Material Haynes 600

Technical Reference Library

Haynes 600

Form Wrought Type Ni-Cr-Fe Solid-Solution UNS N06600

Material Overview

Haynes 600 is Haynes International's trade name for the well-known nickel-chromium-iron solid-solution alloy more commonly sold as Inconel 600. It carries no significant gamma-prime strengthening — its properties come from solid-solution hardening by chromium and iron in a high-nickel matrix (72% minimum nickel) — so this is a moderate-strength, extremely tough and ductile alloy rather than a high-strength turbine alloy.

The high nickel content gives excellent resistance to corrosion by many organic and inorganic compounds and to chloride-ion stress-corrosion cracking, while the 14-17% chromium content provides good resistance to oxidizing conditions and elevated-temperature scaling up to roughly 2000°F (1093°C). Typical applications include chemical and food processing equipment, heat-treating fixtures, furnace components, and other parts requiring both high-temperature strength and corrosion resistance across a very wide temperature range, including cryogenic service.

International Designation Equivalents

Standard Designation
UNS N06600
Werkstoff 2.4816
DIN NiCr15Fe
AMS 5540 (sheet/strip/plate)
Other Trade Names Inconel 600, Alloy 600

Chemical Composition

Element Content
Nickel (Ni) 72.0% min (Balance)
Chromium (Cr) 14.0 - 17.0%
Iron (Fe) 6.0 - 10.0%
Carbon (C) 0.15% max
Manganese (Mn) 1.0% max
Silicon (Si) 0.5% max
Copper (Cu) 0.5% max
Sulfur (S) 0.015% max

Values per AMS 5540/ASTM B168 specification ranges. The old page on file for this material listed a 72%+15.5%+8% Ni/Cr/Fe reading consistent with these ranges; that data has been retained and cross-checked rather than discarded.

Machinability Explained

As a solid-solution nickel-chromium-iron alloy with no gamma-prime hardening, Haynes 600 machines differently than the precipitation-hardened superalloys in this family — it's tough and gummy rather than abrasive. Low thermal conductivity is still the dominant issue: heat generated at the cutting edge has nowhere to go but into the tool, since the workpiece and chip carry it away poorly compared to steel. That concentrated heat accelerates crater wear and edge deformation if speeds are pushed too high.

Work hardening is a major concern with this alloy — because it has no precipitate structure to begin with, the austenitic matrix hardens significantly under mechanical deformation from the cutting action itself, so any rubbing, dwelling, or light interrupted engagement leaves a hardened skin that is far tougher to remove on the next pass. Chip control can also be a problem, since the alloy's ductility produces long, stringy chips that can gall against the tool and workpiece. Positive-rake, sharp coated carbide edges, constant chip loads, rigid setups, and generous coolant are the standard countermeasures.

Recommended Cutting Speeds

Operation Vc (m/min) Vc (SFM)
Turning 60 – 180 200 – 590
Milling 45 – 135 150 – 440
Parting 40 – 115 130 – 380
Grooving 55 – 160 180 – 520
Drilling 55 – 160 180 – 520

General starting-point ranges for heat-resistant Ni/Co-based alloys. Actual optimal speeds depend on tool grade, coating, rigidity, and coolant strategy.

Recommended FM Carbide Grades by Operation

Turning

Grade Coating ISO Application Range
FM524 CVD S05 - S10
FM2533 CVD S15

Parting / Grooving

Grade Operation Coating ISO Application Range
FM2543 Parting CVD S20
FM2553 Parting CVD S30
FM2533 Grooving CVD S10

Milling

Grade Coating ISO Application Range
FM125 PVD S15 - S35

Ready to cut Haynes 600? Shop FM Carbide inserts engineered for nickel-chromium-iron solid-solution alloys.

Shop Turning & Grooving Inserts Shop Milling Inserts

Recommended Insert Cutting-Edge Geometry

Parameter Value
Honing Size 0.02-0.05 mm / 0.001-0.002"
Rake Angle 13° - 18°
Land Angle Neutral
Land Width 0.10-0.20 mm / 0.004-0.008"
Ground Insert Recommended