Aerospace Materials: Sample data

Aerospace material mechanical properties and design allowables at ambient, elevated, and cryogenic temperatures per MMPDS-11 (Metallic Materials Properties Development and Standardization). Covers primary structural alloys: aluminum (2024-T3, 7075-T6, 6061-T6, 2219-T87), titanium (Ti-6Al-4V), nickel superalloys (Inconel 718), and steels (300M, 4130, 4340).

Materials Sciencematerial_id: Sample data30 rows

material id	temp f	E Msi (Msi)	Ec Msi (Msi)	Fbru ksi (ksi)	Fbru ksi 2 (ksi)	Fbry ksi (ksi)	Fbry ksi 2 (ksi)	Fcy ksi (ksi)	Fcy ksi LT (ksi)	Fcy ksi ST (ksi)	Fsu ksi (ksi)	Ftu ksi (ksi)	Ftu ksi 45	Ftu ksi LT (ksi)	Ftu ksi ST (ksi)	Fty ksi (ksi)	Fty ksi LT (ksi)	Fty ksi ST (ksi)	G Msi (Msi)	basis	casting location	casting strength class	condition	density lb in3 (lb/in^3)	designation	elongation pct (%)	elongation pct LT (%)	elongation pct ST (%)	form	poisson ratio	specification	thickness range
15-5PH_BAR	70	28.5	—	—	—	—	—	—	—	—	—	190	—	—	—	170	—	—	—	—	—	—	—	—	—	10	—	—	—	—	AMS 5659	≤12.0 in dia
2014_FORGING_T6_LE1.000_A	70	10.5	10.8	91	123	73	90	59	—	56	40	65	—	—	—	56	—	—	4	A	—	—	T6a	0.101	—	6	—	—	Die forging	0.33	AMS 4133, AMS-A-22771, and AMS-QQ-A-367	<=1.000
2024_BAR_T4_4.001-4.500_S	70	10.5	10.7	93	118	59	67	33	—	—	37	62	—	54	—	42	39	—	4	S	—	—	T4a	0.1	—	10	—	—	Bar and rod; rolled, drawn, or cold-finished	0.33	AMS 4120 and AMS-QQ-A-225/6	4.001-4.500c
2024_PLATE_T851_0.250-0.499_B	70	—	—	103	133	89	105	60	61	—	39	68	—	68	—	60	60	—	—	B	—	—	T851	0.1	—	—	5	—	Plate	—	AMS-QQ-A-250/4	0.250-0.499
2124_PLATE_T851_3.001-4.000_B	70	10.4	10.9	99	128	85	99	59	60	61	39	67	—	67	63	60	60	57	4	B	—	—	T851	0.1	—	—	—	—	Plate	0.33	AMS 4101 and AMS-QQ-A-250/29	3.001-4.000
2297_PLATE_T87_4.001-5.000_A	70	11.3	—	97	126	84	98	—	—	—	—	61	59	61	58	56	56	52	—	A	—	—	T87	0.096	—	5	4	1.5	Plate	—	AMS 4330	4.001-5.000
5083_SHEET_O_3.001-4.000_S	70	10.2	10.4	—	—	—	—	—	—	—	—	38	—	—	—	16	—	—	3.85	S	—	—	O	0.096	—	16	—	—	Sheet and plate	0.33	AMS 4056 and AMS-QQ-A-250/6	3.001-4.000
6061_BAR_UNK_ANY_S_T3_6_2_0d_C3	70	9.9	10.1	—	—	—	—	—	—	—	—	30	—	—	—	14	—	—	3.8	S	—	—	—	0.098	—	18	—	—	Bar and Rod; Rolled, Drawn, or Cold-Finished	0.33	—	—
7040_PLATE_T7451_4.001-5.000_B	70	10.4	10.6	115	147	97	119	62	67	66	46	72	—	73	70	64	65	61	3.9	B	—	—	T7451	0.102	—	—	—	—	Plate	0.33	AMS 4211	4.001-5.000
7050_EXTRUSION_T76511_LE0.499_A	70	10.3	10.7	113	147	94	109	68	70	—	42	77	—	76	—	68	67	—	3.9	A	—	—	T76511	0.102	—	7	—	—	Extrusion	0.33	AMS 4340	<=0.499
7055_EXTRUSION_T76511_LE0.249_A	70	10.4	10.8	122	160	105	124	84	86	—	46	89	—	83	—	85	79	—	3.9	A	—	—	T76511	0.103	—	7	—	—	Extrusion	0.33	AMS 4336	<=0.249
7075_EXTRUSION_T73A_3.000-4.499_B_T3_7_6_0g2_C14	70	10.4	10.7	98	128	76	91	60	51	—	38	70	—	60	—	60	48	—	4	B	—	—	T73a, T73510, T73511	0.101	—	—	—	—	Extrusion (rod, bars, and shapes)	0.33	AMS-QQ-A-200/11	3.000-4.499
7075_FORGING_T73A_LE1.000_A	70	10	10.4	96	125	78	90	58	—	55	39	66	—	—	62	56	—	53	3.8	A	—	—	T73a,b	0.101	—	7	—	3	Die forging	0.33	AMS 4141, AMS-A-22771, and AMS-QQ-A-367	<=1.000
7075_SHEET_T6_AND_T62_0.012-0.039_A	70	10.3	10.6	118	152	100	117	68	74	—	46	76	—	76	—	69	67	—	3.9	A	—	—	T6 and T62a	0.101	—	—	7	—	Sheet	0.33	AMS 4045 and AMS-QQ-A-250/12	0.012-0.039
7175_FORGING_T74_ANY_S_T3_7_8_0c1_C3	70	10.2	10.6	104	136	80	95	61	61	60	43	71	—	70	68	61	58	57	3.9	S	—	—	T74	0.101	—	9	5	4	Hand forging	0.33	AMS 4149 and AMS-A-22771	—
A356_0_CASTING_T6_ANY_S_SC3	70	10.4	10.5	77	96	54	63	34	—	—	28	45	—	—	—	34	—	—	3.9	S	Designated area	3	T6	0.097	—	3	—	—	Casting	0.33	AMS-A-21180	—
C355_0_CASTING_UNK_ANY_S_SC11	70	10.1	10.3	86	60	63	44	30	—	—	23	37	—	—	—	30	—	—	3.85	S	T6	11	—	0.098	—	1	—	—	Casting	0.33	AMS-A-21180	—
CH2_250_MARAGING_STEEL_BAR_MARAGED_AT_900_F_4_000_S_2_5_1_0_B_C4	70	—	28.2	—	—	—	—	—	—	—	—	255	—	—	—	—	—	—	—	S	—	—	Maraged at 900(F	0.286	—	—	—	—	Bar	0.31	AMS 6512	<4.000
CH2_AISI_4135_TUBING_QUENCHED_AND_TEMPEREDA_0_8_S_2_3_1_0_C4_C1	70	29	29	194	251	146	175	109	—	—	75	125	—	—	—	100	—	—	11	S	—	—	Quenched and tempereda	0.283	AISI 4135	—	—	—	Tubing	0.32	AMS-T-6735	0.8
CH2_LOW_ALLOY_STEELS_BAR_FORGING_TUBING_QUENCHED_AND_TEMPEREDB_NA_S_2_3_1_0_F1_C2	70	29	29	297	385	267	294	193	—	—	132	220	—	—	—	185	—	—	11	S	—	—	Quenched and temperedb	0.283	—	10	5	—	Bar, forging, tubing	0.32	—	—
CLAD_2024_SHEET_T351_0.500-1.000_A	70	10.2	10.4	92	113	69	82	37	42	—	36	61	—	61	—	45	40	—	—	A	—	—	T351	0.1	—	—	8	—	Flat sheet and plate	0.33	AMS-QQ-A-250/5	0.500-1.000a
CLAD_2024_SHEET_T861_0.500_S	70	10.2	10.4	104	134	88	104	61	64	—	38	67	—	67	—	61	61	—	—	S	—	—	T861a	0.1	—	—	4	—	Flat sheet and plate	0.33	AMS-QQ-A-250/5	0.500b
CLAD_7075_SHEET_T6_AND_T62_0.008-0.011_S	70	10.3	10.2	—	—	—	—	—	—	—	—	—	—	68	—	—	58	—	—	S	—	—	T6 and T62	0.101	—	—	5	—	Sheet	0.33	AMS-QQ-A-250/13	0.008-0.011
HAYNES_230_BAR_ANN2250_2.001_TO_3.000_B	70	—	—	—	—	—	—	—	—	—	—	115	—	—	—	51	—	—	—	B	—	—	2250 Anneal	0.324	—	46	—	—	Bar	—	AMS 5891	2.001 to 3.000
INCONEL_625_SHEET_PLATE_ANN_0.141-0.062_0.063-0.109_0_B_T6_3_3_0b_C6	70	29.8	29.8	212	276	94	117	63	64	—	83	125	—	126	—	60	61	—	11.8	B	—	—	Annealed	0.305	—	—	—	—	Sheet and plate	0.28	AMS 5599	0.141-0.062 0.063-0.109 0.110-0.140 0.187
MG-AZ31B_FORGING_UNK_ANY_S	70	6.5	6.5	—	—	—	—	—	—	—	—	34	—	—	—	19	—	—	2.4	S	—	—	—	0.0639	—	6	—	—	Forging	0.35	ASTM B 91	—
MG-ZK60A_EXTRUSION_TUBE_T5_LE3.000IN.O.D._0.028_S	70	6.5	6.5	—	—	—	—	26	—	—	—	46	—	—	—	38	—	—	2.4	S	—	—	T5	0.0659	—	4	—	—	Extruded tube	0.35	AMS 4352	<=3.000 in. O.D.; 0.028-0.250 wall
TI-5AL-2.5SN_EXTRUSION_ANN_0.188-1.000_S	70	15.5	15.5	—	—	—	—	—	—	—	—	120	—	—	—	115	—	—	—	S	—	—	Annealed	0.162	—	10	—	—	Extruded bars and shapes	—	AMS-T-81556, Comp. A-1	0.188-1.000
TI-6AL-4V_BAR_UNK_ANY_B_T5_4_1_0c1_C5	70	16.9	17.2	209	262	186	215	135	—	—	86	140	—	143	—	131	132	—	6.2	B	—	—	—	0.16	—	—	—	—	Bar	0.31	—	—
TI-6AL-6V-2SN_BAR_ANN_1.501-....1.5003.000_B_T5_4_2_0c_C2	70	16	16.4	—	—	—	—	—	—	—	—	150	—	152	—	138	141	—	6.2	B	—	—	Air-cool annealeda	0.164	—	—	—	—	Bar	0.31	AMS 4978	1.501-. . . . 1.500 3.000

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Aerospace Materials: Sample data

Materials Sciencematerial_id: Sample data30 rows

material id	temp f	E Msi (Msi)	Ec Msi (Msi)	Fbru ksi (ksi)	Fbru ksi 2 (ksi)	Fbry ksi (ksi)	Fbry ksi 2 (ksi)	Fcy ksi (ksi)	Fcy ksi LT (ksi)	Fcy ksi ST (ksi)	Fsu ksi (ksi)	Ftu ksi (ksi)	Ftu ksi 45	Ftu ksi LT (ksi)	Ftu ksi ST (ksi)	Fty ksi (ksi)	Fty ksi LT (ksi)	Fty ksi ST (ksi)	G Msi (Msi)	basis	casting location	casting strength class	condition	density lb in3 (lb/in^3)	designation	elongation pct (%)	elongation pct LT (%)	elongation pct ST (%)	form	poisson ratio	specification	thickness range
15-5PH_BAR	70	28.5	—	—	—	—	—	—	—	—	—	190	—	—	—	170	—	—	—	—	—	—	—	—	—	10	—	—	—	—	AMS 5659	≤12.0 in dia
2014_FORGING_T6_LE1.000_A	70	10.5	10.8	91	123	73	90	59	—	56	40	65	—	—	—	56	—	—	4	A	—	—	T6a	0.101	—	6	—	—	Die forging	0.33	AMS 4133, AMS-A-22771, and AMS-QQ-A-367	<=1.000
2024_BAR_T4_4.001-4.500_S	70	10.5	10.7	93	118	59	67	33	—	—	37	62	—	54	—	42	39	—	4	S	—	—	T4a	0.1	—	10	—	—	Bar and rod; rolled, drawn, or cold-finished	0.33	AMS 4120 and AMS-QQ-A-225/6	4.001-4.500c
2024_PLATE_T851_0.250-0.499_B	70	—	—	103	133	89	105	60	61	—	39	68	—	68	—	60	60	—	—	B	—	—	T851	0.1	—	—	5	—	Plate	—	AMS-QQ-A-250/4	0.250-0.499
2124_PLATE_T851_3.001-4.000_B	70	10.4	10.9	99	128	85	99	59	60	61	39	67	—	67	63	60	60	57	4	B	—	—	T851	0.1	—	—	—	—	Plate	0.33	AMS 4101 and AMS-QQ-A-250/29	3.001-4.000
2297_PLATE_T87_4.001-5.000_A	70	11.3	—	97	126	84	98	—	—	—	—	61	59	61	58	56	56	52	—	A	—	—	T87	0.096	—	5	4	1.5	Plate	—	AMS 4330	4.001-5.000
5083_SHEET_O_3.001-4.000_S	70	10.2	10.4	—	—	—	—	—	—	—	—	38	—	—	—	16	—	—	3.85	S	—	—	O	0.096	—	16	—	—	Sheet and plate	0.33	AMS 4056 and AMS-QQ-A-250/6	3.001-4.000
6061_BAR_UNK_ANY_S_T3_6_2_0d_C3	70	9.9	10.1	—	—	—	—	—	—	—	—	30	—	—	—	14	—	—	3.8	S	—	—	—	0.098	—	18	—	—	Bar and Rod; Rolled, Drawn, or Cold-Finished	0.33	—	—
7040_PLATE_T7451_4.001-5.000_B	70	10.4	10.6	115	147	97	119	62	67	66	46	72	—	73	70	64	65	61	3.9	B	—	—	T7451	0.102	—	—	—	—	Plate	0.33	AMS 4211	4.001-5.000
7050_EXTRUSION_T76511_LE0.499_A	70	10.3	10.7	113	147	94	109	68	70	—	42	77	—	76	—	68	67	—	3.9	A	—	—	T76511	0.102	—	7	—	—	Extrusion	0.33	AMS 4340	<=0.499
7055_EXTRUSION_T76511_LE0.249_A	70	10.4	10.8	122	160	105	124	84	86	—	46	89	—	83	—	85	79	—	3.9	A	—	—	T76511	0.103	—	7	—	—	Extrusion	0.33	AMS 4336	<=0.249
7075_EXTRUSION_T73A_3.000-4.499_B_T3_7_6_0g2_C14	70	10.4	10.7	98	128	76	91	60	51	—	38	70	—	60	—	60	48	—	4	B	—	—	T73a, T73510, T73511	0.101	—	—	—	—	Extrusion (rod, bars, and shapes)	0.33	AMS-QQ-A-200/11	3.000-4.499
7075_FORGING_T73A_LE1.000_A	70	10	10.4	96	125	78	90	58	—	55	39	66	—	—	62	56	—	53	3.8	A	—	—	T73a,b	0.101	—	7	—	3	Die forging	0.33	AMS 4141, AMS-A-22771, and AMS-QQ-A-367	<=1.000
7075_SHEET_T6_AND_T62_0.012-0.039_A	70	10.3	10.6	118	152	100	117	68	74	—	46	76	—	76	—	69	67	—	3.9	A	—	—	T6 and T62a	0.101	—	—	7	—	Sheet	0.33	AMS 4045 and AMS-QQ-A-250/12	0.012-0.039
7175_FORGING_T74_ANY_S_T3_7_8_0c1_C3	70	10.2	10.6	104	136	80	95	61	61	60	43	71	—	70	68	61	58	57	3.9	S	—	—	T74	0.101	—	9	5	4	Hand forging	0.33	AMS 4149 and AMS-A-22771	—
A356_0_CASTING_T6_ANY_S_SC3	70	10.4	10.5	77	96	54	63	34	—	—	28	45	—	—	—	34	—	—	3.9	S	Designated area	3	T6	0.097	—	3	—	—	Casting	0.33	AMS-A-21180	—
C355_0_CASTING_UNK_ANY_S_SC11	70	10.1	10.3	86	60	63	44	30	—	—	23	37	—	—	—	30	—	—	3.85	S	T6	11	—	0.098	—	1	—	—	Casting	0.33	AMS-A-21180	—
CH2_250_MARAGING_STEEL_BAR_MARAGED_AT_900_F_4_000_S_2_5_1_0_B_C4	70	—	28.2	—	—	—	—	—	—	—	—	255	—	—	—	—	—	—	—	S	—	—	Maraged at 900(F	0.286	—	—	—	—	Bar	0.31	AMS 6512	<4.000
CH2_AISI_4135_TUBING_QUENCHED_AND_TEMPEREDA_0_8_S_2_3_1_0_C4_C1	70	29	29	194	251	146	175	109	—	—	75	125	—	—	—	100	—	—	11	S	—	—	Quenched and tempereda	0.283	AISI 4135	—	—	—	Tubing	0.32	AMS-T-6735	0.8
CH2_LOW_ALLOY_STEELS_BAR_FORGING_TUBING_QUENCHED_AND_TEMPEREDB_NA_S_2_3_1_0_F1_C2	70	29	29	297	385	267	294	193	—	—	132	220	—	—	—	185	—	—	11	S	—	—	Quenched and temperedb	0.283	—	10	5	—	Bar, forging, tubing	0.32	—	—
CLAD_2024_SHEET_T351_0.500-1.000_A	70	10.2	10.4	92	113	69	82	37	42	—	36	61	—	61	—	45	40	—	—	A	—	—	T351	0.1	—	—	8	—	Flat sheet and plate	0.33	AMS-QQ-A-250/5	0.500-1.000a
CLAD_2024_SHEET_T861_0.500_S	70	10.2	10.4	104	134	88	104	61	64	—	38	67	—	67	—	61	61	—	—	S	—	—	T861a	0.1	—	—	4	—	Flat sheet and plate	0.33	AMS-QQ-A-250/5	0.500b
CLAD_7075_SHEET_T6_AND_T62_0.008-0.011_S	70	10.3	10.2	—	—	—	—	—	—	—	—	—	—	68	—	—	58	—	—	S	—	—	T6 and T62	0.101	—	—	5	—	Sheet	0.33	AMS-QQ-A-250/13	0.008-0.011
HAYNES_230_BAR_ANN2250_2.001_TO_3.000_B	70	—	—	—	—	—	—	—	—	—	—	115	—	—	—	51	—	—	—	B	—	—	2250 Anneal	0.324	—	46	—	—	Bar	—	AMS 5891	2.001 to 3.000
INCONEL_625_SHEET_PLATE_ANN_0.141-0.062_0.063-0.109_0_B_T6_3_3_0b_C6	70	29.8	29.8	212	276	94	117	63	64	—	83	125	—	126	—	60	61	—	11.8	B	—	—	Annealed	0.305	—	—	—	—	Sheet and plate	0.28	AMS 5599	0.141-0.062 0.063-0.109 0.110-0.140 0.187
MG-AZ31B_FORGING_UNK_ANY_S	70	6.5	6.5	—	—	—	—	—	—	—	—	34	—	—	—	19	—	—	2.4	S	—	—	—	0.0639	—	6	—	—	Forging	0.35	ASTM B 91	—
MG-ZK60A_EXTRUSION_TUBE_T5_LE3.000IN.O.D._0.028_S	70	6.5	6.5	—	—	—	—	26	—	—	—	46	—	—	—	38	—	—	2.4	S	—	—	T5	0.0659	—	4	—	—	Extruded tube	0.35	AMS 4352	<=3.000 in. O.D.; 0.028-0.250 wall
TI-5AL-2.5SN_EXTRUSION_ANN_0.188-1.000_S	70	15.5	15.5	—	—	—	—	—	—	—	—	120	—	—	—	115	—	—	—	S	—	—	Annealed	0.162	—	10	—	—	Extruded bars and shapes	—	AMS-T-81556, Comp. A-1	0.188-1.000
TI-6AL-4V_BAR_UNK_ANY_B_T5_4_1_0c1_C5	70	16.9	17.2	209	262	186	215	135	—	—	86	140	—	143	—	131	132	—	6.2	B	—	—	—	0.16	—	—	—	—	Bar	0.31	—	—
TI-6AL-6V-2SN_BAR_ANN_1.501-....1.5003.000_B_T5_4_2_0c_C2	70	16	16.4	—	—	—	—	—	—	—	—	150	—	152	—	138	141	—	6.2	B	—	—	Air-cool annealeda	0.164	—	—	—	—	Bar	0.31	AMS 4978	1.501-. . . . 1.500 3.000

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Aerospace Materials: Sample data

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Aerospace Materials: Sample data