ASTM B582-07(2013)
(Specification)Standard Specification for Nickel-Chromium-Iron-Molybdenum-Copper Alloy Plate, Sheet, and Strip
Standard Specification for Nickel-Chromium-Iron-Molybdenum-Copper Alloy Plate, Sheet, and Strip
ABSTRACT
This specification deals with the standard requirements for nickel-chromium-iron-molybdenum-copper alloys (UNS N06007, N06975, N06985, and N06030) in the form of plate, sheet, and strip for use in general corrosive services. These materials shall undergo hot or cold rolling, solution annealing, and descaling. The plates shall have sheared or cut machined, abrasive cut, powder cut, or inert arc cut edges while the sheet and strip shall have sheared or slit edges. Heat and product analysis shall be performed to determine the chemical composition of the specimens which shall conform to the specified nickel, chromium, iron, molybdenum, copper, manganese, cobalt, carbon, tungsten, silicon, phosphorus, sulfur, columbium, tantalum, and titanium limits. The materials shall also conform to the mechanical property requirements for tensile strength, yield strength, elongation, and Rockwell hardness.
SCOPE
1.1 The specification2 covers plate, sheet, and strip of nickel-chromium-iron-molybdenum-copper alloys (UNS N06007, N06975, N06985, and N06030)* as shown in Table 1, for use in general corrosive service.TABLE 1 Chemical Requirements
Element
Composition Limits, %
Alloy N06007
Alloy N06975
Alloy N06985
Alloy N06030
Nickel
remainderA
47.0 to 52.0
remainderA
remainderA
Chromium
21.0 to 23.5
23.0 to 26.0
21.0 to 23.5
28.0 to 31.5
Iron
18.0 to 21.0
remainderA
18.0 to 21.0
13.0 to 17.0
Molybdenum
5.5 to 7.5
5.0 to 7.0
6.0 to 8.0
4.0 to 6.0
Copper
1.5 to 2.5
0.70 to 1.20
1.5 to 2.5
1.0 to 2.4
Manganese
1.0 to 2.0
1.0 max
1.0 max
1.5 max
Cobalt, max
2.5
...
5.0
5.0
Carbon, max
0.05
0.03
0.015
0.03
Tungsten
1.0 max
...
1.5 max
1.5 to 4.0
Silicon, max
1.0
1.0
1.0
0.8
Phosphorus, max
0.04
0.03
0.04
0.04
Sulfur, max
0.03
0.03
0.03
0.02
Columbium + tantalum
1.75 to 2.50
...
0.50 max
0.30 to 1.50
Titanium
...
0.70–1.50
...
... A The composition of the remainder element shall be determined arithmetically by difference.
1.2 The following products are covered under this specification:
1.2.1 Sheet and Strip—Hot or cold rolled, solution annealed, and descaled unless solution anneal is performed in an atmosphere yielding a bright finish.
1.2.2 Plate—Hot or cold rolled, solution annealed, and descaled.
1.3 The values stated in inch-pound units are to be regarded as standard. The values given in parentheses are mathematical conversions to SI units that are provided for information only and are not considered standard.
1.4 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to become familiar with all hazards including those identified in the appropriate Material Safety Data Sheet (MSDS) for this product/material as provided by the manufacturer, to establish appropriate safety and health practices, and determine the applicability of regulatory limitations prior to use.
General Information
Relations
Standards Content (Sample)
NOTICE: This standard has either been superseded and replaced by a new version or withdrawn.
Contact ASTM International (www.astm.org) for the latest information
Designation: B582 −07 (Reapproved 2013)
Standard Specification for
Nickel-Chromium-Iron-Molybdenum-Copper Alloy Plate,
Sheet, and Strip
This standard is issued under the fixed designation B582; the number immediately following the designation indicates the year of
original adoption or, in the case of revision, the year of last revision. A number in parentheses indicates the year of last reapproval. A
superscript epsilon (´) indicates an editorial change since the last revision or reapproval.
1. Scope 3. Terminology
1.1 The specification covers plate, sheet, and strip of 3.1 Definitions of Terms Specific to This Standard:
3 3
nickel-chromium-iron-molybdenum-copper alloys (UNS 3.1.1 cold-rolled plate, n—material ⁄16 to ⁄8 in. (4.76 to
N06007, N06975, N06985, and N06030)* as shown in Table 1,
9.52 mm), inclusive, in thickness.
for use in general corrosive service.
3.1.2 hot-rolled plate, n—material ⁄16 in. (4.76 mm) and
1.2 The following products are covered under this specifi- over in thickness.
cation: 3
3.1.3 plate, n—material ⁄16 in. (4.76 mm) and over in
1.2.1 Sheet and Strip—Hotorcoldrolled,solutionannealed,
thickness.
and descaled unless solution anneal is performed in an atmo-
3.1.4 sheet and strip, n—material under ⁄16 in. (4.76 mm) in
sphere yielding a bright finish.
thickness.
1.2.2 Plate—Hot or cold rolled, solution annealed, and
descaled.
4. General Requirements
1.3 The values stated in inch-pound units are to be regarded
4.1 Materials furnished to this specification shall conform to
as standard. The values given in parentheses are mathematical
the applicable requirements of Specification B906 unless
conversions to SI units that are provided for information only
otherwise provided herein.
and are not considered standard.
1.4 This standard does not purport to address all of the
5. Ordering Information
safety concerns, if any, associated with its use. It is the
5.1 It is the responsibility of the purchaser to specify all
responsibility of the user of this standard to become familiar
requirements that are necessary for material ordered under this
with all hazards including those identified in the appropriate
specification. Examples of such requirements include, but are
Material Safety Data Sheet (MSDS) for this product/material
not limited to, the following:
as provided by the manufacturer, to establish appropriate
5.1.1 Alloy—Table 1,
safety and health practices, and determine the applicability of
5.1.2 Dimensions—Thickness (in decimals of an inch),
regulatory limitations prior to use.
width, and length (inch or fractions of an inch),
2. Referenced Documents
5.1.3 Optional Requirement, Plate—How the plate is to be
cut (see 8.1 and Specification B906, Table A2.3),
2.1 ASTM Standards:
5.1.4 Certification—State if certification or a report of test
B906 Specification for General Requirements for Flat-
results is required (Specification B906),
Rolled Nickel and Nickel Alloys Plate, Sheet, and Strip
5.1.5 Purchaser Inspection—State which tests or inspec-
tions are to be witnessed (Specification B906), and
This specification is under the jurisdiction of ASTM Committee B02 on
5.1.6 Samples for Product (Check) Analysis—State whether
Nonferrous Metals and Alloys and is the direct responsibility of Subcommittee
samples should be furnished (Section 6).
B02.07 on Refined Nickel and Cobalt and Their Alloys.
Current edition approved Feb. 1, 2013. Published February 2013. Originally
approved in 1973. Last previous edition approved in 2007 as B582 – 07. DOI:
6. Chemical Composition
10.1520/B0582-07R13.
For ASME Boiler and Pressure Vessel Code applications, see related Specifi-
6.1 Heat Analysis—The material shall conform to the com-
cation SB-582 in Section II of that Code.
position limits specified in Table 1.
* New designation established in accordance withASTM E527 and SAE J1086,
Practice for Numbering Metals and Alloys (UNS).
6.2 Product (Check) Analysis—If a product (check) analysis
For referenced ASTM standards, visit the ASTM website, www.astm.org, or
is made by the purchaser, the material shall conform to the
contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM
requirements specified in Table 1 subject to the permissible
Standards volume information, refer to the standard’s Document Summary page on
the ASTM website. tolerances in Specification B906.
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B582 − 07 (2013)
TABLE 1 Chemical Requirements
Composition Limits, %
Element
Alloy N06007 Alloy N06975 Alloy N06985 Alloy N06030
A A A
Nickel remainder 47.0 to 52.0 remainder remainder
Chromium 21.0 to 23.5 23.0 to 26.0 21.0 to 23.5 28.0 to 31.5
A
Iron 18.0 to 21.0 remainder 18.0 to 21.0 13.0 to 17.0
Molybdenum 5.5 to 7.5 5.0 to 7.0 6.0 to 8.0 4.0 to 6.0
Copper 1.5 to 2.5 0.70 to 1.20 1.5 to 2.5 1.0 to 2.4
Manganese 1.0 to 2.0 1.0 max 1.0 max 1.5 max
Cobalt, max 2.5 . 5.0 5.0
Carbon, max 0.05 0.03 0.015 0.03
Tungsten 1.0 max . 1.5 max 1.5 to 4.0
Silicon, max 1.0 1.0 1.0 0.8
Phosphorus, max 0.04 0.03 0.04 0.04
Sulfur, max 0.03 0.03 0.03 0.02
Columbium + tantalum 1.75 to 2.50 . 0.50 max 0.30 to 1.50
Titanium . 0.70–1.50 . .
A
The composition of the remainder element shall be determined arithmetically by difference.
7. Mechanical Properties and Other Requirements
Density
3 3
Alloy lb/in. g/cm
7.1 Tensile Propert
...
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