Table 6.3.8.0: (b). Design Mechanical and Physical Properties of Waspaloy

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

Last Updated 29 Oct 2026

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	AMS 5544		AMS 5704	AMS 5706 and AMS 5707
Specification	<0.020	>0.020	<3.500	<3.500
Form	Sheet, strip, and plate		Forging	Bar, forging, and ring
Condition	Solution, stabilization, and precipitation heat treated
Thickness, in.	<0.020	>0.020	<3.500	<3.500
Basis	S	S	S	S
Mechanical Properties:
F_tu, ksi:
L			175	160
LT	170	175
F_ty, ksi:
L			120	110
LT	110	115
F_cy, ksi:
L
LT
F_su, ksi
F_bru, ksi:
(e/D = 1.5)
(e/D = 2.0)
F_bry, ksi:
(e/D = 1.5)
(e/D = 2.0)
e, percent:
L			15	15
LT	15	20
RA, percent:
L			18	18
E, 10³ ksi			30.6
E_c, 10³ ksi
G, 10³ ksi.
μ
Physical Properties:
ω, lb/in.³				0.298
C, Btu/(lb)(°F)				See Figure 6.3.8.0
K, Btu/[(hr)(ft²)(°F)/ft]				See Figure 6.3.8.0
a, 10^-6 in./in./°F.				See Figure 6.3.8.0

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.

	AMS 5544		AMS 5704	AMS 5706 and AMS 5707
Specification	<0.020	>0.020	<3.500	<3.500
Form	Sheet, strip, and plate		Forging	Bar, forging, and ring
Condition	Solution, stabilization, and precipitation heat treated
Thickness, in.	<0.020	>0.020	<3.500	<3.500
Basis	S	S	S	S
Mechanical Properties:
F_tu, ksi:
L			175	160
LT	170	175
F_ty, ksi:
L			120	110
LT	110	115
F_cy, ksi:
L
LT
F_su, ksi
F_bru, ksi:
(e/D = 1.5)
(e/D = 2.0)
F_bry, ksi:
(e/D = 1.5)
(e/D = 2.0)
e, percent:
L			15	15
LT	15	20
RA, percent:
L			18	18
E, 10³ ksi			30.6
E_c, 10³ ksi
G, 10³ ksi.
μ
Physical Properties:
ω, lb/in.³				0.298
C, Btu/(lb)(°F)				See Figure 6.3.8.0
K, Btu/[(hr)(ft²)(°F)/ft]				See Figure 6.3.8.0
a, 10^-6 in./in./°F.				See Figure 6.3.8.0