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ASTM B574-17

Historical Revision

Standard Specification for Low-Carbon Nickel-Chromium-Molybdenum, Low-Carbon Nickel-Molybdenum-Chromium, Low-Carbon Nickel-Molybdenum-Chromium-Tantalum, Low-Carbon Nickel-Chromium-Molybdenum-Copper, and Low-Carbon Nickel-Chromium-Molybdenum-Tungsten Alloy Rod and Bar

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1.1 This specification2 covers rod of low-carbon nickel-chromium-molybdenum alloys (UNS N10276, N06022, N06035, N06044, N06455, N06058, and N06059), low-carbon nickel-molybdenum-chromium (USN N10362), low-carbon nickel-molybdenum-chromium-tantalum (UNS N06210), low-carbon nickel-chromium-molybdenum-copper alloy (UNS N06200), and low-carbon nickel-chromium-molybdenum-tungsten (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
N10362

Alloy
N06210

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

21.5-23.0

18.0–20.0

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

13.8-15.6

18.0–20.0

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

1.25 max

1.0 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 max

2.0 max

...

1.0

...

Carbon, max

0.050

0.02

0.010

0.015

0.015

0.010

0.010

0.010

0.010

0.015

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

0.5

0.60

0.5

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

0.025

0.02

0.04

Sulfur, max

0.015

0.020

0.03

0.02

0.03

0.010

0.010

0.010

0.010

0.02

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) See 12.1.1.

TABLE 2 Permissible Variations in Diameter and Out-of-Roundness of As Cold Finished Rods

Specified Diameter, in. (mm)

Permissible Variations, in. (mm)

Diameter

Out of Roundness, max

+

1/4 –7/16 (6.35–11.11), incl

0.012 (0.30)

0.012 (0.30)

0.018 (0.46)

Over 7/16 –5/8 (11.11–15.87), incl

0.014 (0.36)

0.014 (0.36)

0.020 (0.51)

Over 5/8 –3/4 (15.87–19.05), excl

0.016 (0.41)

0.016 (0.41)

0.024 (0.61)

3/4 –31/2 (19.05–88.9), incl

0.010 (0.25)

0.010 (0.25)

0.010 (0.25)

TABLE 3 Mechanical Property Requirements for As Cold Finished Rods

Alloy

Grade

Tensile Strength, min, psi (MPa)

Yield Strength (0.2 % Offset), min, psi
(MPa)

Elongation in 2 in.
(50.8 mm) or 4DA
min, %

N06059

1

120 (827)

85 (586)

20

 

2

135 (931)

125 (862)

20

 

3

160 (1103)

150 (1034)

15

N06686

1

120 (827)

85 (586)

20

 

2

135 (931)

125 (862)

20

 

3

160 (1103)

150 (1034)

20

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

TABLE 4 Permissible Variations in Diameter and Out-of-Roundness of Hot or Cold Finished, Solution Annealed Rods

Specified Diameter, in. (mm)

Permissible Variations, in. (mm)

Diameter

Out of Roundness, max

+

5/16 Hot-Finished, Annealed, and Descaled Rods

5/16 –7/16 (7.94–11.11), incl

0.012 (0.30)

0.012 (0.30)

0.018 (0.46)

Over 7/16 –5/8 (11.11–15.87), incl

0.014 (0.36)

0.014 (0.36)

0.020 (0.51)

Over 5/8 –3/4 (15.87–19.05), excl

0.016 (0.41)

0.016 (0.41)

0.024 (0.61)

Hot-Finished, Annealed, and Ground or Turned Rods

3/4 –31/2 (19.05–88.9), incl

0.010 (0.25)

0

0.008 (0.20)

TABLE 5 Mechanical Property Requirements for Hot or Cold Finished, Solution Annealed Rods

Alloy

Tensile Strength, min, psi (MPa)

Yield Strength (0.2 % Offset), min, psi
(MPa)

Elongation in 2 in.
(50.8 mm) or 4DA
min, %

N10276

100 000 (690)

41 000 (283)

40

N06022

100 000 (690)

45 000 (310)

45

N06035

 85 000 (586)

35 000 (241)

30

N06044

100 000 (690)

45 000 (310)

30

N06455

100 000 (690)

40 000 (276)

40

N06058

110 000 (760)

52 000 (360)

40

N06059

100 000 (690)

45 000 (310)

45

N06200

100 000 (690)

45 000 (310)

45

N10362

105 000 (725)

45 000 (310)

40

N06686

100 000 (690)

45 000 (310)

45

N06210

100 000 (690)

45 000 (310)

45

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

1.2 The following products are covered under this specification:

1.2.1 Rods 5/16 to 3/4 in. (7.94 to 19.05 mm), exclusive, in diameter, hot or cold finished, solution annealed and pickled, or mechanically descaled.

1.2.2 Rods 3/4 to 31/2 in. (19.05 to 88.9 mm), inclusive, in diameter, hot or cold finished, solution annealed, ground or turned.

1.2.3 Rods 1/4 to 3 1/2 in. (6.35 to 88.9 mm), inclusive, in diameter, solution annealed, cold finished, as cold finished, ground or turned (N06059 and N06686 only, see Table 2 and Table 3).

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.


This specification2 covers rod of low-carbon nickel-chromium- molybdenum alloys (UNS N10276, N06022, N06035, N06455, N06058, and N06059), low-carbon nickel-molybdenum- chromium-tantalum (UNS N06210), low-carbon nickel-chromium-molybdenum-copper alloy (UNS N06200), and low-carbon nickel-chromium-molybdenum-tungsten (UNS N06686), for use in general corrosive service. Product and chemical analyses shall be performed on the materials and shall conform to the required chemical composition in molybdenum, chromium, iron, tungsten, cobalt, carbon, silicon, manganese, vanadium, phosphorus, sulfur, titanium, nickel, aluminum, copper, and tantalum. Tension test shall be performed and shall comply to required mechanical properties for hot or cold finished, solution annealed rods such as tensile strength, yield strength, and elongation.


SDO ASTM: ASTM International
Document Number B574
Publication Date June 1, 2017
Language en - English
Page Count 6
Revision Level 17
Supercedes
Committee B02.07
Publish Date Document Id Type View
Nov. 1, 2023 B0574-23 Revision
Nov. 1, 2018 B0574-18 Revision
June 1, 2017 B0574-17 Revision
Oct. 1, 2015 B0574-15 Revision
Oct. 1, 2010 B0574-10 Revision
June 1, 2006 B0574-06E01 Revision
June 1, 2006 B0574-06 Revision
Feb. 1, 2005 B0574-05 Revision
Feb. 1, 2004 B0574-04 Revision
Oct. 10, 1999 B0574-99A Revision