Steel Jethete M152

Technical Reference Library

Jethete M152

Wnr. 1.4938 DIN/EN X12CrNiMoV12-3 UNS S64152

Material Overview

Jethete M152 is a nitrogen-bearing, 12% chromium martensitic stainless steel developed by Firth Vickers for jet-engine service and still widely specified today under AMS 5719 and UNS S64152. Unlike simple 410/420-type martensitic stainless, M152 carries meaningful nickel (2-3%) and molybdenum (1.5-2%) alongside vanadium and a controlled nitrogen addition, which together push its creep-rupture strength and temper resistance well above what a plain 12Cr grade can hold at elevated temperature. It is supplied and used in the hardened-and-tempered condition, retaining good toughness and dimensional stability in continuous service up to roughly 1040°F (560°C).

That combination of hot strength, creep resistance, and corrosion resistance is why M152 became a standard material for compressor discs and blades, turbine hardware, shafts, high-temperature bolting, and rings in gas turbine and jet-engine assemblies. In the DIN/EN system it corresponds to X12CrNiMoV12-3, Wnr. 1.4938 — note that the closely related X12CrNiMoV12-2 carries the similar-looking number 1.4939, and the two are sometimes confused in supplier literature.

International Designation Equivalents

Standard Designation
Wnr. 1.4938
DIN/EN X12CrNiMoV12-3
UNS S64152
AMS 5719
BS S151 / S159 (Jethete M152)

Chemical Composition

Element Amount
Chromium (Cr) 11.0-12.5%
Nickel (Ni) 2.00-3.00%
Molybdenum (Mo) 1.50-2.00%
Vanadium (V) 0.25-0.40%
Manganese (Mn) 0.50-0.90%
Nitrogen (N) 0.02-0.04%
Carbon (C) 0.08-0.13%
Silicon (Si) 0.35% max

Machinability Explained

M152 is normally machined in the hardened-and-tempered condition rather than annealed, which puts it firmly in the same challenging category as other PH/creep-resisting martensitic aerospace stainless grades: high cutting forces, accelerated flank wear from the alloyed carbide- and nitride-forming elements (Mo, V), and low thermal conductivity that concentrates heat right at the cutting edge. It does not work-harden as aggressively as an austenitic grade, but a dull edge or excessive dwell will still glaze the surface and shorten tool life on the next pass.

Rigid tooling and workholding matter more here than on lower-strength stainless — deflection under cutting load is a bigger threat to accuracy than on a soft annealed part. Sharp, positive-rake inserts with adequate feed to stay below any work-hardened layer, combined with steady coolant flow, are the standard approach. Because tempered hardness varies with the temper temperature selected by the heat treater, always confirm actual hardness before committing to aggressive speeds.

Recommended Cutting Speeds

Application Vc (m/min) Vc (SFM)
Turning 95-130 310-425
Milling 60-85 195-280
Parting 35-50 115-165
Grooving 55-75 180-245
Drilling 25-35 80-115

Recommended FM Carbide Grades

Turning

Grade Coating ISO Application Range
FM324 PVD M10-M20
FM2553 CVD M30

Parting / Grooving

Grade Coating ISO Application Range
FM2543 CVD P20
FM2553 CVD M30

Milling

Grade Coating ISO Application Range
FM125 PVD M15-M35

Recommended Insert Cutting Edge Geometry

Parameter Value
Honing Size 0.03-0.05 mm / 0.001-0.002"
Rake Angle 9°-11°
Land Angle Positive
Land Width 0.20-0.30 mm / 0.008-0.012"