b>distorts<\/b>; and its carbide content makes it <b>harder to machine<\/b>. Where damage tolerance and a salt environment are involved, <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/aermet-100\/\">AerMet 100<\/a> is clearly the right answer.<br \/><b>300M<\/b> (0.40C \u2013 1.6Si \u2013 0.8Cr \u2013 1.8Ni \u2013 0.4Mo \u2013 0.07V) is the classic quenched-and-tempered landing-gear steel: the AMS 6417 minima are <b>1862 MPa tensile \/ 1517 MPa yield, 8% elongation, 30% reduction of area, \u226552 HRC<\/b>. Well below the 350 on strength; being oil quenched it is <b>the most distortion-prone<\/b> and <b>the most hydrogen-sensitive<\/b> option. In return it is <b>far cheaper<\/b>. <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/300m\/\">300M<\/a> is a cost-performance choice.<br \/><b>Decision rule in one sentence:<\/b> for the absolute tensile ceiling and distortion-free manufacture, <b>Maraging 350<\/b>; for damage tolerance in a salt environment, <b>AerMet 100<\/b>; where budget dominates and the part is a solid forging, <b>300M<\/b>; for a balanced structural material, <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/maraging-250\/\">Maraging 250<\/a>.<\/p>\n<h4 id=\"dm-b12\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Common Datasheet Errors and Traps<\/h4>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>1. UNS number confusion \u2014 the biggest single trap on this alloy.<\/b> Three numbers circulate: <b>K93160<\/b>, <b>K93540<\/b> and <b>K93120<\/b>. <b>K93120 belongs to Maraging 300 and using it for the 350 is simply wrong<\/b> \u2014 yet some aerospace supplier pages are headed &#8220;Maraging 350 AMS 6515 UNS K93120&#8221;. Sources also diverge between K93160 and K93540. <b>On orders and certificates, rely on AMS 6515 plus the chemistry, not on the UNS number.<\/b><br \/><b>2. Yield strength given as ~2400 MPa \u2014 WRONG, that is the tensile strength.<\/b> The published values are <b>yield 2275\u20132365 MPa<\/b> and <b>tensile 2350\u20132430 MPa<\/b>. The name &#8220;350&#8221; refers to the <b>350 ksi = 2413 MPa tensile class<\/b>. Even a widely used encyclopaedia source lists &#8220;yield ~2413 MPa&#8221; for the 350; that figure is the nominal tensile, not a measured yield.<br \/><b>3. AMS 6515 presented as a sheet\/plate specification \u2014 WRONG.<\/b> Its title is <b>&#8220;Bars, Forgings, Tubing, and Rings&#8221;<\/b>. <b>There is no verified AMS sheet or plate number for the 350<\/b> (AMS 6520 exists for the 250, AMS 6521 for the 300). For plate, the only verified route is <b>MIL-S-46850<\/b>.<br \/><b>4. A 350 grade attributed to ASTM A538 \u2014 WRONG.<\/b> A538 contains only <b>Grade A (200), Grade B (250) and Grade C (300)<\/b>; <b>there is no 350 grade<\/b>. And A538 is in any case an old, no longer active document.<br \/><b>5. ASTM A579 presented as current \u2014 WRONG.<\/b> A579\/A579M was <b>withdrawn in May 2024 with no replacement<\/b>. In addition, which grade number in the 71\u201375 range corresponds to the 350 could not be independently confirmed.<br \/><b>6. A W.Nr. or EN name is invented.<\/b> The 250 has <b>1.6359 \/ X2NiCoMo18-8-5<\/b>; <b>no confirmed European equivalent was found for the 350<\/b>. Do not put a number you cannot verify on a certificate.<br \/><b>7. Sold as &#8220;Maraging 350 stainless steel&#8221; \u2014 metallurgically WRONG.<\/b> Chromium is at residual level and there is no passive film. Some suppliers carry &#8220;maraging-350-stainless-steel&#8221; even in their product-page addresses.<br \/><b>8. &#8220;Maraging steels resist stress corrosion and hydrogen embrittlement&#8221; repeated for the 350.<\/b> The measured reality: <b>the 350 fails in salt water at only 55% of yield in under two days<\/b> and is the most susceptible member of the family. Using that sentence without qualification on a 350 page is <b>not defensible engineering<\/b>.<br \/><b>9. A single elongation figure published.<\/b> Published values scatter across <b>2.8% \u00b7 4.0% \u00b7 6.2% \u00b7 8.0%<\/b> (differences of gauge length, orientation, section and cycle). <b>Quoting one number without stating the condition is misleading.<\/b><br \/><b>10. &#8220;350 is aged longer than 250&#8221; \u2014 WRONG.<\/b> The mill cycles are <b>482\u2013496 \u00b0C for 6 hours<\/b> or <b>510 \u00b0C for 3 hours<\/b>; the second is <b>hotter and shorter<\/b>. In the same defence programme the 250 was aged at <b>900 \u00b0F\/3 h<\/b> and the 350 at <b>950 \u00b0F\/3 h<\/b>.<br \/><b>11. The 250 grade&#8217;s physical properties copied across to the 350.<\/b> <b>Density, modulus and expansion coefficient differ<\/b> (8.08 vs 8.0 g\/cm\u00b3 \u00b7 200 vs 186 GPa \u00b7 11.3 vs 10.1 \u00d7 10\u207b\u2076\/\u00b0C). Moreover <b>conductivity, specific heat, resistivity and melting range could not be verified for the 350<\/b> \u2014 do not fill those rows with the 250 values.<br \/><b>12. The MIL-S-46850 toughness minimum applied wrongly.<\/b> One revision of the specification requires a minimum fracture toughness of <b>50 ksi\u221ain for the 300 class<\/b>. <b>The measured 350 value (35.2 ksi\u221ain) is below that<\/b> \u2014 one grade&#8217;s minimum cannot be applied to another. Read the minimum that applies to the 350 <b>from your own specification revision<\/b>.<br \/><b>13. Export control skipped.<\/b> The gas-centrifuge control text explicitly names <b>&#8220;maraging steel capable of an ultimate tensile strength of 1.95 GPa or more&#8221;<\/b>. <b>The aged tensile strength of Maraging 350 (~2.35\u20132.43 GPa) is well above that threshold<\/b> \u2014 it is the grade in this family that is most unambiguously caught by export control. Thresholds vary between regimes, and some lists apply lower thresholds to sheet, plate and tube forms (the exact figure could not be independently verified in this research). <b>Always have end-use statements, export licences and destination-country documentation checked for international shipments.<\/b><\/p>\n<p><!-- \/dm-zengin --><\/p>\n<p><!-- dm-ld --><script type=\"application\/ld+json\">{\"@context\":\"https:\/\/schema.org\",\"@type\":\"WebPage\",\"name\":\"Maraging 350\",\"url\":\"https:\/\/www.defencemetal.com\/index.php\/en\/maraging-350\/\",\"inLanguage\":\"en\",\"description\":\"Maraging 350 (18Ni-350 \/ C350 \/ Vascomax C350 \/ ATI C-350) is the highest-strength and lowest-toughness step of the 18Ni maraging family. The 350 in the name denotes the nominal 350 ksi (2413 MPa) tensile class in the aged condition; the measured 0.2% yield strength lies in the 2275\u20132365 MPa band.\",\"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 350\",\"description\":\"Maraging 350 (18Ni-350 \/ C350 \/ Vascomax C350 \/ ATI C-350) is the highest-strength and lowest-toughness step of the 18Ni maraging family. The 350 in the name denotes the nominal 350 ksi (2413 MPa) tensile class in the aged condition; the measured 0.2% yield strength lies in the 2275\u20132365 MPa band.\",\"inDefinedTermSet\":{\"@type\":\"DefinedTermSet\",\"name\":\"Defence Metal - metals and alloys\",\"url\":\"https:\/\/www.defencemetal.com\/\"},\"alternateName\":[\"W.Nr. 1.6359\"],\"identifier\":[{\"@type\":\"PropertyValue\",\"propertyID\":\"Werkstoffnummer\",\"value\":\"1.6359\"}]}}<\/script><!-- \/dm-ld --><\/p>\n","protected":false},"excerpt":{"rendered":"<p>Maraging 350 \/ AMS 6515 DEFENCE METAL Maraging 350 UNS K93160 \u00b7 18Ni(350) \/ C350 \u00b7 18.0-19.0% Ni \u2013 11.5-12.5% Co \u2013 4.6-5.2% Mo \u2013 1.30-1.60% Ti \u2013 0.05-0.15% Al \u2013 C \u2264 0.03% Not to be confused with Maraging 300 For what The highest-strength grade of the maraging family. Cobalt is raised to 12% &hellip; <\/p>\n<p class=\"link-more\"><a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/maraging-350\/\" class=\"more-link\"><span class=\"screen-reader-text\"> &#8220;Maraging 350 \/ AMS 6515&#8221;<\/span>devam\u0131n\u0131 oku<\/a><\/p>\n","protected":false},"author":1,"featured_media":0,"parent":3526,"menu_order":0,"comment_status":"closed","ping_status":"closed","template":"","meta":{"_yoast_wpseo_title":"MARAGING 350 \/ AMS 6515 | Defence Metal","_yoast_wpseo_metadesc":"Maraging 350 (AMS 6515) \u2014 the highest strength maraging grade, aged at 480-510 \u00b0C with minimal distortion. Bar, plate and forgings.","inspiro_hide_title":false,"inspiro_hide_featured_image":false,"footnotes":""},"dm_sektor":[10,9,15],"class_list":["post-3541","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 350 \/ AMS 6515 | Defence Metal<\/title>\n<meta name=\"description\" content=\"Maraging 350 (AMS 6515) \u2014 the highest strength maraging grade, aged at 480-510 \u00b0C with minimal distortion. 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