ASTM B575-17

Standard Specification for Low-Carbon Nickel-Chromium-Molybdenum, Low-Carbon Nickel-Chromium-Molybdenum-Copper, Low-Carbon Nickel-Chromium-Molybdenum-Tantalum, Low-Carbon Nickel-Chromium-Molybdenum-Tungsten, and Low-Carbon Nickel-Molybdenum-Chromium Alloy Plate, Sheet, and Strip

ABSTRACT
This specification covers plate, sheet, and strip of low-carbon nickel-chromium-molybdenum alloys (UNS N10276, N06022, N06455, N06035, UNS N06058, UNS N06059), low carbon nickel-chromium-molybdenum-copper alloy (UNS N06200), low-carbon nickel-chromium-molybdenum-tantalum alloy (UNS N06210), and low-carbon nickel-chromium-molybdenum-tungsten alloy (UNS N06686) for use in general corrosive service. The materials shall conform to the required chemical composition for molybdenum, chromium, iorn, tungsten, cobalt, arbon, silicon, manganese, vanadium, phosphorus, sulfur, titanium, nickel, aluminum, copper, and tantalum. The alloys shall connform to the required tensile properties such as tensile strength, yield strength, elongation, and Rockwell hardness. Sheet and strip shall conform to the required grain sizes. Dimensions such as plate, sheet and strip thickness, width, length, straightness, squareness, flatness and edges shall be determined.
SCOPE
1.1 This specification2 covers plate, sheet, and strip of low-carbon nickel-chromium-molybdenum alloys (UNS N10276, N06022, N06455, N06035, N06044, UNS N06058, UNS N06059),3 low-carbon nickel-chromium-molybdenum-copper alloy (UNS N06200), low-carbon nickel-molybdenum-chromium (UNS N10362), low-carbon nickel-chromium-molybdenum-tantalum alloy (UNS N06210), and low-carbon nickel-chromium-molybdenum-tungsten alloy (UNS N06686) as shown in Table 1, for use in general corrosive service.
TABLE 1 Chemical Requirements    
Element  
Composition Limits, %  
Alloy
N06035  
Alloy
N06044  
Alloy
N10276  
Alloy
N06022  
Alloy
N06455  
Alloy
N06059  
Alloy
N06058  
Alloy
N06200  
Alloy
N06210  
Alloy
N10362  
Alloy
N06686  
Molybdenum  
7.60–9.00  
0.80-1.20  
15.0–17.0  
12.5–14.5  
14.0–17.0  
15.0–16.5  
18.5–21.0  
15.0–17.0  
18.0–20.0  
21.5–23.0  
15.0-17.0  
Chromium  
32.25–34.25  
43.5-45.3  
14.5–16.5  
20.0–22.5  
14.0–18.0  
22.0–24.0  
20.0–23.0  
22.0–24.0  
18.0–20.0  
13.8–15.6  
19.0-23.0  
Iron  
2.00 max  
0.3 max  
4.0–7.0  
2.0–6.0  
3.0 max  
1.5, max  
1.5, max  
3.0 max  
1.0 max  
1.25 max  
5.0 max  
Tungsten  
0.60 max  
...  
3.0–4.5  
2.5–3.5  
...  
...  
0.3 max  
...  
...  
...  
3.0-4.4  
Cobalt, max  
1.00  
...  
2.5  
2.5  
2.0  
0.3  
0.3  
2.0 max  
1.0  
...  
...  
Carbon, max  
0.050  
0.02  
0.010  
0.015  
0.015  
0.010  
0.010  
0.010  
0.015  
0.010  
0.010  
Silicon, max  
0.60  
0.20  
0.08  
0.08  
0.08  
0.10  
0.10  
0.08  
0.08  
0.08  
0.08  
Manganese, max  
0.50  
0.07-0.30  
1.0  
0.50  
1.0  
0.5  
0.5  
0.50  
0.5  
0.60  
0.75  
Vanadium, max  
0.20  
...  
0.35  
0.35  
...  
...  
...  
...  
0.35  
...  
...  
Phosphorus, max  
0.030  
0.020  
0.04  
0.02  
0.04  
0.015  
0.015  
0.025  
0.02  
0.025  
0.04  
Sulfur, max  
0.015  
0.020  
0.03  
0.02  
0.03  
0.010  
0.010  
0.010  
0.02  
0.010  
0.02  
Titanium  
...  
0.10-0.30  
...  
...  
0.7 max  
...  
...  
...  
...  
...  
0.02-0.25  
Nickel  
remainderA  
Bal  
remainderA  
remainderA  
remainderA  
Bal  
Bal  
remainderA  
remainderA  
remainderA  
remainderA  
Aluminum  
0.40 max  
0.30 max  
...  
...  
...  
0.1–0.4  
0.40 max  
0.50 max  
...  
0.50 max  
...  
Copper  
0.30 max  
...  
...  
...  
...  
0.50 max  
0.50 max  
1.3–1.9  
...  
...  
...  
Tantalum  
...  
...  
...  
...  
...  
...  
...  
...  
1.5–2.2  
...  
...  
Nitrogen  
...  
...  
...  
...  
...  
...  
0.02–0.15  
(A) Shall be determined arithmetically by difference.  
TABLE 2 Mechanical Property Requirements    
Alloy  
Tensile Strength, min, psi (MPa)  
Yield Strength (0.2 % Offset), min, psi
(MPa)  
Elongation in 2 in.
(50.8 mm) or 4DA
min, %  
Rockwell Hardness,B
max  
N10...

General Information

• Status: Historical
• Publication Date: 31-May-2017
• ICS: 77.150.40 - Nickel and chromium products
• Technical Committee: B02 - Nonferrous Metals and Alloys
• Drafting Committee: B02.07 - Refined Nickel and Cobalt and Their Alloys

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: B575 − 17
Standard Specification for
Low-Carbon Nickel-Chromium-Molybdenum, Low-Carbon
Nickel-Chromium-Molybdenum-Copper, Low-Carbon Nickel-
Chromium-Molybdenum-Tantalum, Low-Carbon Nickel-
Chromium-Molybdenum-Tungsten, and Low-Carbon Nickel-
1
Molybdenum-Chromium Alloy Plate, Sheet, and Strip
This standard is issued under the fixed designation B575; 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.
This standard has been approved for use by agencies of the U.S. Department of Defense.
1. Scope* by the manufacturer, to establish appropriate safety and health
2 practices, and determine the applicability of regulatory limi-
1.1 This specification covers plate, sheet, and strip of
tations prior to use.
low-carbon nickel-chromium-molybdenum alloys (UNS
1.5 This international standard was developed in accor-
N10276, N06022, N06455, N06035, N06044, UNS N06058,
3 dance with internationally recognized principles on standard-
UNS N06059), low-carbon nickel-chromium-molybdenum-
ization established in the Decision on Principles for the
copper alloy (UNS N06200), low-carbon nickel-molybdenum-
Development of International Standards, Guides and Recom-
chromium (UNS N10362), low-carbon nickel-chromium-
mendations issued by the World Trade Organization Technical
molybdenum-tantalum alloy (UNS N06210), and low-carbon
Barriers to Trade (TBT) Committee.
nickel-chromium-molybdenum-tungsten alloy (UNS N06686)
as shown in Table 1, for use in general corrosive service.
2. Referenced Documents
1.2 The following products are covered under this specifi- 4
2.1 ASTM Standards:
cation:
B906 Specification for General Requirements for Flat-
1.2.1 Sheet and Strip—Hot or cold rolled, solution annealed,
Rolled Nickel and Nickel Alloys Plate, Sheet, and Strip
and descaled unless solution anneal is performed in an atmo-
E112 Test Methods for Determining Average Grain Size
sphere yielding a bright finish.
E140 Hardness Conversion Tables for Metals Relationship
1.2.2 Plate—Hot or cold rolled, solution annealed, and
Among Brinell Hardness, Vickers Hardness, Rockwell
descaled.
Hardness, Superficial Hardness, Knoop Hardness, Sclero-
1.3 The values stated in inch-pound units are to be regarded scope Hardness, and Leeb Hardness
as standard. The values given in parentheses are mathematical E527 Practice for Numbering Metals and Alloys in the
conversions to SI units that are provided for information only Unified Numbering System (UNS)
and are not considered standard.
3. Terminology
1.4 This standard does not purport to address all of the
3.1 Definitions of Terms Specific to This Standard:
safety concerns, if any, associated with its use. It is the
3 3
3.1.1 cold-rolled plate, n—material ⁄16 to ⁄8 in. (4.76 to
responsibility of the user of this standard to become familiar
9.52 mm), inclusive, in thickness.
with all hazards including those identified in the appropriate
3
Safety Data Sheet (SDS) for this product/material as provided 3.1.2 hot-rolled plate, n—material ⁄16 in. (4.76 mm) and
over in thickness.
3
3.1.3 plate, n—material ⁄16 in. (4.76 mm) and over in
1
This specification is under the jurisdiction of ASTM Committee B02 on
thickness.
Nonferrous Metals and Alloys and is the direct responsibility of Subcommittee
3
3.1.4 sheet and strip, n—material under ⁄16 in. (4.76 mm) in
B02.07 on Refined Nickel and Cobalt and Their Alloys.
Current edition approved June 1, 2017. Published June 2017. Originally thickness.
ɛ1
approved in 1972. Last previous edition approved in 2015 as B575 – 15 . DOI:
10.1520/B0575-17.
2 4
For ASME Boiler and Pressure Vessel Code applications, see related Specifi- For referenced ASTM standards, visit the ASTM website, www.astm.org, or
cation SB-575 in Section II of that Code. contact ASTM Customer Service at [e-mail]. For Annual Book of ASTM
3
Designation established in accordance with Practice E527 and SAE J1086, Standards volume information, refer to the standard’s Document Summary page on
Practice for Numbering Metals and Alloys (UNS). the ASTM website.
*A Summary of Changes section appears at the end of this standard
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1

---------------------- Page: 1 ----------------------
B575 − 17
2
TABLE 1 Chemical Requirements
Composition Limits, %
Element
Alloy Alloy Alloy Alloy Alloy Alloy Alloy Alloy Alloy Alloy Alloy
N06035 N06044 N10276 N06022 N06455 N06059 N06058 N06200 N06210 N10362 N06686
Molybdenum 7.60–9.00 0.80-1.20 15.0–17.0 12.5–14.5 14.0–17.0 15.0–16.5 18.5–21.0 15.0–17.0 18.0–20
...

This document is not an ASTM standard and is intended only to provide the user of an ASTM standard an indication of what changes have been made to the previous version. Because
it may not be technically possible to adequately depict all changes accurately, ASTM recommends that users consult prior editions as appropriate. In all cases only the current version
of the standard as published by ASTM is to be considered the official document.
´1
Designation: B575 − 15 B575 − 17
Standard Specification for
Low-Carbon Nickel-Chromium-Molybdenum, Low-Carbon
Nickel-Chromium-Molybdenum-Copper, Low-Carbon Nickel-
Chromium-Molybdenum-Tantalum, Low-Carbon Nickel-
Chromium-Molybdenum-Tungsten, and Low-Carbon Nickel-
1
Molybdenum-Chromium Alloy Plate, Sheet, and Strip
This standard is issued under the fixed designation B575; 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.
This standard has been approved for use by agencies of the U.S. Department of Defense.
1
ε NOTE—The chemistry for aluminum in N06058 in Table 1 was editorially corrected in April 2016.
1. Scope*
2
1.1 This specification covers plate, sheet, and strip of low-carbon nickel-chromium-molybdenum alloys (UNS N10276,
3
N06022, N06455, N06035, N06044, UNS N06058, UNS N06059), low-carbon nickel-chromium-molybdenum-copper alloy
(UNS N06200), low-carbon nickel-molybdenum-chromium (UNS N10362), low-carbon nickel-chromium-molybdenum-tantalum
alloy (UNS N06210), and low-carbon nickel-chromium-molybdenum-tungsten alloy (UNS N06686) as shown in Table 1, for use
in general corrosive service.
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 Safety Data Sheet
(SDS) 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.
1.5 This international standard was developed in accordance with internationally recognized principles on standardization
established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued
by the World Trade Organization Technical Barriers to Trade (TBT) Committee.
2. Referenced Documents
4
2.1 ASTM Standards:
B906 Specification for General Requirements for Flat-Rolled Nickel and Nickel Alloys Plate, Sheet, and Strip
E112 Test Methods for Determining Average Grain Size
E140 Hardness Conversion Tables for Metals Relationship Among Brinell Hardness, Vickers Hardness, Rockwell Hardness,
Superficial Hardness, Knoop Hardness, Scleroscope Hardness, and Leeb Hardness
E527 Practice for Numbering Metals and Alloys in the Unified Numbering System (UNS)
1
This specification is under the jurisdiction of ASTM Committee B02 on Nonferrous Metals and Alloys and is the direct responsibility of Subcommittee B02.07 on Refined
Nickel and Cobalt and Their Alloys.
Current edition approved Oct. 1, 2015June 1, 2017. Published November 2015June 2017. Originally approved in 1972. Last previous edition approved in 20142015 as
ɛ1
B575 – 14.15 . DOI: 10.1520/B0575-15E01.10.1520/B0575-17.
2
For ASME Boiler and Pressure Vessel Code applications, see related Specification SB-575 in Section II of that Code.
3
Designation established in accordance with Practice E527 and SAE J1086, Practice for Numbering Metals and Alloys (UNS).
4
For referenced ASTM standards, visit the ASTM website, www.astm.org, or contact ASTM Customer Service at [e-mail]. For Annual Book of ASTM Standards
volume information, refer to the standard’s Document Summary page on the ASTM website.
*A Summary of Changes section appears at the end of this standard
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1

---------------------- Page: 1 ----------------------
B575 − 17
2
TABLE 1 Chemical Requirements
Composition Limits, %
Element
Alloy Alloy Alloy Alloy Alloy Alloy Alloy Alloy Alloy Alloy
N06035 N10276 N06022 N06455 N06059 N06058 N06200 N06210 N10362 N06686
Molybdenum 7.60–9.00 15.0–17.0 12.5–14.5 14.0–17.0 15.0–16.5 18.5–21.0 15.0–17.0 18.0
...