Warning

Your browser does not currently support JavaScript. It is possible that some feature will not work. JavaScript is required for the online shop to function fully. Here are the instructions on how to enable JavaScript in your web browser.

Displayed currency: USD

Price display: excl. VAT

Additional information

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

Translate name

STANDARD published on 1.6.2017

Language
Format	PDF - Immediate download - 73.00 USD Print design - 73.00 USD
Availability	IN STOCK
Price	73.00 USD excl. VAT
73.00 USD

The information about the standard:

Designation standards: ASTM B575-17
Note: WITHDRAWN
Publication date standards: 1.6.2017
SKU: NS-686091
The number of pages: 4
Approximate weight : 12 g (0.03 lbs)
Country: American technical standard
Category: Technical standards ASTM

Send to a colleague

Query

The category - similar standards:

Nickel and chromium products

Annotation of standard text ASTM B575-17 :

Keywords:

N06022, N06035, N06044, N06058, N06059, N06200, N06210, N10362, N06455, N06686, N10276, plate, sheet, strip,, ICS Number Code 77.150.40 (Nickel and chromium products)

Additional information

1. 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

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

2.0

0.3

2.0 max

1.0

...

Carbon, max

0.050

0.02

0.010

0.015

0.010

0.015

0.010

Silicon, max

0.60

0.20

0.08

0.10

0.08

Manganese, max

0.50

0.07-0.30

1.0

0.50

1.0

0.5

0.50

0.5

0.60

0.75

Vanadium, max

0.20

...

0.35

...

0.35

...

Phosphorus, max

0.030

0.020

0.04

0.02

0.04

0.015

0.025

0.02

0.025

0.04

Sulfur, max

0.015

0.020

0.03

0.02

0.03

0.010

0.02

0.010

0.02

Titanium

...

0.10-0.30

...

0.7 max

...

0.02-0.25

Nickel

remainder^A

Bal

remainder^A

Bal

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

1.3–1.9

...

Tantalum

...

1.5–2.2

...

Nitrogen

...

0.02–0.15

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)

100 HRB

N06022

100 000 (690)

45 000 (310)

100 HRB

N06455

100 000 (690)

40 000 (276)

100 HRB

N06035

85 000 (586)

35 000 (241)

100 HRB

N06044

100 000 (690)

45 000 (310)

100 HRB

N06058

110 000 (760)

52 000 (360)

100 HRB

N06059

100 000 (690)

45 000 (310)

100 HRB

N06200

100 000 (690)

45 000 (310)

100 HRB

N10362

105 000 (725)

45 000 (310)

100 HRB

N06686

100 000 (690)

45 000 (310)

100 HRB

N06210

100 000 (690)

45 000 (310)

100 HRB

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

B906-22	Standard Specification for General Requirements for Flat-Rolled Nickel and Nickel Alloys Plate, Sheet, and Strip
E140-12B(2019)e1	Standard Hardness Conversion Tables for Metals Relationship Among Brinell Hardness, Vickers Hardness, Rockwell Hardness, Superficial Hardness, Knoop Hardness, Scleroscope Hardness, and Leeb Hardness (Includes all amendments and changes 5/7/2019).
E527-23	Standard Practice for Numbering Metals and Alloys in the Unified Numbering System (UNS)
E112-13(2021)	Standard Test Methods for Determining Average Grain Size

We recommend:

Technical standards updating

Do you want to make sure you use only the valid technical standards?
We can offer you a solution which will provide you a monthly overview concerning the updating of standards which you use.

Would you like to know more? Look at this page.