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Material(Grade)

321/321H(1.4541/1.4878) Mechanical Properties

Room Temperature Tensile Properties
Minimum mechanical properties of the stabilized Alloys 321 and 347 chromium-nickel grades in the annealed condition (2000°F [1093°C], air cooled) are shown in the table.

Elevated Temperature Tensile Properties
Typical elevated temperature mechanical properties for Alloys 321 and 347 sheet/strip are shown below. Strength of these stabilized alloys is distinctly higher than that of non-stabilized 304 alloys at temperatures of 1000°F (538°C) and above.

High carbon Alloys 321H and 347H (UNS32109 and S34700, respectively) have higher strength at temperatures above 1000°F (537°C). ASME maximum allowable design stress data for Alloy 347H reflects the higher strength of this grade in comparison to the lower carbon Alloy 347 grade. The Alloy 321H is not permitted for Section VIII applications and is limited to 800°F (427°C) use temperatures for Section III code applications.

Creep and Stress Rupture Properties
Typical creep and stress rupture data for Alloys 321 and 347 stainless steel tubing are shown in the figures below. The elevated temperature creep and stress rupture strengths of the stabilized steels are higher than those of unstabilized Alloys 304 and 304L. These superior properties for the 321 and 347 alloys permit design of pressure-containing components for elevated temperature service to higher stress levels as recognized in the ASME Boiler and Pressure Vessel Code.

Minimum Room Temperature Mechanical Properties Per ASTM A 240 and ASME SA-240
Alloy

Yield
Strength
.2% Offset
psi (MPa)

Ultimate
Tensile
Strength
psi (MPa)

Elongation
in 2 in. (%)

321 30,000
(205)
75,000
(515)
40.0
347 30,000
(205)
75,000
(515)
40.0
Minimum Room Temperature Mechanical Properties Per ASTM A 240 and ASME SA-240
Alloy Hardness, Maximum
Plate Sheet Strip
321

217
Brinell

95Rb 95Rb
347 201
Brinell
92Rb 92Rb

Typical Elevated Temperature Tensile Properties
Alloy 321 (0.036 inch thick / 0.9 mm thick)
Test Temperature Yield Strength
.2% Offset psi
(MPa)
Ultimate Tensile Strength
psi
(MPa)

% Elongation
in 2 in.

°F °C
68 20 31,400
(215)
85,000
(590)
55.0
400 204 23,500
(160)
66,600
(455)
38.0
800 427 19,380
(130)
66,300
(455)
32.0
1000 538 19,010
(130)
64,400
(440)
32.0
1200 649 19,000
(130)
55,800
(380)
28.0
1350 732 18,890
(130)
41,500
(285)
26.0
1500 816 17,200
(115)
26,000
(180)
45.0

Typical Elevated Temperature Tensile Properties
Alloy 347 (0.060 inch thick / 1.54 mm thick)
Test Temperature Yield Strength
.2% Offset psi
(MPa)
Ultimate Tensile Strength
psi
(MPa)

% Elongation
in 2 in.

°F °C
68 20

36,500
(250)

93,250
(640)
45.0
400 204 36,600
(250)
73,570
(505)
36.0
800 427 29,680
(205)
69,500
(475)
30.0
1000 538 27,400
(190)
63,510
(435)
27.0
1200 649 24,475
(165)
52,300
(360)
26.0
1350 732 22,800
(155)
39,280
(270)
40.0
1500 816 18,600
(125)
26,400
(180)
50.0

Impact Strength
Alloys 321 and 347 have excellent toughness at room and sub-zero temperatures. In the following table are Charpy V-notch impact values for annealed Alloy 347 after holding the samples for one hour at the indicated testing temperatures. Data for Alloy 321 would be expected to be similar.

Impact Strength Alloys 321 and 347
Test Temperature Charpy Impact Energy Absorbed
°F °C Ft-lb Joules
75 24 90 122
-25 -32 66 89
-80 -62 57 78

Fatigue Strength
The fatigue strength of practically every metal is affected by corrosive conditions, surface finish, form, and mean stress. For this reason, no definite values can be shown which would be representative of the fatigue strength under all operating conditions. The fatigue endurance limits of Alloys 321 and 347 are approximately 35% of their tensile strengths.

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