Item # I625-078, Inconel® 625 Sheet On Continental Steel & Tube Co.

All Categories > Nickel and High Temperature Alloys > Inconel® > Inconel® 625 Sheet > Item # I625-078


	Item # I625-078, Inconel® 625 Sheet

larger image

Inconel 625 is a nickel-chromium-molybdenum alloy with an addition of niobium that acts with the molybdenum to stiffen the alloy's matrix and thereby provide high strength without a strengthening heat treatment. The Inconel 625 resists a wide range of severely corrosive environments and is especially resistant to pitting and crevice corrosion. Inconel 625 is used in chemical processing, aerospace and marine engineering, pollution-control equipment and nuclear reactors. Standard product forms are round, flats, forging stock, extruded section, pipe, tube, plate, sheet, strip and wire.

Unit of Measure: Imperial

Specifications · Nickel Alloy Compositions · Typical Mechanical Properties

Specifications

Material		Inconel®

Shapeform		Sheets

Thickness		0.078 inches

Nickel Alloy Compositions

Alloy		Inconel® 625

Basic Composition		1.0% Iron 16.3% Molybdenum 20.5% Chrominum 3.8% Tungsten 58.0% Nickel

Density		0.305 lbs/in³

ASTM Specification		ASME SB-443 ASTM B443 SAE 5599 SAE 5869 UNS N06626

Typical Mechanical Properties

Melting Temperature Range		2350 to 2460 ºF 1290 to 1350 ºC

Rupture Strength (1000 h at 1200°F/650°C)		52000 psi 360 MPa

Rupture Strength (1000 h at 1400°F/760°C)		23000 psi 160 MPa

Rupture Strength (1000 h at 1600°F/870°C)		7200 psi 50 MPa

Rupture Strength (1000 h at 1800°F/980°C)		2600 psi 18 MPa

DOWNLOADS


		Terminology Sheet

		Nickel Alloys Comparison Chart

		Inconel® Datasheet

		Inconel® Reference Guide

Item # I625-078, Inconel® 625 Sheet

Material

Shapeform

Thickness

Alloy

Basic Composition

Density

ASTM Specification

Melting Temperature Range

Rupture Strength (1000 h at 1200°F/650°C)

Rupture Strength (1000 h at 1400°F/760°C)

Rupture Strength (1000 h at 1600°F/870°C)

Rupture Strength (1000 h at 1800°F/980°C)