Aerospace Superior metals for higher-performance demand

We supply our clients high strength Aerospace metals and represent and distribute leading Aerospace production mills worldwide. Our aim is to provide metal solutions and support to our customers in alloy selection to match the exact needs of each and every product and project. The quality of the raw material is critical to success and we always strive to provide our clients with the best materials. We provide a broad range of alloys from Aluminum, Stainless and Alloy steel to Titanium, Beryllium Copper and heavy metals and more.

Typical Applications

Jet Engine Parts

Landing Gear

Aircraft Wings

Metals Used in This Industry

Stainless Steel Alloy 15-5Ph
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General Characteristics

15-5Ph is a precipitation hardening martensitic stainless-steel considered of being a compositional modification of 17-4 with minimal delta ferrite. A wide range of mechanical properties is available via simple aging within a 900-1150°F (482-621°C) temperature range. Vacuum arc re-melting provides low gas content, superior cleanliness and optimum transverse properties.

Typical applications include aircraft and missile structural components, gears, valves, fasteners, jet engine and nuclear reactor parts. It is favored over 17-4 when transverse properties are of concern.
Typical Chemical Composition

Weight % C Mn Si Cr Ni P S Cu Nb Fe

minimum — — — 14.00 3.50 — — 2.50 0.15 Remainder

maximum 0.07 1.00 1.00 15.50 5.50 0.04 0.03 4.50 0.45

Weight %	C	Mn	Si	Cr	Ni	P	S	Cu	Nb	Fe
minimum	—	—	—	14.00	3.50	—	—	2.50	0.15	Remainder
maximum	0.07	1.00	1.00	15.50	5.50	0.04	0.03	4.50	0.45

Physical Properties (Annealed condition)

Characteristics		English	Metric
Nominal density (68°F/20°C)		0.28 lbs/in³	7.80 g/cm³
Melting range		2560°F-2625°F	1400°C-1440°C
Specific heat (212 °F/100°C)		0.10 BTU/lb – °F	420 J/KG- °K
Coefficient of thermal expansion	32°F – 212°F 0°C – 100°C	6.0 micro in/in- °F	10.8 micro m/m- °K
Coefficient of thermal expansion	32°F – 600°F 0°C – 315°C	6.3 micro in/in- °F	11.4 micro m/m- °K
Thermal conductivity	100°C	10.3 BTU/ft- hr – °F	17.8 W/m – °K
Thermal conductivity	500°C	13.1 BTU/ft- hr – °F	23 W/m – °K
Electrical properties	Electrical resistivity	770 nΩ ∙ m
Electrical properties	Magnetic parambility	95

Mechanical Properties

Condition	Tensile								Hardness
	Ultimate		Yield		Elongation		Reduction in area, %		HB
	KSI	MPa	KSI	MPa	Lo	Tr	Lo	Tr	Range
H900	190	1310	170	1170	10	6	35	15	388-444
H925	170	1170	155	1070	10	7	38	20	375-429
H1025	155	1070	145	1000	12	8	45	27	331-401
H1075	145	1000	125	860	13	9	45	28	311-375
H1150	135	930	105	725	16	11	50	30	302-363
H1150M	115	795	75	515	18	14	55	35	277-352

Specifications
- AMS – 5659
- ASTM – A564
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Stainless Steel Alloy 15-5Ph Sales:+972 4 618 2000

General Characteristics

15-5Ph is a precipitation hardening martensitic stainless-steel considered of being a compositional modification of 17-4 with minimal delta ferrite. A wide range of mechanical properties is available via simple aging within a 900-1150°F (482-621°C) temperature range. Vacuum arc re-melting provides low gas content, superior cleanliness and optimum transverse properties.

Typical applications include aircraft and missile structural components, gears, valves, fasteners, jet engine and nuclear reactor parts. It is favored over 17-4 when transverse properties are of concern.
Typical Chemical Composition

Weight % C Mn Si Cr Ni P S Cu Nb Fe

minimum — — — 14.00 3.50 — — 2.50 0.15 Remainder

maximum 0.07 1.00 1.00 15.50 5.50 0.04 0.03 4.50 0.45

Weight %	C	Mn	Si	Cr	Ni	P	S	Cu	Nb	Fe
minimum	—	—	—	14.00	3.50	—	—	2.50	0.15	Remainder
maximum	0.07	1.00	1.00	15.50	5.50	0.04	0.03	4.50	0.45

Physical Properties (Annealed condition)

Characteristics		English	Metric
Nominal density (68°F/20°C)		0.28 lbs/in³	7.80 g/cm³
Melting range		2560°F-2625°F	1400°C-1440°C
Specific heat (212 °F/100°C)		0.10 BTU/lb – °F	420 J/KG- °K
Coefficient of thermal expansion	32°F – 212°F 0°C – 100°C	6.0 micro in/in- °F	10.8 micro m/m- °K
Coefficient of thermal expansion	32°F – 600°F 0°C – 315°C	6.3 micro in/in- °F	11.4 micro m/m- °K
Thermal conductivity	100°C	10.3 BTU/ft- hr – °F	17.8 W/m – °K
Thermal conductivity	500°C	13.1 BTU/ft- hr – °F	23 W/m – °K
Electrical properties	Electrical resistivity	770 nΩ ∙ m
Electrical properties	Magnetic parambility	95

Mechanical Properties

Condition	Tensile								Hardness
	Ultimate		Yield		Elongation		Reduction in area, %		HB
	KSI	MPa	KSI	MPa	Lo	Tr	Lo	Tr	Range
H900	190	1310	170	1170	10	6	35	15	388-444
H925	170	1170	155	1070	10	7	38	20	375-429
H1025	155	1070	145	1000	12	8	45	27	331-401
H1075	145	1000	125	860	13	9	45	28	311-375
H1150	135	930	105	725	16	11	50	30	302-363
H1150M	115	795	75	515	18	14	55	35	277-352

Specifications
- AMS – 5659
- ASTM – A564

Aluminum Alloy 7050
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General Characteristics

The 7050 alloy is used in aircraft structural parts. This alloy has characteristics of high strength coupled with good resistance to exfoliation and stress corrosion cracking (SCC). It also has good fracture toughness and fatigue resistance.

Typical Chemical Composition

										Other
Weight %	Si	Fe	Cu	Mn	Mg	Cr	Zn	Ti	Zr	Each	Total	Aluminum
minimum	—	—	2.00	—	1.90	—	5.70	—	0.08	—	—	Remainder
maximum	0.12	0.15	2.60	0.10	2.60	0.04	6.70	0.06	0.15	0.05	0.15	Remainder

Physical Properties

Characteristics		English	Metric
Nominal density (68°F/20°C)		0.102 lbs/in³	2.83 Mg/m³
Melting range		870°F-1175°F	524°C-635°C
Coefficient of thermal expansion	Linear 68°F – 212°F 20°C – 100°C	13.1 micro in/in- °F	23.5 micro m/m- °K
Coefficient of thermal expansion	Volumetric 68°F / 20°C	3.78 x 10^-5 in.³/in.³– °F	68 x 10^-6 m³/m³– °K
Thermal conductivity (68°F/20°C)	T76, T76511	89 BTU/ft- hr – °F	154 W/m – °K
Thermal conductivity (68°F/20°C)	T3, T7351, T74, T74511	91 BTU/ft- hr – °F	157 W/m – °K
Electrical conductivity (68°F/20°C)	Equal Volume	T76, T76511	39.5% IACS
Electrical conductivity (68°F/20°C)	Equal Volume	T3, T7351, T74, T74511	40.5% IACS

Mechanical Properties

Temper	Tensile					Hardness	Shear		Fatigue		Modulus
	Ultimate		Yield		Elongation/4D	Brinell 500 kg 10 mm	Ultimate shearing strength		Endurance limit-R.R.Moore type		Modulus of elasticity
	KSI	MPa	KSI	MPa	0.500″ Dia. Specimen		KSI	MPa	KSI	MPa	KSIx103	Gpa
T74511	76	524	68	469	11	140	44	303	—	—	10.2	70.3
T76511	80	552	71	489	11	150	47	324	—	—	10.2	70.3

Specifications
- AMS – 4108, QQ-A-430
- ASTM – B247, B316
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Aluminum Alloy 7050 Sales:+972 4 618 2000

General Characteristics

The 7050 alloy is used in aircraft structural parts. This alloy has characteristics of high strength coupled with good resistance to exfoliation and stress corrosion cracking (SCC). It also has good fracture toughness and fatigue resistance.

Typical Chemical Composition

										Other
Weight %	Si	Fe	Cu	Mn	Mg	Cr	Zn	Ti	Zr	Each	Total	Aluminum
minimum	—	—	2.00	—	1.90	—	5.70	—	0.08	—	—	Remainder
maximum	0.12	0.15	2.60	0.10	2.60	0.04	6.70	0.06	0.15	0.05	0.15	Remainder

Physical Properties

Characteristics		English	Metric
Nominal density (68°F/20°C)		0.102 lbs/in³	2.83 Mg/m³
Melting range		870°F-1175°F	524°C-635°C
Coefficient of thermal expansion	Linear 68°F – 212°F 20°C – 100°C	13.1 micro in/in- °F	23.5 micro m/m- °K
Coefficient of thermal expansion	Volumetric 68°F / 20°C	3.78 x 10^-5 in.³/in.³– °F	68 x 10^-6 m³/m³– °K
Thermal conductivity (68°F/20°C)	T76, T76511	89 BTU/ft- hr – °F	154 W/m – °K
Thermal conductivity (68°F/20°C)	T3, T7351, T74, T74511	91 BTU/ft- hr – °F	157 W/m – °K
Electrical conductivity (68°F/20°C)	Equal Volume	T76, T76511	39.5% IACS
Electrical conductivity (68°F/20°C)	Equal Volume	T3, T7351, T74, T74511	40.5% IACS

Mechanical Properties

Temper	Tensile					Hardness	Shear		Fatigue		Modulus
	Ultimate		Yield		Elongation/4D	Brinell 500 kg 10 mm	Ultimate shearing strength		Endurance limit-R.R.Moore type		Modulus of elasticity
	KSI	MPa	KSI	MPa	0.500″ Dia. Specimen		KSI	MPa	KSI	MPa	KSIx103	Gpa
T74511	76	524	68	469	11	140	44	303	—	—	10.2	70.3
T76511	80	552	71	489	11	150	47	324	—	—	10.2	70.3

Specifications
- AMS – 4108, QQ-A-430
- ASTM – B247, B316

Aluminum Alloy 7075
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General Characteristics

The 7075 alloy offers the highest strength of the common screw machine alloys. The superior stress corrosion resistance of the T173 and T7351 tempers makes it a logical replacement for 2024, 2014 and 2017 in many critical applications. The T6 and T651 tempers have fair machinability, resistance welding and corrosion resistance ratings. This alloy is heavily utilized by the aircraft and ordnance industries given its superior strength.
Typical Chemical Composition

Other

Weight % Si Fe Cu Mn Mg Cr Zn Ti Each Total Aluminum

minimum — — 1.20 — 2.10 0.18 5.10 — — — Remainder

maximum 0.40 0.50 2.00 0.30 2.90 0.28 6.10 0.20 0.05 0.15

	Other
minimum	—	—	1.20	—	2.10	0.18	5.10	—	—	—	Remainder
maximum	0.40	0.50	2.00	0.30	2.90	0.28	6.10	0.20	0.05	0.15

Physical Properties

Characteristics		English	Metric
Nominal density (68°F/20°C)		0.101 lbs/in³	2.80 Mg/m³
Melting range		990°F-1175°F	532°C-635°C
Coefficient of thermal expansion	Linear 68°F – 212°F 20°C – 100°C	13.0 micro in/in- °F	23.4 micro m/m- °K
Coefficient of thermal expansion	Volumetric 68°F / 20°C	3.78 x 10^-5 in.³/in.³– °F	68 x 10^-6 m³/m³– °K
Thermal conductivity (68°F/20°C)	T6, T651	75 BTU/ft- hr – °F	130 W/m – °K
Thermal conductivity (68°F/20°C)	T73, T7351	90 BTU/ft- hr – °F	155 W/m – °K
Electrical conductivity (68°F/20°C)	Equal Volume	T6, T651	33% IACS
	Equal Volume	T73, T7351	40% IACS
	Equal Weight	T6, T651	105% IACS

Mechanical Properties

Temper	Tensile (0.500″ Dia. Specimen)					Hardness	Shear		Fatigue		Modulus
	Ultimate		Yield		Elongation/4D	Brinell 500 kg 10 mm	Ultimate shearing strength		Endurance limit-R.R.Moore type		Modulus of elasticity
	KSI	MPa	KSI	MPa	%		KSI	MPa	KSI	MPa	KSIx103	Gpa
O	33	228	15	103	17	60	22	152	—	—	10.3	71.0
T6, T651	83	572	73	503	11	150	48	331	23	158	10.3	71.0
T73, T7351	73	503	63	434	13	—	44	303	23	158	10.3	71.0

Specifications
- AMS – 4122, 4123, 4124, 4154, 4166, 4167, 4168, 4169, 4187, QQ-A-225/9, QQ-A-200/11
- ASTM – B211, B221
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Aluminum Alloy 7075 Sales:+972 4 618 2000

General Characteristics

The 7075 alloy offers the highest strength of the common screw machine alloys. The superior stress corrosion resistance of the T173 and T7351 tempers makes it a logical replacement for 2024, 2014 and 2017 in many critical applications. The T6 and T651 tempers have fair machinability, resistance welding and corrosion resistance ratings. This alloy is heavily utilized by the aircraft and ordnance industries given its superior strength.
Typical Chemical Composition

Other

Weight % Si Fe Cu Mn Mg Cr Zn Ti Each Total Aluminum

minimum — — 1.20 — 2.10 0.18 5.10 — — — Remainder

maximum 0.40 0.50 2.00 0.30 2.90 0.28 6.10 0.20 0.05 0.15

	Other
minimum	—	—	1.20	—	2.10	0.18	5.10	—	—	—	Remainder
maximum	0.40	0.50	2.00	0.30	2.90	0.28	6.10	0.20	0.05	0.15

Physical Properties

Characteristics		English	Metric
Nominal density (68°F/20°C)		0.101 lbs/in³	2.80 Mg/m³
Melting range		990°F-1175°F	532°C-635°C
Coefficient of thermal expansion	Linear 68°F – 212°F 20°C – 100°C	13.0 micro in/in- °F	23.4 micro m/m- °K
Coefficient of thermal expansion	Volumetric 68°F / 20°C	3.78 x 10^-5 in.³/in.³– °F	68 x 10^-6 m³/m³– °K
Thermal conductivity (68°F/20°C)	T6, T651	75 BTU/ft- hr – °F	130 W/m – °K
Thermal conductivity (68°F/20°C)	T73, T7351	90 BTU/ft- hr – °F	155 W/m – °K
Electrical conductivity (68°F/20°C)	Equal Volume	T6, T651	33% IACS
	Equal Volume	T73, T7351	40% IACS
	Equal Weight	T6, T651	105% IACS

Mechanical Properties

Temper	Tensile (0.500″ Dia. Specimen)					Hardness	Shear		Fatigue		Modulus
	Ultimate		Yield		Elongation/4D	Brinell 500 kg 10 mm	Ultimate shearing strength		Endurance limit-R.R.Moore type		Modulus of elasticity
	KSI	MPa	KSI	MPa	%		KSI	MPa	KSI	MPa	KSIx103	Gpa
O	33	228	15	103	17	60	22	152	—	—	10.3	71.0
T6, T651	83	572	73	503	11	150	48	331	23	158	10.3	71.0
T73, T7351	73	503	63	434	13	—	44	303	23	158	10.3	71.0

Specifications
- AMS – 4122, 4123, 4124, 4154, 4166, 4167, 4168, 4169, 4187, QQ-A-225/9, QQ-A-200/11
- ASTM – B211, B221

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BROWSE CATALOGUE

Aerospace

Superior metals for higher-performance demand

Typical Applications

Jet Engine Parts

Landing Gear

Aircraft Wings

Metals Used in This Industry

VIEW

General Characteristics

Typical Chemical Composition

Physical Properties (Annealed condition)

Mechanical Properties

Specifications

General Characteristics

Typical Chemical Composition

Physical Properties (Annealed condition)

Mechanical Properties

Specifications

VIEW

General Characteristics

Typical Chemical Composition

Physical Properties

Mechanical Properties

Specifications

General Characteristics

Typical Chemical Composition

Physical Properties

Mechanical Properties

Specifications

VIEW

General Characteristics

Typical Chemical Composition

Physical Properties

Mechanical Properties

Specifications

General Characteristics

Typical Chemical Composition

Physical Properties

Mechanical Properties

Specifications

View full Quality Metals catalogue

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