Inconel 600 Fasteners

Specifications

Plate: ASTM B168
Bar: ASTM B166

Physical Properties

Physical Constants

Density	lb/in³	0.306
Density	Mg/m³	8.47
Melting Range	°F	2470-2575
Melting Range	°C	1354-1413
Specific Heat	Btu/lb-°F	0.106
Specific Heat	J/kg-°C	444
Electrical Resistivity	ohm-circ mil/ft	620
Electrical Resistivity	μΩ-m	1.03
Curie Temperature	°F	-192
Curie Temperature	°C	-124
Permeability at 200 oersted	15.9 kA/m	1.010

Mechanical Properties

Thermal Properties

Temperature	Coefficient of Expansion^a	Electrical Resistivity	Thermal Conductivity	Specific Heat
°F	10^-6in/in•°F	ohm•circ•mil/ft	Btu•in/ft²•h•°F	Btu/lb•°F
-250	6.0	–	86	0.073
-200	6.3	–	89	0.079
-100	6.7	–	93	0.090
70	5.8	620	103	0.106
200	7.4	625	109	0.111
400	7.7	634	121	0.116
600	7.9	644	133	0.121
800	8.1	657	145	0.126
1000	8.4	680	158	0.132
1200	8.6	680	172	0.140
1400	8.9	680	186	0.145
1600	9.1	686	200	0.149
1800	9.3	698	–	–
2000	–	704	–	–
°C	μm/m•°C	μΩ•m	W/m•°C	J/kg•°C
-150	10.9	–	12.5	310
-100	11.7	–	13.1	352
-50	12.3	–	13.6	394
20	10.4	1.03	14.9	444
100	13.3	1.04	15.9	465
200	13.8	1.05	17.3	486
300	14.2	1.07	19.0	502
400	14.5	1.09	20.5	519
500	14.9	1.12	22.1	536
600	15.3	1.13	23.9	578
700	15.8	1.13	25.7	595
800	16.1	1.13	27.5	611
900	16.4	1.15	–	628

^aMean coefficient of linear expansion between 70°F (21°C) and temperature shown except that the room-temperature value was measured from -320°F (-196°C).

Modulus of Elasticity

Temperature	Young Modulus	Shear Modulus	Poisson’s Ratio
°F	10³ksi	10³ksi	Poisson’s Ratio
72	31.1	11.72	0.327
200	30.5	11.56	0.319
400	29.7	11.32	0.312
600	28.8	11.02	0.307
800	27.8	10.68	0.301
1000	26.7	10.29	0.297
1200	25.5	9.83	0.297
1400	24.3	9.24	0.315
1600	22.8	8.58	0.329
1800	21.0	7.85	0.338
°C	GPa	GPa	Poisson’s Ratio
22	214	80.8	0.324
100	210	79.6	0.319
200	205	78.0	0.314
300	199	76.2	0.306
400	193	74.2	0.301
500	187	71.9	0.300
600	180	69.2	0.301
700	172	65.9	0.305
800	164	62.1	0.320
900	154	57.9	0.330
1000	143	53.4	0.339

Emissivity

	Temperature, °F (°C)
	600 (315)	900 (480)	1200 (650)	1500 (815)	1800 (980)	2000 (1090)
Total Hemispherical Emissivity	0.69	0.72	0.76	0.79	0.82	–
Total Normal Emissivity As-Rolled and Oxidized^a	–	0.85	0.87	0.90	0.95	0.98
Sand-Blasted and Oxidized^b	–	0.86	0.90	0.93	0.96	0.97

^aOxidized by heating 13 min in air at 2000°F (1090°C). ^bOxidized by heating 15 min at 1500°F (815°C), 15 min at 1800°F (980°C), and 15 min at 2100°F (1150°C).

Tensile Properties

Typical Mechanical-Property Ranges^a

Form and Condition	Tensile Strength		Yield Strength (0.2% Offset)		Elongation, %	Hardness, Rockwell
Form and Condition	ksi	MPa	ksi	MPa	Elongation, %	Hardness, Rockwell
Rod and Bar
Cold-Drawn
Annealed	80-100	550-690	25-50	170-345	55-35	65-85B
As-Drawn	105-150	725-1035	80-125	550-860	30-10	90B-30C
Hot-Finished
Annealed	80-100	550-690	30-50	205-345	55-35	65-85B
Hot-Finished	85-120	585-830	35-90	240-620	50-30	75-95B
Plate
Hot-Rolled
Annealed	80-105	550-725	30-50	205-345	55-35	65-85B
As-Rolled	85-110	580-760	35-65	240-450	50-30	80-95B
Sheet
Cold-Rolled
Annealed	80-100	550-690	30-45	205-310	55-35	88B max.
Hard	120-150	830-1035	90-125	620-860	15-2	24C min.
Strip
Cold-Rolled
Annealed	80-100	550-690	30-45	205-310	55-35	84B max.
Spring Temper	145-170	1000-1170	120-160	830-1100	10-2	30C min.
Tube and Pipe
Hot-Finished
Hot-Finished	75-100	520-690	25-50	170-345	55-35	–
Annealed	75-100	520-690	25-50	170-345	55-35	–
Cold-Drawn
Annealed	80-100	550-690	25-50	170-345	55-35	88B max.
Wire^b
Cold-Drawn
Annealed	80-120	550-830	35-75	240-520	45-20	–
No. 1 Temper	105-135	725-930	70-105	480-725	35-15	–
Spring Temper	170-220	1170-1520	150-210	1035-1450	5-2	–

^aValues shown are composites for various product sizes and therefore are not suitable for specification purposes. ^bProperties shown are for sizes 0.0625- to 0.250-in. (1.6 to 6.4 mm) dia. Properties for other sizes may vary from these.

High-temperature tensile properties of cold-drawn bar

Room-Temperature Tensile Properties of Hot-Rolled Rod

Heat Treatment^a		Tensile Strength		Yield Strength (0.2% Offset)		Elongation, %	Reduction of Area, %	Hardness, Rb
°F/1 hr	°C/1 hr	ksi	MPa	ksi	MPa	Elongation, %	Reduction of Area, %	Hardness, Rb
As-rolled	As-rolled	97.5	672.3	44.5	306.8	46.0	68.0	86
1600	870	95.6	659.1	41.1	283.3	44.0	66.0	85
1700	925	95.6	659.1	41.0	282.7	45.0	46.5	84
1800	980	90.5	624.0	30.4	209.6	49.0	69.5	75
1900	1040	86.5	596.4	20.5	141.3	55.0	71.5	70
2000	1090	86.3	595.0	24.2	166.9	55.0	71.5	70
2100	1150	84.5	582.6	24.0	165.5	57.5	69.5	69

^aAir-cooled after all treatments.

Room-Temperature Properties of Forged^a Rod

Heat Treatment^b		Tensile Strength		Yield Strength (0.2% Offset)		Elongation, %	Hardness, Rb
°F/1 hr	°C/1 hr	ksi	MPa	ksi	MPa	Elongation, %	Hardness, Rb
As-forged	As-forged	99.0	682.6	58.0	399.9	35	91
1300	705	100.5	692.9	61.0	420.6	34	92
1400	760	97.5	672.3	57.0	393.0	31	89
1500	815	98.5	679.2	57.0	393.0	33	91
1600	870	102.0	703.3	62.0	427.5	32	93
1700	925	102.5	706.7	41.5	286.1	39	88

^a31% reduction, finished at 1600°F (870°C). ^bAir-cooled after all treatments.

Room-Temperature Properties of Hot-Rolled Plate

Heat Treatment^a		Tensile Strength		Yield Strength (0.2% Offset)		Elongation, %	Reduction of Area, %	Hardness, Rb
°F/1 hr	°C/1 hr	ksi	MPa	ksi	MPa	Elongation, %	Reduction of Area, %	Hardness, Rb
As-rolled	As-rolled	99.0	682.6	50.2	346.1	42.0	55.5	87
1600	870	98.0	675.7	48.0	331.0	40.0	55.0	87
1700	925	98.5	679.2	49.4	340.6	40.5	58.0	84
1800	980	92.7	639.2	28.9	199.3	49.0	63.0	75
1900	1040	91.0	627.4	27.5	189.6	51.0	65.0	73
2000	1090	89.8	619.2	26.7	184.1	52.5	66.5	72
2100	1150	84.5	582.6	23.5	162.0	58.0	65.0	68

^aAir-cooled after all treatments.

Room-Temperature Properties of Cold-Drawn Rod

Heat Treatment		Tensile Strength		Yield Strength (0.2% Offset)		Elongation, %	Reduction of Area, %	Hardness, Rockwell
°F/1 hr	°C/1 hr	ksi	MPa	ksi	MPa	Elongation, %	Reduction of Area, %	Hardness, Rockwell
As-drawn	As-drawn	123.5	851.5	118.5	817.1	16.0	55	28C
1200	650	134.0	923.9	113.0	779.4	20.0	51	23C
1300	705	148.0	1020.5	100.0	689.5	22.0	52	99B
1400	760	118.3	815.7	90.4	623.3	23.5	53	97B
1500	815	99.4	685.4	40.0	275.8	42.0	61	76B
1600	870	99.2	684.0	39.7	273.7	43.0	63	77B

Room-Temperature Properties of Cold-Drawn Tubing^a

Heat Treatment		Tensile Strength		Yield Strength (0.2% Offset)		Elongation, %	Hardness, Rockwell
°F/1 hr	°C/1 hr	ksi	MPa	ksi	MPa	Elongation, %	Hardness, Rockwell
As-drawn	As-drawn	144.0	992.9	132.8	915.7	8.0	34C
1200	650	143.5	989.4	124.0	855.0	17.5	32C
1300	705	131.5	906.7	108.2	746.0	18.0	30C
1400	760	103.0	710.2	41.5	286.1	41.0	88B
1500	815	100.3	691.6	39.7	273.7	42.0	83B
1600	870	100.5	692.9	40.5	279.2	43.0	83B

^a0.625-in. (15.9-mm) OD x 0.075-in. (1.9-mm) wall.

Low-temperature tensile properties of cold-drawn rod

Hot hardness of hot-rolled material.

High-temperature tensile properties of annealed, 1600°F (870°C)/1 hr, hot-rolled rod.

High-temperature tensile properties of annealed, 1600°F (870°C)/1 hr, hot-rolled plate.

Impact Strength and Ductility

Impact Strength (Charpy Keyhole) of Plate

Orientation	Temperature		Impact Strength
Orientation	°F	°C	ft–lb	J
Transverse	70	21	63.5	86.1
	-110	-79	65.5	88.8
	-320	-196	60.8	82.4
Longitudinal	70	21	61.7	83.7
	-110	-79	67.0	90.8
	-320	-196	61.3	83.1

^aValues are the average of three tests.

Room-Temperature Impact Strength of Rod

	Impact Strength
Condition	Izod Notch		Charpy U-Notch
Condition	ft•lb	J	ft•lb	J
Cold-Drawn	>120	>163	230	312
Cold-Drawn, Annealed	70-100	95-136	151	205
Hot-Rolled	>120	>163	230	312
Hot-Rolled, Annealed	100-120	136-163	–	–

Impact Strength (Charpy V-Notch) at Elevated Temperatures

Temperature		Impact Strength
Temperature		Annealed		Cold-Drawn
°F	°C	ft•lb	J	ft•lb	J
70	21	180	244	114	155
800	430	187	254	84	114
1000	540	160	217	86	116
1200	650	160	217	104	141
1400	760	154	209	163	221

Shear Properties

Shear Strength of Cold-Rolled Sheet and Strip

Temper	Shear Strength		Tensile Strength		Hardness, Rockwell
Temper	ksi	MPa	ksi	MPa	Hardness, Rockwell
Annealed	60.8	419.2	85.0	586.1	71 B
Half-Hard	66.3	456.8	98.8	681.2	98 B
Full-Hard	82.4	568.1	152.2	1049.5	31 C

Fatigue Strength

Room-Temperature Fatigue Strength

Condition	Fatigue Strength (10⁸Cycles)		Tensile Strength		Average Endurance Ratio
Condition	ksi	MPa	ksi	MPa	Average Endurance Ratio
Annealed	39.0	268.9	85-114	586.1-786.0	0.39
Hot-Rolled	40.5	279.2	87-129.5	600.0-892.9	0.41
Cold-Drawn	45.0	310.3	112.5-202	775.7-1393	0.32
Cold-Drawn, Stress-Equalized^a	52.5	361.0	121.5-173	837.7-1193	0.34

^a525°F (274°C) 3 hr.

Low-Cycle^aFatigue of Annealed Rod

Temperature		Reversed Strain, %, to Cause Failure In
°F	°C	10,000 Cycles	50,000 Cycles	100,000 Cycles
75	24	±0.36	±0.21	±0.18
200	93	±0.43	±0.21	±0.18
400	204	±0.58	±0.26	±0.20
600	316	±0.52	±0.23	±0.18

^a550 cycles/hr.

Room-Temperature Low-Cycle^aFatigue of Forgings

Material Condition	Reversed Strain, %, to Cause Failure In
Material Condition	1000 Cycles	10,000 Cycles	50,000 Cycles
As-Forged	±1.25	±0.50	±0.35
Stress-Relieved 1400°F (760°C)/4 hr	±1.25	±0.47	±0.27

^a675 cycles/hr.

Rotating-beam fatigue strength (10⁸ cycles) of cold-drawn, annealed rod at elevated temperatures

Low-cycle fatigue strength of forgings in four conditions

Rotating-beam fatigue strength of forgings in four conditions

Creep and Rupture Properties

Room-Temperature Properties of Material Forged by Four Different Practices

Condition	Tensile Strength		Yield Strength (0.2% Offset)		Elongation, %	Reduction of Area, %	Hardness, Rb	Grain Size
Condition	ksi	MPa	ksi	MPa	Elongation, %	Reduction of Area, %	Hardness, Rb	in.	mm
Fine Grain, Hard	103.0	710	64.6	445	35.0	60.3	93.0	0.0028^a	0.0711
Fine Grain, Soft	92.0	634	40.5	279	44.0	61.0	83.5	0.0028^a	0.0711
Coarse Grain, Hard	102.0	703	74.7	515	28.0	56.7	94.0	0.006-0.02^b	0.152-0.51^b
Coarse Grain, Soft	86.4	596	32.7	225	61.7	50.7	76.5	0.006-0.02^b	0.152-0.51^b

^aAverage diameter. ^bMixed grain size.

Creep Properties

Temperature		Stress for a Secondary Creep Rate of:
		0.01%/1000 hr				0.1%/1000 hr
		Cold-Drawn, Annealed^a		Solution-Treated^b		Cold-Drawn, Annealed^a		Solution-Treated^b
°F	°C	ksi	MPa	ksi	MPa	ksi	MPa	ksi	MPa
800	427	30.00	206.9	–	–	40.00	275.8	–	–
900	482	18.00	124.1	–	–	28.00	193.1	–	–
1000	538	6.10	42.1	–	–	12.50	86.2	–	–
1100	593	3.40	23.4	–	–	6.80	46.9	–	–
1200	649	2.20	15.2	–	–	–	–	–	–
1300	704	1.40	9.7	4.00	27.6	–	–	5.00	34.5
1400	760	0.97	6.7	3.50	24.1	–	–	–	–
1500	816	0.66	4.6	2.80	19.3	–	–	3.20	22.1
1600	871	0.45	3.1	1.70	11.7	0.88	6.1	2.00	13.8
1700	927	–	–	0.81	5.6	–	–	1.10	7.6
1800	982	0.34	2.3	0.35	2.4	0.56	3.9	0.56	3.9
2000	1093	0.16	1.1	0.16	1.1	0.27	1.9	0.27	1.9
2100	1149	0.10	0.7	0.10	0.7	0.17	1.2	0.17	1.2

^a1750°F (954°C)/3 hr, A.C ^b2050°F (1121°C)/2 hr, A.C.

Creep rates of plate in the as-hot-rolled condition (1000°F-1300°F (538°C-704°C) data) and in the hot-rolled and solution-annealed (2050°F (1121°C)/2 h) condition (1500°F-2000°F (816°C-1093°C) data).

Rupture Properties

Temperature		Stress^ato Produce Rupture in
Temperature		10 hr		100 hr		1,000 hr		10,000 hr		100,000 hr
°F	°C	ksi	MPa	ksi	MPa	ksi	MPa	ksi	MPa	ksi	MPa
Cold-Drawn, Annealed at 1750°F (954°C)/3 hr, A.C.
100	538	74.00	510.2	50.00	344.8	34.00	234.4	23.00	158.6	16.00	110.3
1200	649	34.00	234.4	23.00	158.6	14.50	100.0	9.40	64.8	6.00	41.4
1400	760	13.00	89.6	8.40	57.9	5.60	38.6	3.60	24.8	2.40	16.5
1600	871	7.50	51.7	4.80	33.1	3.00	20.7	1.90	13.1	1.20	8.3
1800	982	4.40	30.3	2.80	19.3	1.80	12.4	1.15	7.9	0.73	5.0
2000	1093	2.10	14.5	1.40	9.7	0.92	6.3	0.62	4.3	0.42	2.9
Hot-Rolled, Annealed at 1650°F (899°C)/2 hr
1350	732	20.00	137.9	13.50	93.1	9.20	63.4	6.40	44.1	4.40	30.3
1600	871	8.10	55.8	5.30	36.5	3.50	24.1	2.20	15.2	1.50	10.3
1800	982	4.40	30.3	2.80	19.3	1.80	12.4	1.15	7.9	0.73	5.0
2000	1093	2.10	14.5	1.40	9.7	0.92	6.3	0.62	4.3	0.40	2.8
Solution-Treated at 2050°F (1121°C)/2 hr, A.C.
1350	732	19.00	131.0	14.00	96.5	9.80	67.6	7.00	48.3	5.00	34.5
1500	816	11.50	79.3	8.00	55.2	5.60	38.6	4.00	27.6	2.80	19.3
1600	871	8.00	55.2	5.30	36.5	3.50	24.1	2.30	15.9	1.50	10.3
1800	982	4.40	30.3	2.80	19.3	1.80	12.4	1.15	7.9	0.73	5.0
2000	1093	2.10	14.5	1.40	9.7	0.92	6.3	0.62	4.3	0.40	2.8
2100	1149	1.60	11.0	1.10	7.6	–	–	–	–	–	–

^aValues in bold are extrapolated.

Rupture life of plate in the as-hot-rolled condition (1000°F-1300°F (538°C-704°C) data) and in the hot-rolled and solutionannealed (2050°F (1121°C)/2h) condition (1350°F-2000°F (732°C-1093°C) data)

Room-Temperature Mechanical Properties of Creep-Test Specimens^a

Conditions of Creep Test					Room-Temperature Properties
Temperature		Stress		Duration, hr	Tensile Strength		Yield Strength (0.2% Offset)		Elongation, %	Reduction of Area, %	Hardness, R_b
°F	°C	ksi	MPa	Duration, hr	ksi	MPa	ksi	MPa	Elongation, %	Reduction of Area, %	Hardness, R_b
80	27	0	0	0	97.30	670.9	35.60	245.5	41	66	79
800	427	50.00	344.8	1945	101.00	696.4	60.30	415.8	40	65	90
800	427	30.00	206.9	1874	96.80	667.4	40.80	281.3	43	64	80
900	482	40.00	275.8	1508	98.00	675.7	57.80	398.5	46	66	90
900	482	30.00	206.9	1900	96.50	665.4	39.40	271.7	44	67	80
900	482	20.00	137.9	1969	96.30	664.0	39.40	271.7	45	65	80
1000	538	20.00	137.9	264	96.60	666.1	40.80	281.3	44	64	80
1000	538	15.00	103.4	2159	95.50	658.5	36.60	252.4	43	65	80
1000	538	10.00	69.0	1942	93.70	646.1	36.70	253.0	44	65	80
1100	593	10.00	69.0	576	98.20	677.1	40.40	278.6	43	65	80
1100	593	5.00	34.5	1602	94.50	651.6	35.10	242.0	43	65	80
1100	593	2.50	17.2	2205	96.60	666.1	35.80	246.8	42	65	80

^aCold-drawn rod, annealed 1750°F (954°C)/3 hr, A.C.

Room-Temperature Impact Strength of Creep-Test Specimens^a

Conditions of Creep Test					Room-Temperature Properties
Temperature		Stress		Duration, hr	ModifiedIzod Impact Strength		Hardness, Rb
°F	°C	ksi	MPa	Duration, hr	ft•lb	J	Hardness, Rb
80	27	0	0	0	94-95	127-129	79
800	427	40	275.8	1861	76-78	103-106	80
900	482	30	206.9	1617	90-96	122-130	80
900	482	15	103.4	1876	97-98	132-133	80
1000	538	20	137.9	582	85	115	80
1000	538	5	34.5	2022	87-89	118-121	80
1100	593	5	34.5	1850	101-109	137-148	80

^aCold-drawn rod, annealed 1750°F (954°C)/3 hr, A.C.

Corrosion Resistance

Gas Carburization Tests (100 h) in Hydrogen/2% Methane

Alloy	Weight Gain, mg/cm²
Alloy	1700°F (925°C)	2000°F (1095°C)^a
INCONEL alloy 600	2.66	12.30
INCONEL alloy 601	2.72	16.18
INCOLOY alloy 800HT	4.94	21.58
Type 330 Stainless Steel	6.42	24.00

^aAtmosphere also contained 5% argon.

Results of cyclic oxidation tests at 1800°F (980°C). Cycles were 15 minutes of heating and 5 minutes of cooling in air

Hot and Cold Forming

Effect of Cold Work on Recrystallization Temperature of Cold-Rolled, Fine-Grain Sheet

Cold Reduction, %	Temperature Required for Recrystallization in
	15 min		30 min		60 min		120 min
	°F	°C	°F	°C	°F	°C	°F	°C
5	1775	968	1750	954	1700	927	1700	927
10	1650	899	1600	871	1550	843	1550	843
20	1525	829	1475	802	1425	774	1425	774
50	1350	732	1325	718	1275	691	1275	691
80	1250	677	1225	663	1200	649	1200	649

Welding

Thermal Expansion of Weld Metals

Material	Mean Linear Expansion^a
	10-6 in/in-°F					μm/m-°C
	200°F	300°F	400°F	500°F	600°F	93°C	149°C	204°C	260°C	316°C
INCONEL alloy 600	7.4	–	7.7	–	7.9	13.3	–	13.9	–	14.2
INCONEL Filler Metal 82	6.7	7.2	7.6	7.8	7.9	12.1	13.0	13.7	14.0	14.2
INCONEL Welding Electrode 182	7.6	8.0	8.1	8.2	8.3	13.7	14.4	14.6	14.8	14.9

^aFrom 70°F (21°C) to temperature shown.

Impact Strength (Charpy Keyhole) of INCONEL Welding Electrode 182 Deposited Weld Metal

Temperature		Impact Strength^a
°F	°C	ft•lb	J
70	21	48.8	66.2
-110	-79	46.5	63.0
-320	-196	42.2	57.2

^aValues at 70°F (21°C) and -110°F (-79°C) are the average of three tests; value at -320°F (-196°C) is the average of two tests.

Room-Temperature Tensile Properties of All-Weld-Metal Deposits

Welding Material	Tensile Strength		Yield Strength (0.2% Offset)		Elongation in 1.25 in (31.75 mm), %
Welding Material	ksi	MPa	ksi	MPa	Elongation in 1.25 in (31.75 mm), %
INCONEL Filler Metal 82^a	96.20	663.3	57.10	393.7	45
INCONEL Welding Electrode 182^a	92.40	637.1	55.10	379.9	44
INCONEL Welding Electrode 182^b	98.80	681.2	61.40	423.4	40

^a0.505-in. (12.83 mm)-dia. specimen. ^b0.252-in. (6.40-mm)-dia. specimen.

High-temperature tensile properties of welds made with INCONEL FIller Metal 82 (left) and INCONEL Welding Electrode 182 (right)

Rupture Strength of All-Weld-Metal Deposits

Welding Material	Temperature		Stress^ato Produce Rupture in
	Temperature		100 hr		1000 hr		10,000 hr
	°F	°C	ksi	MPa	ksi	MPa	ksi	MPa
INCONEL Filler Metal 82	1000	538	58.00	399.9	52.00	358.5	47.00	324.1
	1200	649	36.50	251.7	27.50	189.6	20.50	141.3
	1400	760	16.00	110.3	11.50	79.3	8.30	57.2
	1600	871	6.80	46.9	3.50	24.1	1.75	12.1
	1800	982	2.70	18.6	1.25	8.6	0.57	3.9
INCONEL Welding Electrode 182	1000	538	53.00	365.4	50.00	344.8	41.00	282.7
	1200	649	34.00	234.4	22.50	155.1	14.50	100.0
	1350	732	13.50	93.1	8.20	56.5	4.90	33.8
	1500	816	7.00	48.3	4.00	27.6	2.25	15.5
	1600	871	4.00	27.6	2.15	14.8	1.15	7.9
	1800	982	1.70	11.7	0.82	5.7	0.41	2.8
INCO-WELD A Electrode	1000	538	60.00	413.7	51.00	351.6	39.00	268.9
	1200	649	35.00	241.3	24.50	168.9	16.00	110.3
	1400	760	16.50	113.8	11.00	75.8	7.10	48.9
	1600	871	7.00	48.3	3.65	25.2	1.90	13.1
	1800	982	2.30	15.9	0.90	6.2	–	–

^aValues in bold are extrapolated.

Inconel 600

Inconel 600

Key

UNS N06600

Summary

Specifications & Technical Data

Specifications

Physical Properties

Physical Constants

Mechanical Properties

Thermal Properties

Modulus of Elasticity

Emissivity

Tensile Properties

Typical Mechanical-Property Rangesa

High-temperature tensile properties of cold-drawn bar

Room-Temperature Tensile Properties of Hot-Rolled Rod

Room-Temperature Properties of Forgeda Rod

Room-Temperature Properties of Hot-Rolled Plate

Room-Temperature Properties of Cold-Drawn Rod

Room-Temperature Properties of Cold-Drawn Tubinga

Low-temperature tensile properties of cold-drawn rod

Hot hardness of hot-rolled material.

High-temperature tensile properties of annealed, 1600°F (870°C)/1 hr, hot-rolled rod.

High-temperature tensile properties of annealed, 1600°F (870°C)/1 hr, hot-rolled plate.

Impact Strength and Ductility

Impact Strength (Charpy Keyhole) of Plate

Room-Temperature Impact Strength of Rod

Impact Strength (Charpy V-Notch) at Elevated Temperatures

Shear Properties

Shear Strength of Cold-Rolled Sheet and Strip

Fatigue Strength

Room-Temperature Fatigue Strength

Low-Cyclea Fatigue of Annealed Rod

Room-Temperature Low-Cyclea Fatigue of Forgings

Rotating-beam fatigue strength (108 cycles) of cold-drawn, annealed rod at elevated temperatures

Low-cycle fatigue strength of forgings in four conditions

Rotating-beam fatigue strength of forgings in four conditions

Creep and Rupture Properties

Room-Temperature Properties of Material Forged by Four Different Practices

Creep Properties

Creep rates of plate in the as-hot-rolled condition (1000°F-1300°F (538°C-704°C) data) and in the hot-rolled and solution-annealed (2050°F (1121°C)/2 h) condition (1500°F-2000°F (816°C-1093°C) data).

Rupture Properties

Rupture life of plate in the as-hot-rolled condition (1000°F-1300°F (538°C-704°C) data) and in the hot-rolled and solutionannealed (2050°F (1121°C)/2h) condition (1350°F-2000°F (732°C-1093°C) data)

Room-Temperature Mechanical Properties of Creep-Test Specimensa

Room-Temperature Impact Strength of Creep-Test Specimensa

Corrosion Resistance

Gas Carburization Tests (100 h) in Hydrogen/2% Methane

Results of cyclic oxidation tests at 1800°F (980°C). Cycles were 15 minutes of heating and 5 minutes of cooling in air

Hot and Cold Forming

Effect of Cold Work on Recrystallization Temperature of Cold-Rolled, Fine-Grain Sheet

Welding

Thermal Expansion of Weld Metals

Impact Strength (Charpy Keyhole) of INCONEL Welding Electrode 182 Deposited Weld Metal

Room-Temperature Tensile Properties of All-Weld-Metal Deposits

High-temperature tensile properties of welds made with INCONEL FIller Metal 82 (left) and INCONEL Welding Electrode 182 (right)

Rupture Strength of All-Weld-Metal Deposits

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