High-Speed Steel Grades: M2, M35, M42 Composition and Cutting Performance
High-speed steels (HSS) are a family of highly alloyed tool steels whose defining characteristic is the ability to retain cutting hardness at the elevated temperatures generated during machining — a property termed red hardness or hot hardness. The three grades examined in depth here — M2, M35, and M42 — span the range from the universal general-purpose standard to cobalt-enhanced grades for difficult-to-machine materials, and together account for the overwhelming majority of HSS cutting tools in global production. Understanding their alloy chemistry, carbide microstructure, heat treatment responses, and performance envelopes is essential for any manufacturing metallurgist or tooling engineer specifying or applying these materials.
- HSS derives its red hardness from thermally stable alloy carbides (MC, M6C, M23C6) and a secondary hardening martensite matrix; plain carbon tool steels lose hardness above 200°C whereas HSS sustains cutting performance to over 550°C.
- M2 (6W-5Mo-4Cr-2V) is the de facto general-purpose HSS; M35 adds 5 wt% Co for improved hot hardness; M42 adds 8 wt% Co plus higher Mo and C for the most demanding applications, achieving up to 70 HRC.
- Austenitising temperatures for HSS (1190–1230°C for M2) are far higher than for conventional alloy steels and must dissolve MC and M6C carbides to enrich the matrix for secondary hardening during tempering.
- Triple tempering at 540–560°C is mandatory for all HSS grades: the first temper transforms retained austenite; the second tempers fresh martensite; the third completes conversion and stress-relieves the microstructure.
- Cobalt raises the Ac1 temperature, allowing higher austenitising temperatures and greater carbide dissolution without excessive grain growth, directly improving hot hardness.
- Powder metallurgy (PM) HSS of the same nominal grade as conventionally produced material offers superior grindability, higher transverse rupture strength, and more uniform carbide distribution by eliminating macrosegregation.
The Metallurgical Basis of High-Speed Steel Performance
High-speed steels are a subset of tool steels characterised by very high alloy content — primarily tungsten (W), molybdenum (Mo), chromium (Cr), vanadium (V), and, in cobalt grades, cobalt (Co) — combined with elevated carbon (0.80–1.10 wt%) to provide the carbon needed for carbide formation. The AISI designation system divides HSS into two families: the M-series (molybdenum base) and the T-series (tungsten base). M-series grades, particularly M2, have largely displaced T-series in modern practice due to lower raw material cost and equivalent or superior performance.
Carbide Types in High-Speed Steels
The microstructure of hardened and tempered HSS consists of a tempered martensite matrix containing four distinct carbide types, each with different crystal structure, composition, hardness, and role:
| Carbide Type | Crystal Structure | Principal Elements | Hardness (HV) | Role in HSS |
|---|---|---|---|---|
| MC | FCC (NaCl type) | V, (Mo, W, Cr) | 2400–3000 | Abrasion resistance; primary and secondary precipitation; partially dissolves on austenitising |
| M6C | FCC (complex) | W, Mo, Fe, Cr | 1600–2000 | Main carbide in W- and Mo-type HSS; provides red hardness; dissolves substantially at austenitising temperature |
| M23C6 | FCC (complex) | Cr, Fe, (Mo, W) | 1200–1600 | Forms on tempering below 600°C; provides some hardness but dissolves easily; present in tempered condition |
| M7C3 | Orthorhombic | Cr, Fe | 1200–1800 | Present in Cr-rich HSS; less significant than M6C and MC in M-series grades |
The distribution and volume fraction of these carbides depend critically on the austenitising temperature and time, which control how much carbide is dissolved into the matrix versus retained as undissolved primary particles. Undissolved primary carbides (primarily MC and some M6C) provide wear resistance but do not contribute to secondary hardening or hot hardness. The dissolved carbide-formers (W, Mo, V, Cr, C) re-precipitate as fine secondary carbides during tempering, providing the secondary hardening peak that is the signature property of HSS. The martensite formation behaviour in HSS is complex due to the high alloy content stabilising austenite and generating substantial retained austenite fractions after quenching — a key reason triple tempering is necessary.
The Secondary Hardening Mechanism
Secondary hardening in HSS is the increase in hardness that occurs during tempering at 500–600°C after an initial decrease. It is caused by the precipitation of fine, coherent MC and M2C carbides (nanometre-scale) within the martensite laths, driven by the high supersaturation of W, Mo, and V in the as-quenched martensite. These precipitates create a dense dispersion of obstacles to dislocation motion that raises yield strength and hardness significantly above the as-quenched matrix hardness contribution from martensite alone.
Secondary hardening peak location (approximate): T_peak ≈ 540–560°C for M2, M35 T_peak ≈ 550–570°C for M42 (Co shifts peak higher) Secondary hardening increment: ΔHRC ≈ +4 to +8 HRC above the softening trough at 300-400°C Retained austenite (as-quenched, typical): M2: 15–25 vol% (austenitised 1210°C) M35: 18–28 vol% (austenitised 1220°C) M42: 20–30 vol% (austenitised 1180–1210°C) After triple temper at 560°C (3 x 1 hr): Retained austenite: <3 vol% (stable for tool service)
Cobalt (Co) in M35 and M42 does not itself form carbides in HSS. Its role is to raise the Ac1 temperature (allowing higher austenitising temperatures without excessive grain growth), to increase the solubility of W and Mo in austenite at the austenitising temperature, and to slow the recovery of the dislocation substructure during service at elevated temperature. The net effect is a higher secondary hardening peak temperature and a greater retained hardness at 500–600°C, directly translating to improved tool life in high-speed cutting of difficult materials. Understanding the grain boundary phenomena underlying carbide precipitation and segregation is assisted by the Grain Boundaries Guide.
Chemical Composition of M2, M35, and M42
| Element (wt%) | M2 (AISI) | M35 (AISI) | M42 (AISI) | T1 (for comparison) |
|---|---|---|---|---|
| Carbon (C) | 0.78–0.88 | 0.80–0.90 | 1.05–1.15 | 0.65–0.80 |
| Tungsten (W) | 5.50–6.75 | 5.50–6.75 | 1.15–1.85 | 17.25–18.75 |
| Molybdenum (Mo) | 4.50–5.50 | 4.50–5.50 | 9.00–10.00 | — |
| Chromium (Cr) | 3.75–4.50 | 3.75–4.50 | 3.50–4.25 | 3.75–4.50 |
| Vanadium (V) | 1.75–2.20 | 1.75–2.20 | 0.95–1.35 | 0.90–1.30 |
| Cobalt (Co) | — | 4.50–5.50 | 7.75–8.75 | — |
| Manganese (Mn, max) | 0.45 | 0.45 | 0.45 | 0.40 |
| Silicon (Si, max) | 0.45 | 0.45 | 0.65 | 0.40 |
| Sulphur (S, max) | 0.030 | 0.030 | 0.030 | 0.030 |
Source: ASTM A600 (Standard Specification for Tool Steel High Speed), current edition. The M2 and M35 grades differ only in cobalt content; the base W-Mo-Cr-V balance is identical. M42 is a distinct grade with significantly higher Mo and C and reduced W and V.
The Tungsten-Molybdenum Equivalence Principle
In HSS metallurgy, tungsten and molybdenum are largely interchangeable in their effects on hardenability, secondary hardening, and hot hardness, following an empirical equivalence of approximately 2 parts W = 1 part Mo by weight. This relationship arises from the similar atomic radii and carbide-forming tendencies of the two elements, and from the fact that both form M6C carbides with similar thermodynamic stability. The M2 grade exemplifies this: its 6W-5Mo composition is approximately equivalent to a 6+10 = 16 “W-equivalent” content, closely matching the T1 grade (18W).
Tungsten-Equivalent (Weq) approximation: Weq = W% + 2 × Mo% M2: Weq = 6 + 2×5 = 16 (vs T1 at 18W) M35: Weq = 6 + 2×5 = 16 (same base, +5Co) M42: Weq = 1.5 + 2×9.5 = 20.5 (highest Weq of the three) Note: M42 achieves its highest hot hardness via high Weq + 8Co despite lower nominal W content than M2.
The higher Mo content in M42 (9.0–10.0 wt%) versus M2 (4.5–5.5 wt%) is the primary driver of M42’s superior hot hardness. Mo is approximately twice as effective as W per unit weight in solid-solution strengthening of the martensite matrix, which directly contributes to elevated-temperature hardness retention beyond what cobalt alone would provide.
Heat Treatment of High-Speed Steels
Preheating
Due to the low thermal conductivity of HSS (approximately 20–25 W/m·K, compared to 50 W/m·K for carbon steel) and the extreme austenitising temperatures required, direct charging into a hot furnace creates massive thermal gradients that cause cracking in all but the simplest geometries. A two-stage preheat is mandatory:
First preheat: 450–500°C, hold 20–30 min per 25 mm of section. This removes residual stresses from machining or prior operations and allows uniform heating to begin.
Second preheat: 850–870°C (slightly above Ac1), hold 20–30 min. At this temperature carbide dissolution begins slowly and the piece reaches thermal uniformity before the final rapid transfer to the hardening furnace.
Austenitising (Hardening Temperature)
| Grade | Hardening Temp. (°C) | Soak Time at Temp. | As-Quenched Hardness (HRC) | Retained Austenite (vol%) |
|---|---|---|---|---|
| M2 | 1190–1230 | 2–5 min (salt bath); 3–8 min (atmosphere) | 63–66 | 15–25 |
| M35 | 1200–1240 | 2–5 min (salt bath) | 64–67 | 18–28 |
| M42 | 1180–1210 | 2–5 min (salt bath) | 66–68 | 20–30 |
Quenching
HSS tools are quenched by one of three methods, in order of decreasing cooling rate:
Salt bath quench (martempering): The most common method for complex-geometry tools. The workpiece is transferred to a salt bath at 500–600°C (above Ms), held for temperature equalisation (typically 3–8 min), then air cooled to room temperature. This interrupted quench minimises distortion and thermal shock while achieving sufficient cooling rate to suppress pearlite and bainite formation. Given the deep hardenability of HSS, the cooling rate in a salt bath at 550°C is adequate for sections up to 75–100 mm.
Oil quench: Used for simpler geometries and smaller sections. Faster cooling rate than salt bath; higher distortion and cracking risk for complex tools.
Air quench: Used for very large sections or intricate thin-wall tools where oil and salt bath risks are unacceptable. Adequate due to very high hardenability of HSS.
Triple Tempering
Every HSS grade must receive a minimum of three separate tempering cycles. This is not optional — single or double tempering leaves unacceptable levels of retained austenite and untempered fresh martensite that will cause dimensional instability and brittle failure. Each temper is typically 1 hour at temperature plus adequate heating time.
| Grade | Tempering Temp. (°C) | Final HRC (3 tempers) | Purpose of Each Temper |
|---|---|---|---|
| M2 | 540–560 (all 3 cycles) | 62–65 | 1st: transform RA, begin secondary hardening. 2nd: temper fresh martensite from RA conversion. 3rd: complete conversion, stress relieve, stabilise. |
| M35 | 545–565 (all 3 cycles) | 63–66 | |
| M42 | 550–570 (all 3 cycles) | 67–70 |
The cryogenic treatment of HSS tools (cooling to −70 to −196°C after quench, before tempering) is practiced by some manufacturers to more completely convert retained austenite and improve dimensional stability. For tools with stringent dimensional tolerances, cryogenic treatment between the quench and first temper can reduce retained austenite to <1 vol%, significantly improving repeat grinding accuracy over tool life.
Mechanical Properties and Performance Data
| Property | M2 | M35 | M42 |
|---|---|---|---|
| Hardness after triple temper (HRC) | 62–65 | 63–66 | 67–70 |
| Hot hardness at 540°C (HRC equiv.) | 50–54 | 53–57 | 57–61 |
| Transverse rupture strength (MPa) | 3100–3700 | 3000–3500 | 2600–3100 |
| Compressive yield strength (MPa) | 2000–2400 | 2100–2500 | 2400–2800 |
| Density (g/cm³) | 8.16 | 8.18 | 8.00 |
| Toughness (Charpy unnotched, J) | 18–27 | 16–24 | 10–16 |
| Grindability index (relative) | Good (1.0 reference) | Moderate (0.85) | Moderate (0.80) |
| Relative wear resistance | 1.0 (reference) | 1.1 | 1.2 |
| Red hardness limit (°C for >55 HRC) | ~520 | ~540 | ~570 |
| Austenitising temp. range (°C) | 1190–1230 | 1200–1240 | 1180–1210 |
The inverse relationship between hardness and toughness is clearly visible: M42, with the highest hardness, has the lowest transverse rupture strength and Charpy toughness. This is why M42 is unsuitable for heavily interrupted cuts (milling hard materials, broaching) in the conventionally produced form — powder metallurgy M42 partially recovers toughness through finer carbide distribution and eliminates the large primary carbide clusters that act as fracture initiation sites in wrought M42.
The hardness testing methods article details the Vickers, Rockwell, and microhardness scales used for quality verification of HSS tools, including the conversion tables applicable when comparing HRC values from hot hardness testing to room-temperature HRC values. Impact testing methodology for tool steels is covered in the Charpy impact test article.
Grade-by-Grade Technical Profile
M2: The Universal High-Speed Steel
M2 is the most widely produced and specified HSS grade globally, accounting for approximately 80% of all HSS tool production by volume. Its balanced 6W-5Mo-4Cr-2V chemistry delivers a combination of hot hardness, wear resistance, grindability, and toughness that no single alternative grade matches across the full range of cutting applications. M2 is the reference against which all other HSS grades are judged.
The 2 wt% vanadium content in M2 provides abrasion resistance through MC carbide particles while remaining grindable with conventional aluminium oxide (Al2O3) grinding wheels. Higher vanadium grades (M3 type 2 at 3 wt% V; T15 at 5 wt% V) offer superior wear resistance but mandate CBN or SiC grinding wheels and command substantially higher grinding costs in tool manufacture and resharpening.
M2 Typical Applications
Twist drills, jobber drills, step drills, taps (all sizes), reamers (hand and machine), end mills, slot drills, form tools, milling cutters (plain and side-and-face), gear hobs, broaches, saw blades, and threading dies. M2 is the standard specification for drills and taps per ISO 521, ISO 529, and DIN 338/340.
M35: Cobalt-Enhanced General Purpose Grade
M35 is produced by adding 4.5–5.5 wt% cobalt to the M2 base composition. The metallurgical effects are: (1) the Ac1 temperature rises by approximately 30°C, permitting slightly higher austenitising temperatures and greater carbide dissolution without grain growth penalty; (2) the martensite Ms temperature is marginally lowered, slightly increasing retained austenite in the as-quenched condition; (3) the secondary hardening peak temperature rises by approximately 10°C; and (4) the hot hardness at 540°C improves by approximately 2–3 HRC equivalent over M2 of the same base heat treatment.
M35 is marketed under various proprietary names: Cobalt HSS, HSCo, HSS-Co5, Cobalt 5, and Gold Point in different markets. The gold or yellow titanium nitride (TiN) PVD coating commonly applied to cobalt HSS tools serves both as a performance coating (reducing friction and improving chip flow) and as a visual identifier — though the coating composition varies by supplier and should not be relied upon to identify the base steel grade.
M35 Typical Applications
Drills and taps for stainless steels, heat-resistant alloys, titanium, copper alloys, and hardened steels up to 42 HRC. End mills for stainless and hard steels. Reamers for difficult-to-machine materials. M35 is specified when M2 tools show accelerated flank wear or edge breakdown under the conditions described — it is not a universal upgrade, as the marginal cost premium is not justified for standard carbon steel machining.
M42: High-Cobalt Super High-Speed Steel
M42 is a fundamentally different alloy design from M2/M35: higher C (1.05–1.15 wt%), dramatically higher Mo (9–10 wt%), reduced W (1.15–1.85 wt%), reduced V (0.95–1.35 wt%), and 8 wt% Co. This chemistry maximises the tungsten-equivalent and cobalt content to achieve the highest secondary hardening and hot hardness of any standard HSS grade, at the cost of reduced toughness and grindability.
The high Mo content of M42 creates a predominantly M6C carbide microstructure based on (Fe,Mo)6C and (Fe,W,Mo)6C rather than the (Fe,W)6C typical of W-heavy grades. These Mo-rich M6C carbides dissolve slightly more easily than W-rich M6C at the austenitising temperature, providing better matrix enrichment per unit temperature — which is why M42 can be austenitised at the lower end of the HSS range (1180–1210°C) while still achieving exceptional hot hardness.
M42 Typical Applications
End mills, drills, and taps for nickel-based superalloys (Inconel 718, Waspaloy, Hastelloy), titanium alloys (Ti-6Al-4V), hardened steels (35–55 HRC), cobalt alloys, and hard cast irons. Saw blades for aerospace structural materials. Form tools for interrupted cuts in hard steels where controlled chip load and sharp edge retention are critical. PM-M42 is strongly preferred over wrought M42 for these applications.
Powder Metallurgy HSS
Conventional wrought HSS is produced by arc or induction melting followed by ingot casting, homogenisation, and multi-step hot working. During ingot solidification, carbides segregate to interdendritic regions, forming large, unevenly distributed primary carbide particles and bands visible in the final wrought product. These carbide bands reduce transverse properties, create preferential fracture paths, and cause non-uniform hardness after heat treatment.
PM-HSS eliminates these problems: the liquid metal is gas-atomised into spherical powder particles (typically 50–150 μm), each solidifying as a microsegregation-free rapidly-solidified droplet. The powder is consolidated by hot isostatic pressing (HIP) at 1100–1150°C into fully dense billets with carbide particle sizes of 1–3 μm uniformly distributed throughout the matrix, compared to 5–30 μm carbide clusters in wrought material.
The practical benefits of PM-HSS include: transverse rupture strength 20–40% higher than wrought equivalents; grinding ratio (material removed per unit wheel wear) 30–60% improved for vanadium-rich grades; ability to incorporate alloying additions beyond the segregation limits of conventional casting (e.g., T15 at 5 wt% V, ASP2052 at 8 wt% V). PM grades are designated by prefix in some systems (CPM-M4, CPM-Rex, ASP series) and carry a 3–5× price premium over wrought HSS that is justified in high-value tooling applications.
Cutting Tool Coatings on HSS
Physical vapour deposition (PVD) coatings are routinely applied to HSS tools to extend tool life, reduce cutting forces, and improve chip control. Coatings must be applied below the HSS tempering temperature to avoid softening the substrate:
| Coating | Deposition Temp. (°C) | Hardness (HV) | Max. Service Temp. (°C) | Best Application |
|---|---|---|---|---|
| TiN (Titanium Nitride) | 200–500 | 2300–2500 | 600 | General purpose; drilling, tapping carbon steel |
| TiCN (Titanium Carbo-Nitride) | 200–500 | 3000–3500 | 400 | Abrasive materials; higher hardness than TiN |
| TiAlN (Titanium Aluminium Nitride) | 200–500 | 3200–3500 | 800–900 | Hard steels, stainless steels, dry cutting |
| CrN (Chromium Nitride) | 200–450 | 1800–2200 | 700 | Non-ferrous metals, aluminium, plastics |
| AlCrN (Aluminium Chromium Nitride) | 200–500 | 3200–3800 | 1100 | Nickel alloys, titanium, hard milling |
Coating adhesion to HSS depends critically on surface preparation (grinding, polishing, degreasing) and the substrate hardness — fully hardened M42 at 69 HRC provides better coating support than under-hardened M2 at 58 HRC. The coating layer (2–5 μm typical) does not change the base metal properties but significantly reduces the coefficient of friction at the tool-chip interface, reducing cutting temperatures and extending the regime within which HSS outperforms uncoated carbide on grounds of edge toughness and cost.
International Equivalents and Standard Cross-Reference
| AISI Grade | EN ISO 4957 | DIN | JIS | BS | GOST |
|---|---|---|---|---|---|
| M2 | HS6-5-2 | S6-5-2 / 1.3343 | SKH51 | M2 | R6M5 |
| M35 | HS6-5-2-5 | S6-5-2-5 / 1.3243 | SKH55 | M35 | R6M5K5 |
| M42 | HS2-9-1-8 | S2-9-1-8 / 1.3247 | SKH59 | M42 | R2M9K8 |
| T1 | HS18-0-1 | S18-0-1 / 1.3355 | SKH2 | T1 | R18 |
| T15 | HS12-1-5-5 | S12-1-5-5 / 1.3202 | SKH57 | T15 | R12F5K5 |
The EN HS designation encodes W-Mo-V-Co content in sequence. HS6-5-2 = 6W-5Mo-2V; HS6-5-2-5 = 6W-5Mo-2V-5Co; HS2-9-1-8 = 2W-9Mo-1V-8Co. This naming system is immediately informative for composition identification, in contrast to the AISI M/T numbering system which conveys no compositional information directly. Correlation with the iron-carbon phase diagram fundamentals helps understand why the higher alloy content of HSS shifts the eutectoid to lower carbon and why the large primary carbide volume fraction in HSS (20–30 vol%) places the alloy composition well above the hypereutectoid region of the eutectoid reaction baseline. The pearlite colony growth and bainite microstructure articles provide context on the transformation products that must be suppressed during HSS quenching. The annealing and normalising article covers the softening treatments applied to HSS bar stock before machining into tool blanks.
Frequently Asked Questions
What is the austenitising temperature for M2 high-speed steel?
What hardness does M2 achieve after hardening and tempering?
What is red hardness in high-speed steels?
What is the difference between M2, M35, and M42 HSS?
Why must high-speed steel be triple tempered?
What is the role of vanadium in high-speed steels?
Can high-speed steel be welded?
What are the international equivalents of M2 and M42 HSS?
What is powder metallurgy HSS and how does it differ from conventional HSS?
How do I select between M2, M35, and M42 for a specific machining application?
Recommended References
ASM Handbook Vol. 16: Machining
Comprehensive reference covering tool material selection, cutting speeds, tool geometry, and failure analysis for HSS and carbide tooling across all machining operations.
View on AmazonTool Steel Simplified — Palmer & Luerssen
Classic industry reference covering the full range of tool steel families — HSS, cold work, hot work, and shock-resistant grades — with heat treatment data and application guidance.
View on AmazonFundamentals of Metal Cutting and Machine Tools — Boothroyd & Knight
Graduate-level text on cutting mechanics, tool materials, wear mechanisms, and the thermomechanics of the cutting zone that governs tool life in HSS and carbide tooling.
View on AmazonASM Handbook Vol. 4: Heat Treating
Definitive reference for HSS heat treatment procedures, including austenitising temperature selection, tempering cycles, retained austenite measurement, and distortion control for complex tool geometries.
View on AmazonDisclosure: MetallurgyZone participates in the Amazon Associates programme. If you purchase through these links, we may earn a small commission at no extra cost to you. This helps support free technical content on this site.
Further Reading
Quenching and Tempering
Full treatment of the Q&T cycle, secondary hardening mechanisms, and martensite tempering stages in alloy steels.
Martensite Formation
Mechanisms of martensitic transformation, Ms temperature effects, morphology types, and retained austenite.
Iron-Carbon Phase Diagram
Foundational guide to equilibrium phases and the thermodynamic basis for carbide stability in tool steels.
Hardness Testing Methods
Rockwell, Vickers, and microhardness scales with conversion tables applicable to HSS tool quality verification.
Grain Boundaries Guide
Grain boundary types, segregation behaviour, and the relationship between grain size and mechanical properties in alloy steels.
Bainite Microstructure
Upper and lower bainite formation and why bainite in the core of HSS tools (from insufficient quench) is detrimental.
Annealing and Normalising
Softening treatments applied to HSS bar stock before machining into tool blanks, including spheroidise annealing procedures.
Charpy Impact Testing
Impact testing methodology and significance for comparing toughness of HSS grades and PM versus wrought variants.