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Inconel 600-Annealed Bar and rod: MIL-HDBK-5J Design Allowables

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Material class	Heat-Resistant
Alloy / temper / form	Inconel 600 / Annealed / Bar and rod
Specifications	ASTM B166
Handbook	MIL-HDBK-5J, 31 January 2003, section 6.3.2.0, Table 6.3.2.0(d) (pdf page 30 of the chapter file)
Dimension bands	1
Density	0.304 lb/in3

Design Mechanical and Physical Properties (room temperature)

As printed in the handbook table. Bases: A and B are statistical minimums (99 % and 90 % probability at 95 % confidence), S the specification minimum. Grain directions: L longitudinal, LT long transverse, ST short transverse.

Dimension band		all
Specification		ASTM B166
Basis		S
F_tu, ksi	L	80
F_ty, ksi	L	35
F_cy, ksi	L	35
F_su, ksi	L	51
F_bru (e/D = 2.0), ksi	L	152
e, %	L	30
E, Msi		30
E_c, Msi		30
G, Msi		11
ν		0.29
ρ, lb/in3		0.304

Effect of Temperature

Percent of the room-temperature value against temperature, digitized from the handbook figures (the shortest exposure of each figure, every 10 °F). Strength curves give the allowable at temperature; "after exposure" curves give the room-temperature property after a soak at that temperature.

Strength allowables at temperature, percent of room temperature

Moduli at temperature

°F	F_tu	F_ty	F_cy	F_su	F_bru
100	99	99	98.4	98.4	99.1
200	97	97	94	98.3	98.6
300	94.1	94.1	90.4	97.6	98.1
400	91.4	91.4	89.7	97	97.5
500	89.6	87.9	89.1	96.2	96.6
600	85.9	85.9	87.5	95.7	95.9
700	84.6	82	84.9	95.1	94.8
800	82	79.3	81.7	93.5	94.3
1000	77.1	73.2		86.5	88.9
1200	65.4	65.4		75.5	70.8

Factors in percent of the room-temperature allowable.

Other Inconel 600 Tables

Inconel 600-Annealed Forging (Table 6.3.2.0(b))
Inconel 600-Annealed Sheet, strip, and plate (Table 6.3.2.0(b))
Inconel 600-Cold drawn Tubing (Table 6.3.2.0(b))
Inconel 600-Cold-worked Round (Table 6.3.2.0(c))
Inconel 600-Cold-worked Square, hexagon, and rectangle (Table 6.3.2.0(c))
Inconel 600-Hot-worked Round (Table 6.3.2.0(d))
Inconel 600-Hot-worked Square, / hexagon, and / rectangle (Table 6.3.2.0(d))

Source and Use

U.S. Department of Defense (2003). Metallic Materials and Elements for Aerospace Vehicle Structures. MIL-HDBK-5J, 31 January 2003 (public domain). The values are the handbook's design allowables as extracted from the chapter tables; check the printed table before use in a certified analysis, and note that MIL-HDBK-5J was superseded by MMPDS, whose later editions may differ. No warranty is given.