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ASTM B333-03(2013)

Historical Reaffirmation

Standard Specification for Nickel-Molybdenum Alloy Plate, Sheet, and Strip

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1.1 This specification2 covers plate, sheet, and strip of nickel-molybdenum alloys (UNS N10001, N10665, N10675, N10629, and N10624)* as shown in Table 1, for use in general corrosive service.

TABLE 1 Chemical Requirements

Element

Composition Limits, %

 

Alloy
N10001

Alloy
N10665

Alloy
N10675

Alloy
N10629

Alloy
N10624

Nickel

remainderA

remainderA

65.0 min

remainderA

Bal

Molybdenum

26.0–30.0

26.0–30.0

27.0–32.0

26.0–30.0

21.0-25.0

Iron

 4.0–6.0

 2.0 max

 1.0–3.0

 1.0–6.0

 5.0-8.0

Chromium

 1.0 max

 1.0 max

 1.0–3.0

 0.5–1.5

 6.0-10.0

Carbon, max

 0.05

 0.02

 0.01

 0.01

 0.01

Silicon, max

 1.0

 0.10

 0.10

 0.05

 0.10

Cobalt, max

 2.5

 1.00

 3.0

 2.5

 1.0

Manganese,
 max

 1.0

 1.0

 3.0

 1.5

 1.0

Phosphorus,
 max

 0.04

 0.04

 0.030

 0.04

 0.025

Sulfur, max

 0.03

 0.03

 0.010

 0.01

 0.01

Vanadium

 0.2–0.4

 ...

 0.20 max

 ...

 ...

Nickel plus
 Molybdenum

 ...

 ...

94.0–98.0

 

 ...

Aluminum

 ...

 ...

 0.50 max

 0.1–0.5

 0.5

Columbium
 (Nb), max

 ...

 ...

 0.20

 

 ...

Copper, max

 ...

 ...

 0.20

 0.5

 0.5

Tantalum,
 max

 ...

 ...

 0.20

 

 ...

Titanium,
 max

 ...

 ...

 0.20

 

 ...

Tungsten,
 max

 ...

 ...

 3.0

 

 ...

Zirconium,
 max

 ...

 ...

 0.10

 

 ...

Magnesium,
 max

 ...

 ...

 ...

 ...

 ...

A See Specification B906.
TABLE 2 Mechanical Property Requirements

Alloy

Thickness,
in. (mm)

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

 

 

Sheet and Strip

 

 

 

N10001

Under 3/16 (4.76)

115 000 (795)

50 000 (345)

45

100 HRB

N10665

Under 3/16 (4.76)

110 000 (760)

51 000 (350)

40

100 HRB

N10675

Under 3/16 (4.76)

110 000 (760)

51 000 (350)

40

100 HRB

N10629

Under 3/16 (4.76)

110 000 (760)

51 000 (350)

40

100 HRB

N10624

Under 3/16 (4.76)

104 000 (720)

46 000 (320)

40

100 HRB

 

 

Plate

 

 

 

N10001

3/16 to 21/2 in. (4.76 to 63.5 mm), incl

100 000 (690)

45 000 (310)

40

100 HRB

N10665

3/16 to 21/2 in. (4.76 to 63.5 mm), incl

110 000 (760)

51 000 (350)

40

100 HRB

N10675

3/16 to 21/2 in. (4.76 to 63.5 mm), incl

110 000 (760)

51 000 (350)

40

100 HRB

N10629

3/16 to 21/2 in. (4.76 to 63.5 mm), incl

110 000 (760)

51 000 (350)

40

100 HRB

N10624

3/16 to 21/2 in. (4.76 to 63.5 mm), incl

104 000 (720)

46 000 (320)

40

100 HRB

AD 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 for rejection or acceptance. For approximate hardness conversions, see Hardness Conversion Tables E140.

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.


This specification covers plate, sheet, and strip of nickel-molybdenum alloys covering UNS N10001, N10665, N10675, N10629, and N10624 for use in general corrosive service. Product analysis shall be performed on the alloy and shall conform to the chemical composition requirement in nickel, molybdenum, iron, chromium, carbon, silicon, cobalt, manganese, phosphorus, sulfur, vanadium, nickel, molybdenum, aluminum, columbium, copper, tantalum, titanium, tungsten, zirconium, and magnesium. Sheet and strip shall undergo hot or cold rolling, solution annealing, and descaling unless solution annealed in atmosphere. Plates shall undergo hot or cold rolling, solution annealing, and descaling. The material shall conform to the required tensile properties such as tensile strength, yield strength, elongation, and Rockwell hardness. Sheet and strip shall conform to the specified grain size requirement


SDO ASTM: ASTM International
Document Number B333
Publication Date Feb. 1, 2013
Language en - English
Page Count 3
Revision Level 03(2013)
Supercedes
Committee B02.07
Publish Date Document Id Type View
June 10, 2003 B0333-03 Revision
Jan. 1, 1997 B0333-98 Revision
Nov. 1, 2018 B0333-03R18 Reaffirmation
Feb. 1, 2013 B0333-03R13 Reaffirmation
Nov. 1, 2008 B0333-03R08 Reaffirmation