ASTM B 575 : 2017 : REDLINE

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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

Available format(s): PDF

Language(s): English

Published date: 19-06-2017

Publisher: American Society for Testing and Materials

Abstract - (Show below) - (Hide below)

CONTAINED IN VOL. 02.04, 2017 Defines plate, sheet, and strip of low-carbon nickel-chromium-molybdenum alloys (UNS N10276, N10276, N06022, N06455, N06035, 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) for use in general corrosive service.

Scope - (Show below) - (Hide below)

1.1This 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, %
Element	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	remainder^A	Bal	remainder^A	remainder^A	remainder^A	Bal	Bal	remainder^A	remainder^A	remainder^A	remainder^A
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 4D^A min, %	Rockwell Hardness,^B max
N10276	100 000 (690)	41 000 (283)	40	100 HRB
N06022	100 000 (690)	45 000 (310)	45	100 HRB
N06455	100 000 (690)	40 000 (276)	40	100 HRB
N06035	85 000 (586)	35 000 (241)	30	100 HRB
N06044	100 000 (690)	45 000 (310)	30	100 HRB
N06058	110 000 (760)	52 000 (360)	40	100 HRB
N06059	100 000 (690)	45 000 (310)	45	100 HRB
N06200	100 000 (690)	45 000 (310)	45	100 HRB
N10362	105 000 (725)	45 000 (310)	40	100 HRB
N06686	100 000 (690)	45 000 (310)	45	100 HRB
N06210	100 000 (690)	45 000 (310)	45	100 HRB

(A)D refers to the diameter of the tension specimen.

(B)Hardness values are shown for information purposes only and are not to be used as a basis of acceptance or rejection. For approximate hardness conversions, see Hardness Conversion Tables E140.

1.2The following products are covered under this specification:

1.2.1Sheet and Strip—Hot or cold rolled, solution annealed, and descaled unless solution anneal is performed in an atmosphere yielding a bright finish.

1.2.2Plate—Hot or cold rolled, solution annealed, and descaled.

1.3The 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.

1.4This 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.

1.5This 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.

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Committee	B 02
Document Type	Redline
ISBN
Pages
Published
Publisher	American Society for Testing and Materials
Status	Current

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