Inconel 625 ASTM B446 Specification

This specification covers nickel-chromiummolybdenum-columbium (UNS N06625), nickel-chromiummolybdenum-silicon alloy (UNS N06219), and NickelChromium-Molybdenum-Tungsten Alloy (UNS N06650)* in the form of hot-worked rod and bar and cold-worked rod in the conditions. UNS N06625 products are furnished in two grades of different heat-treated conditions: Grade 1 (Annealed)—Material is normally employed in service temperatures up to 1100°F (593°C). Grade 2 (Solution Annealed)—Material is normally employed in service temperatures above 1100°F (593°C) when resistance to creep and rupture is required.

Inconel 625 Chemical Composition

Element Composition Limits, %
N06625
Carbon 0.10 max
Manganese 0.50 max
Silicon 0.50 max
Phosphorus 0.015 max
Sulfur 0.015 max
Chromium 20.0 min - 23.0 max
Columbium + tantalum 3.15 min - 4.15 max
Cobalt (if determined) 1.0 max
Molybdenum 8.0 min
Iron 5.0 max
Aluminum 0.40 max
Titanium 0.40 max
NickelA 58.0 min
Note:

A. Element shall be determined arithmetically by difference

Mechanical Properties for Hot-Worked Rod and Bar and ColdWorked Rod A

Diameter or Distance Between Parallel Surfaces, in. (mm) Tensile Strength min, ksi (MPa) Yield Strength (0.2 % offset), min, ksi (MPa) Elongation in 2 in. or 50 mm or 4D, min, %
UNS N06625 Grade 1 (Annealed)B
Up to 4 (102), incl 120 60 30
Over 4 (102) to 10 (254), incl 110 50 25
UNS N06625 Grade 2 (Solution Annealed)C
All sizes 100 40 30
Note:

A. Forging quality is furnished to chemical requirements and surface inspection only. No tensile properties are required. Forging stock is typically supplied in the hot worked condition, (see X1.1.5).
B. Annealed 1600°F (871°C) minimum.
C. Solution annealed at 2000°F (1093°C) minimum, with or without subsequent stabilization anneal at 1800°F (982°C) minimum to increase resistance to sensitization.