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

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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, ,%
Element	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	remainder^A	Bal	remainder^A	remainder^A	remainder^A	Bal	Bal	remainder^A	remainder^A	remainder^A	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	0.50 max	1.3–,1.9	...	...	...
Tantalum	...	...	...	...	...	...	...	...	1.5–,2.2	...	...
Nitrogen	...	...	...	...	...	...	0.02–,0.15	,	,	,	,

(A) ,Shall be determined arithmetically by difference.

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ASTM C1272-17

ASTM B575-17

ASTM B575-17

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