Standard Specification for Nickel-Molybdenum Alloy Rod

ABSTRACT
This specification covers rod of nickel-molybdenum alloys of UNS N10001, N10665, N10675, N10629, and N10624 for use in general corrosive service. The material shall conform to the required chemical composition for nickel, molybdenum, iron, chromium, carbon, silicon, cobalt, manganese, phosphorus, sulfur, vanadium, nickel, molybdenum, aluminum, columbium, copper, tantalum, titanium, tungsten, zirconium, and magnesium. The alloys shall conform to the required mechanical properties such as tensile strength, yield strength, elongation, and Rockwell hardness.
SCOPE
1.1 This specification2 covers rod 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 12.1  
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) excl 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) incl in diameter, hot or cold finished, solution annealed, ground or turned.  
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.

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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:B335 −03(Reapproved 2013)
Standard Specification for
Nickel-Molybdenum Alloy Rod
This standard is issued under the fixed designation B335; 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 Department of Defense.
1. Scope Check Analysis Limits for Nickel, Nickel Alloys and
2 Cobalt Alloys
1.1 This specification covers rod of nickel-molybdenum
E8 Test Methods for Tension Testing of Metallic Materials
alloys (UNS N10001, N10665, N10675, N10629, and
E29 Practice for Using Significant Digits in Test Data to
N10624)* as shown in Table 1, for use in general corrosive
Determine Conformance with Specifications
service.
E55 Practice for Sampling Wrought Nonferrous Metals and
1.2 The following products are covered under this specifi-
Alloys for Determination of Chemical Composition
cation:
E1473 Test Methods for Chemical Analysis of Nickel,
5 3
1.2.1 Rods ⁄16 to ⁄4 in. (7.94 to 19.05 mm) excl in diameter,
Cobalt, and High-Temperature Alloys
hot or cold finished, solution annealed and pickled or mechani-
cally descaled.
3. Terminology
3 1
1.2.2 Rods ⁄4 to 3 ⁄2 in. (19.05 to 88.9 mm) incl in diameter,
3.1 Definitions of Terms Specific to This Standard:
hot or cold finished, solution annealed, ground or turned.
3.1.1 rod, n—a product of round solid section furnished in
1.3 The values stated in inch-pound units are to be regarded
straight lengths.
as standard. The values given in parentheses are mathematical
conversions to SI units that are provided for information only
4. Ordering Information
and are not considered standard.
4.1 It is the responsibility of the purchaser to specify all
1.4 This standard does not purport to address all of the
requirements that are necessary for material ordered under this
safety concerns, if any, associated with its use. It is the
specification. Examples of such requirements include, but are
responsibility of the user of this standard to become familiar
not limited to the following:
with all hazards including those identified in the appropriate
4.1.1 Alloy—Table 1.
Material Safety Data Sheet (MSDS) for this product/material
4.1.2 Dimensions—Nominal diameter and length. The
as provided by the manufacturer, to establish appropriate
shortest usable multiple length shall be specified (Table 2).
safety and health practices, and determine the applicability of
regulatory limitations prior to use. 4.1.3 Certification—State if certification or a report of test
results is required (Section 16).
2. Referenced Documents
4.1.4 Purchaser Inspection—State which tests or inspec-
tions are to be witnessed (Section 13).
2.1 ASTM Standards:
4.1.5 Samples for Product (Check) Analysis—State whether
B880 Specification for General Requirements for Chemical
samples should be furnished (9.2.2).
1 5. Chemical Composition
This specification is under the jurisdiction of ASTM Committee B02 on
Nonferrous Metals and Alloys and is the direct responsibility of Subcommittee
5.1 The material shall conform to the composition limits
B02.07 on Refined Nickel and Cobalt and Their Alloys.
specified in Table 1.
Current edition approved Feb. 1, 2013. Published February 2013. Originally
approved in 1958. Last previous edition approved in 2008 as B335 – 03 (2008).
5.2 If a product (check) analysis is made by the purchaser,
DOI: 10.1520/B0335-03R13.
For ASME Boiler and Pressure Vessel Code applications see related Specifi- the material shall conform to the requirements specified in
cation SB-335 in Section II of that Code.
Table 1 subject to the permissible tolerances in B880.
* New designation established in accordance withASTM E527 and SAE J1086,
Recommended Practice for Numbering Metals and Alloys (UNS).
6. Mechanical Properties and Other Requirements
For referenced ASTM standards, visit the ASTM website, www.astm.org, or
contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM
6.1 The mechanical properties of the material at room
Standards volume information, refer to the standard’s Document Summary page on
the ASTM website. temperature shall conform to those shown in Table 3.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
B335−03(2013)
TABLE 1 Chemical Requirements
Density
3 3
Alloy lb/in g/cm
Composition Limits, %
N10001 0.334 9.24
Element
Alloy Alloy Alloy Alloy Alloy
N10665 0.333 9.22
N10001 N10665 N10675 N10629 N10624
N10675 0.333 9.22
A A A
Nickel remainder remainder 65.0 min remainder Bal
N10629 0.333 9.22
Molybdenum 26.0–30.0 26.0–30.0 27.0–32.0 26.0–30.0 21.0-25.0
N10624 0.322 8.9
Iron 4.0–6.0 2.0 max 1.0–3.0 1.0–6.0 5.0-8.0
7.7 Straightness—The maximum curvature (depth of chord)
Chromium 1.0 max 1.0 max 1.0–3.0 0.5–1.5 6.0-10.0
Carbon, 0.05 0.02 0.01 0.01 0.01 shall not exceed 0.050 in. multiplied by the length of the chord
max
in feet (0.04 mm multiplied by the length in centimetres).
Silicon, max 1.0 0.10 0.10 0.05 0.10
Cobalt, max 2.5 1.00 3.0 2.5 1.0
8. Workmanship, Finish, and Appearance
Manganese, 1.0 1.0 3.0 1.5 1.0
max
8.1 The material shall be uniform in quality and condition,
Phosphorus, 0.04 0.04 0.030 0.04 0.025
max
smooth, and free of injurious imperfections.
Sulfur, max 0.03 0.03 0.010 0.01 0.01
Vanadium 0.2–0.4 . 0.20 max . .
9. Sampling
Nickel plus . . 94.0–98.0 .
Molybdenum
9.1 Lots for Chemical Analysis and Mechanical Testing:
Aluminum . . 0.50 max 0.1–0.5 0.5
9.1.1 A lot for chemical analysis shall consist of one heat.
Columbium . . 0.20 .
(Nb), max 9.1.2 A lot of bar for mechanical testing shall be defined as
Copper, max . . 0.20 0.5 0.5
the material from one heat in the same condition and specified
Tantalum, . . 0.20 .
diameter.
max
Titanium, . . 0.20 .
9.2 Sampling for Chemical Analysis:
max
9.2.1 A representative sample shall be obtained from each
Tungsten, . . 3.0 .
max
heat during pouring or subsequent processing.
Zirconium, . . 0.10 .
9.2.2 Product (check) analysis shall be wholly the respon-
max
Magnesium, . . . . . sibility of the purchaser.
max
9.3 Sampling for Mechanical Testing:
A
See 12.1
9.3.1 Arepresentativesampleshallbetakenfromeachlotof
finished material.
10. Number of Tests and Retests
7. Dimensions and Permissible Variations
10.1 Chemical Analysis—One test per heat.
7.1 Diameter—The permissible variations from the speci-
10.2 Tension Tests—One test per lot.
fied diameter shall be as prescribed in Table 2.
10.3 Retests—If the specimen used in the mechanical test of
7.2 Out of Roundness—The permissible variation in round-
any lot fails to meet the specified requirements, two additional
ness shall be as prescribed in Table 2.
specimens shall be taken from different sample pieces and
tested. The results of the tests on both of these specimens shall
7.3 Machining Allowances—When the surfaces of finished
meet the specified requirements.
material are to be machined, the following allowances are
suggested for normal machining operations.
11. Specimen Preparation
7.3.1 As-finished (Annealed and Descaled)—For diameters
5 11 1
of ⁄16 to ⁄16 in. (7.94 to 17.46 mm
...

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