logo

Standards Manage Your Business

We Manage Your Standards

ASTM

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

Standard Details

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

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

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) 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 4DA
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)

Status : Historical
Standard Type: Main
Document No: ASTM B575 : 17
Document Year: 2017
Pages: 4
  • Section Volume:
  • 02.04 Volume 02.04 Nonferrous Metals - Nickel, Titanium, Lead, Tin, Zinc, Zirconium, Precious, Reactive, Refractory Metals and Alloys: Materials for Thermostats, Electrical Heating and Resistance Contact, and Connectors

Life Cycle

Currently Viewing

Historical
ASTM B575 : 17

Historical

Historical

Historical

Historical

Historical

Historical

© Copyright 2024 BSB Edge Private Limited.