Table 2.2.1.0: (b). Design Mechanical and Physical Properties of AISI 1025 Carbon Steel

MIL-HDBK-5J, Metallic Materials and Elements for Aerospace Vehicle Structures

Last Updated 29 Oct 2026

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Specification	AMS 5046 and AMS-S-7952	AMS 5075, AMS 5077 and AMS-T-5066^a	ASTM A 108
Form.	Sheet, strip, and plate	Tubing	Bar
Condition	Annealed	Normalized	All
Thickness, in.
Basis	S	S	S^b
Mechanical Properties:
F_tu ksi:
L	55	55	55
LT	55	55	55
ST			55
F_ty ksi:
L	36	36	36
LT	36	36	36
ST			36
F_cy ksi:
L	36	36	36
LT	36	36	36
ST			36
F_su ksi	35	35	35
F_bru ksi:
(e/D = 1.5)
(e/D = 2.0)	90	90	90
F_bry ksi:
(e/D = 1.5)
(e/D = 2.0)
e, percent:
L		c	c
LT	c
E, 10³ ksi	29.0
E_c, 10³ ksi	29.0
G, 10³ ksi	11.0
μ	0.32
Physical Properties:
ω, lb/in.³	0.284
C, Btu/(lb)(°F)	0.116 (122 to 212°F)
K, Btu/[(hr)(ft²)(°F)/ft]	30.0 (at 32°F)
α, 10^-6 in./in./°F	See Figure 2.2.1.0

MIL-HDBK-5J

MIL-HDBK-5J, Metallic Materials and Elements for Aerospace Vehicle Structures

Last Updated 29 Oct 2026

Hover any section to copy its link or text, ask Copilot about it, or bookmark it.

Specification	AMS 5046 and AMS-S-7952	AMS 5075, AMS 5077 and AMS-T-5066^a	ASTM A 108
Form.	Sheet, strip, and plate	Tubing	Bar
Condition	Annealed	Normalized	All
Thickness, in.
Basis	S	S	S^b
Mechanical Properties:
F_tu ksi:
L	55	55	55
LT	55	55	55
ST			55
F_ty ksi:
L	36	36	36
LT	36	36	36
ST			36
F_cy ksi:
L	36	36	36
LT	36	36	36
ST			36
F_su ksi	35	35	35
F_bru ksi:
(e/D = 1.5)
(e/D = 2.0)	90	90	90
F_bry ksi:
(e/D = 1.5)
(e/D = 2.0)
e, percent:
L		c	c
LT	c
E, 10³ ksi	29.0
E_c, 10³ ksi	29.0
G, 10³ ksi	11.0
μ	0.32
Physical Properties:
ω, lb/in.³	0.284
C, Btu/(lb)(°F)	0.116 (122 to 212°F)
K, Btu/[(hr)(ft²)(°F)/ft]	30.0 (at 32°F)
α, 10^-6 in./in./°F	See Figure 2.2.1.0