Aerospace Titanium. Guaranteed supply & processing. We deliver what you need.

The use of titanium in the aerospace industry has grown steadily over the years. We can secure supply and can process it however you need.

Discover our titanium stock of commercially pure and alloyed forms.

The principal characteristics of commercially pure titanium include an excellent resistance to corrosion by a wide range of natural and artificial environments, together with a useful strength-to-weight ratio.

Commercially pure titanium can be readily forged, formed, or welded by most of the processes conventionally used for stainless steel, which it resembles in many mechanical and chemical respects.

The most common and widely-used titanium alloy in the aerospace industry is 6Al-4V, which is used for applications that require higher strength and corrosion resistance.

UK	USA	Germany	France	Europe	Alloy	Manufacturers Specifications	Company
		W.-Nr. 3.7025
	ASTM B-265-GR.1	LN 9297
BS TA3		W.-Nr. 3.7035
	ASTM B-265-GR.2	LN 9297
		WL 3.7154
	ASTM B-265-GR.3	LN 9297
		W.-Nr. 3.7065
	ASTM B-265-GR.4	LN 9297
	MIL-T-9046 Type 3 Comp.C					ASN-A 3304	Airbus
	AMS 4904					ASN-A 3307	Airbus
	AMS 4905					BMS 7-347	Boeing
	AMS 4928					BMS 7-380	Boeing
	AMS 4965					DMS 1592	Boeing
						MSRR 8633	Rolls-Royce
BS TA46		W.-Nr. 3.7185
BS TA57
		WL 3.7174
	AMS 4917				13.5V-11Cr-3Al
	AMS 4914				15V-3Al-3Cr-3Sn	BMS 7-281	Boeing
BS TA45		WL 3.7184	AIR 9182 T-A4DE		4Al-4Mo-2Sn
	AMS 4910				5Al-2.5Sn
	AMS 4919				6Al-2Sn-4Zr-2Mo	BMS 7-246	Boeing
BS TA56	ASTM B-265-Gr.5	WL 3.7164			6Al-4V	DMD 776-25	Snecma
	AMS 4918	W.-Nr. 3.7175/			6Al-6V-2Sn
	AMS 4915				8Al-1V-1Mo
	AMS 4916				8Al-1V-1Mo
BS TA6	AMS 4901	WL 3.7064	AIR 9182 T-60		CP1-GRADE 4	DMS 1536	Boeing
DTD 5023	AMS 4900	W.-Nr. 3.7155	AIR 9182 T-50		CP2-GRADE 3	MSRR 8608	Rolls-Royce
BS TA2	AMS 4902	WL 3.7034	AIR 9182 T-40		CP3-GRADE 2	AIMS 08-18-002	Airbus
BS TA1		WL 3.7024	AIR 9182 T-35		CP4-GRADE 1
BS TA10	AMS 4911	W.-Nr. 3.7165	AIR 9182 TA 6V	EN 3464	GRADE 5	DMD 776-24	Snecma

UK	USA	Germany	France	Europe	Alloy	Manufacturers Specifications	Company
		W.-Nr. 3.7025
	ASTM B-265-GR.1	LN 9297
BS TA3		W.-Nr. 3.7035
	ASTM B-265-GR.2	LN 9297
		WL 3.7154
	ASTM B-265-GR.3	LN 9297
		W.-Nr. 3.7065
	ASTM B-265-GR.4	LN 9297
	MIL-T-9046 Type 3 Comp.C					ASN-A 3304	Airbus
	AMS 4904					ASN-A 3307	Airbus
	AMS 4905					BMS 7-347	Boeing
	AMS 4928					BMS 7-380	Boeing
	AMS 4965					DMS 1592	Boeing
						MSRR 8633	Rolls-Royce
BS TA46		W.-Nr. 3.7185
BS TA57
		WL 3.7174
	AMS 4917				13.5V-11Cr-3Al
	AMS 4914				15V-3Al-3Cr-3Sn	BMS 7-281	Boeing
BS TA45		WL 3.7184	AIR 9182 T-A4DE		4Al-4Mo-2Sn
	AMS 4910				5Al-2.5Sn
	AMS 4919				6Al-2Sn-4Zr-2Mo	BMS 7-246	Boeing
BS TA56	ASTM B-265-Gr.5	WL 3.7164			6Al-4V	DMD 776-25	Snecma
	AMS 4918	W.-Nr. 3.7175/			6Al-6V-2Sn
	AMS 4915				8Al-1V-1Mo
	AMS 4916				8Al-1V-1Mo
BS TA6	AMS 4901	WL 3.7064	AIR 9182 T-60		CP1-GRADE 4	DMS 1536	Boeing
DTD 5023	AMS 4900	W.-Nr. 3.7155	AIR 9182 T-50		CP2-GRADE 3	MSRR 8608	Rolls-Royce
BS TA2	AMS 4902	WL 3.7034	AIR 9182 T-40		CP3-GRADE 2	AIMS 08-18-002	Airbus
BS TA1		WL 3.7024	AIR 9182 T-35		CP4-GRADE 1
BS TA10	AMS 4911	W.-Nr. 3.7165	AIR 9182 TA 6V	EN 3464	GRADE 5	DMD 776-24	Snecma

Specification	Grade/Alloy	Company
Europe
EN 3464	GRADE 5	Snecma
France
AIR 9182 T-A4DE	4Al-4Mo-2Sn
AIR 9182 T-60	CP1-GRADE 4	Boeing
AIR 9182 T-50	CP2-GRADE 3	Rolls-Royce
AIR 9182 T-40	CP3-GRADE 2	Airbus
AIR 9182 T-35	CP4-GRADE 1
AIR 9182 TA 6V	GRADE 5	Snecma
Germany
W.-Nr. 3.7025
LN 9297
W.-Nr. 3.7035
LN 9297
WL 3.7154
LN 9297
W.-Nr. 3.7065
LN 9297
W.-Nr. 3.7185
WL 3.7174
WL 3.7184	4Al-4Mo-2Sn
WL 3.7164	6Al-4V	Snecma
W.-Nr. 3.7175/	6Al-6V-2Sn
WL 3.7064	CP1-GRADE 4	Boeing
W.-Nr. 3.7155	CP2-GRADE 3	Rolls-Royce
WL 3.7034	CP3-GRADE 2	Airbus
WL 3.7024	CP4-GRADE 1
W.-Nr. 3.7165	GRADE 5	Snecma
UK
BS TA3
BS TA46
BS TA57
BS TA45	4Al-4Mo-2Sn
BS TA56	6Al-4V	Snecma
BS TA6	CP1-GRADE 4	Boeing
DTD 5023	CP2-GRADE 3	Rolls-Royce
BS TA2	CP3-GRADE 2	Airbus
BS TA1	CP4-GRADE 1
BS TA10	GRADE 5	Snecma
USA
ASTM B-265-GR.1
ASTM B-265-GR.2
ASTM B-265-GR.3
ASTM B-265-GR.4
MIL-T-9046 Type 3 Comp.C		Airbus
AMS 4904		Airbus
AMS 4905		Boeing
AMS 4928		Boeing
AMS 4965		Boeing
AMS 4917	13.5V-11Cr-3Al
AMS 4914	15V-3Al-3Cr-3Sn	Boeing
AMS 4910	5Al-2.5Sn
AMS 4919	6Al-2Sn-4Zr-2Mo	Boeing
ASTM B-265-Gr.5	6Al-4V	Snecma
AMS 4918	6Al-6V-2Sn
AMS 4915	8Al-1V-1Mo
AMS 4916	8Al-1V-1Mo
AMS 4901	CP1-GRADE 4	Boeing
AMS 4900	CP2-GRADE 3	Rolls-Royce
AMS 4902	CP3-GRADE 2	Airbus
AMS 4911	GRADE 5	Snecma

Specification	Grade/Alloy	Company
Europe
EN 3464	GRADE 5	Snecma
France
AIR 9182 T-A4DE	4Al-4Mo-2Sn
AIR 9182 T-60	CP1-GRADE 4	Boeing
AIR 9182 T-50	CP2-GRADE 3	Rolls-Royce
AIR 9182 T-40	CP3-GRADE 2	Airbus
AIR 9182 T-35	CP4-GRADE 1
AIR 9182 TA 6V	GRADE 5	Snecma
Germany
W.-Nr. 3.7025
LN 9297
W.-Nr. 3.7035
LN 9297
WL 3.7154
LN 9297
W.-Nr. 3.7065
LN 9297
W.-Nr. 3.7185
WL 3.7174
WL 3.7184	4Al-4Mo-2Sn
WL 3.7164	6Al-4V	Snecma
W.-Nr. 3.7175/	6Al-6V-2Sn
WL 3.7064	CP1-GRADE 4	Boeing
W.-Nr. 3.7155	CP2-GRADE 3	Rolls-Royce
WL 3.7034	CP3-GRADE 2	Airbus
WL 3.7024	CP4-GRADE 1
W.-Nr. 3.7165	GRADE 5	Snecma
UK
BS TA3
BS TA46
BS TA57
BS TA45	4Al-4Mo-2Sn
BS TA56	6Al-4V	Snecma
BS TA6	CP1-GRADE 4	Boeing
DTD 5023	CP2-GRADE 3	Rolls-Royce
BS TA2	CP3-GRADE 2	Airbus
BS TA1	CP4-GRADE 1
BS TA10	GRADE 5	Snecma
USA
ASTM B-265-GR.1
ASTM B-265-GR.2
ASTM B-265-GR.3
ASTM B-265-GR.4
MIL-T-9046 Type 3 Comp.C		Airbus
AMS 4904		Airbus
AMS 4905		Boeing
AMS 4928		Boeing
AMS 4965		Boeing
AMS 4917	13.5V-11Cr-3Al
AMS 4914	15V-3Al-3Cr-3Sn	Boeing
AMS 4910	5Al-2.5Sn
AMS 4919	6Al-2Sn-4Zr-2Mo	Boeing
ASTM B-265-Gr.5	6Al-4V	Snecma
AMS 4918	6Al-6V-2Sn
AMS 4915	8Al-1V-1Mo
AMS 4916	8Al-1V-1Mo
AMS 4901	CP1-GRADE 4	Boeing
AMS 4900	CP2-GRADE 3	Rolls-Royce
AMS 4902	CP3-GRADE 2	Airbus
AMS 4911	GRADE 5	Snecma

Specification	Grade/Alloy	Country
Airbus
ASN-A 3304		USA
ASN-A 3307		USA
AIMS 08-18-002	CP3-GRADE 2	UK
Boeing
BMS 7-347		USA
BMS 7-380		USA
DMS 1592		USA
BMS 7-281	15V-3Al-3Cr-3Sn	USA
BMS 7-246	6Al-2Sn-4Zr-2Mo	USA
DMS 1536	CP1-GRADE 4	UK
Rolls-Royce
MSRR 8633		UK
MSRR 8608	CP2-GRADE 3	UK
Snecma
DMD 776-25	6Al-4V	UK
DMD 776-24	GRADE 5	UK

Specification	Grade/Alloy	Country
Airbus
ASN-A 3304		USA
ASN-A 3307		USA
AIMS 08-18-002	CP3-GRADE 2	UK
Boeing
BMS 7-347		USA
BMS 7-380		USA
DMS 1592		USA
BMS 7-281	15V-3Al-3Cr-3Sn	USA
BMS 7-246	6Al-2Sn-4Zr-2Mo	USA
DMS 1536	CP1-GRADE 4	UK
Rolls-Royce
MSRR 8633		UK
MSRR 8608	CP2-GRADE 3	UK
Snecma
DMD 776-25	6Al-4V	UK
DMD 776-24	GRADE 5	UK

How to calculate the weight

The weight is easily calculated. Simply multiply the appropriate alloy density by the thickness, width, and length of the required part (see worked example below).

Metric	density (g/cm³)	x T	x W	x L	= weight
Example	4.50g/cm³	x 6mm	x 2m	x 1m	= 54.00 kg

Metric	density (g/cm³)	x T	x W	x L	= weight
Example	0.163 lbs/in³	x 4in	x 48in	x 144in	= 4506.6 lbs

For an accurate calculation it is also important to allow for the rolling tolerance which affects the thickness and the cutting tolerances which affect the width and length. These vary from thickness to thickness – please contact us for details.

Density of titanium

The acknowledged density of titanium is 4.50 g/cm3 (0.163 lbs/in3). Depending on the alloy elements added to manufactured specifications this can vary between 4.4 and 4.9 g/cm3 (0.159 and 0.177 lbs/in3).

The following charts are samples of some of the common thicknesses and sizes that are available. Please contact us for details of our full product range and current stock availability.

Sheet - Metric			Sheet - Imperial			Plate - Metric			Plate - Imperial
Thickness mm	Size m	Weight kg/sheet	Thickness in	Size ft	Weight lbssheet	Thickness mm	Size m	Weight kg/plate	Thickness in	Size ft	Weight lbs/plate
457	2 x 1	4.11	18	10 x 3	12.67	9.53	2 x 1	85.8	375	12 x 4	422.5
508	2 x 1	4.57	20	10 x 3	14.08	10.00	2 x 1	90.0
635	2 x 1	5.72	25	10 x 3	17.60	12.00	2 x 1	108.0
762	2 x 1	6.86	30	10 x 3	21.12	12.700	2 x 1	114.3	500	12 x 4	563.3
813	2 x 1	7.32	32	10 x 3	22.53	15.000	2 x 1	135.0
889	2 x 1	8.00	35	10 x 3	24.65	15.880	2 x 1	142.9	625	12 x 4	704.2
1.016	2 x 1	9.14	40	10 x 3	28.17	19.050	2 x 1	171.5	750	12 x 4	845.0
1.270	2 x 1	11.43	50	10 x 3	35.21	20.00	2 x 1	180.0
1.50	2 x 1	13.50				25.00	2 x 1	225.0
1.60	2 x 1	14.40	63	10 x 3	44.36	25.40	2 x 1	228.6	1	12 x 4	1126.7
1.80	2 x 1	16.20	71	10 x 3	50.00	30.00	2 x 1	270.0
2.03	2 x 1	18.27	80	10 x 3	56.33	31.75	2 x 1	285.8	1.25	12 x 4	1408.3
2.29	2 x 1	20.57	90	10 x 3	63.37	38.10	2 x 1	342.9	1.5	12 x 4	1690.0
2.54	2 x 1	22.86	100	10 x 3	70.42	40.00	2 x 1	360.0
3.00	2 x 1	27.00				44.45	2 x 1	400.1	1.75	12 x 4	1971.6
			125	10 x 3	88.02	45.00	2 x 1	405.0
						50.00	2 x 1	450.0
			140	10 x 3	98.58	50.80	2 x 1	457.2	2	12 x 4	2253.3
			150	10 x 3	105.62	60.00	2 x 1	540.0
						63.50	2 x 1	571.5	2.5	12 x 4	2816.6
						65.00	2 x 1	585.0
			188	10 x 3	132.38	70.00	2 x 1	630.0
						75.00	2 x 1	675.0
			250	12 x 4	176.04	76.20	2 x 1	685.8	3	12 x 4	3380.0
						80.00	2 x 1	720.0
						88.90	2 x 1	800.1	3.5	12 x 4	3943.3
						90.00	2 x 1	810.0
						100.00	2 x 1	900.0
						101.60	2 x 1	914.4	4	12 x 4	4506.6
						125.00	2 x 1	1125.0
						127.00	2 x 1	1143.0	5	12 x 4	5633.3
						150.00	2 x 1	1350.0
						152.40	2 x 1	1371.6	6	12 x 4	6759.9

Sheet - Metric			Sheet - Imperial			Plate - Metric			Plate - Imperial
Thickness mm	Size m	Weight kg/sheet	Thickness in	Size ft	Weight lbssheet	Thickness mm	Size m	Weight kg/plate	Thickness in	Size ft	Weight lbs/plate
457	2 x 1	4.11	18	10 x 3	12.67	9.53	2 x 1	85.8	375	12 x 4	422.5
508	2 x 1	4.57	20	10 x 3	14.08	10.00	2 x 1	90.0
635	2 x 1	5.72	25	10 x 3	17.60	12.00	2 x 1	108.0
762	2 x 1	6.86	30	10 x 3	21.12	12.700	2 x 1	114.3	500	12 x 4	563.3
813	2 x 1	7.32	32	10 x 3	22.53	15.000	2 x 1	135.0
889	2 x 1	8.00	35	10 x 3	24.65	15.880	2 x 1	142.9	625	12 x 4	704.2
1.016	2 x 1	9.14	40	10 x 3	28.17	19.050	2 x 1	171.5	750	12 x 4	845.0
1.270	2 x 1	11.43	50	10 x 3	35.21	20.00	2 x 1	180.0
1.50	2 x 1	13.50				25.00	2 x 1	225.0
1.60	2 x 1	14.40	63	10 x 3	44.36	25.40	2 x 1	228.6	1	12 x 4	1126.7
1.80	2 x 1	16.20	71	10 x 3	50.00	30.00	2 x 1	270.0
2.03	2 x 1	18.27	80	10 x 3	56.33	31.75	2 x 1	285.8	1.25	12 x 4	1408.3
2.29	2 x 1	20.57	90	10 x 3	63.37	38.10	2 x 1	342.9	1.5	12 x 4	1690.0
2.54	2 x 1	22.86	100	10 x 3	70.42	40.00	2 x 1	360.0
3.00	2 x 1	27.00				44.45	2 x 1	400.1	1.75	12 x 4	1971.6
			125	10 x 3	88.02	45.00	2 x 1	405.0
						50.00	2 x 1	450.0
			140	10 x 3	98.58	50.80	2 x 1	457.2	2	12 x 4	2253.3
			150	10 x 3	105.62	60.00	2 x 1	540.0
						63.50	2 x 1	571.5	2.5	12 x 4	2816.6
						65.00	2 x 1	585.0
			188	10 x 3	132.38	70.00	2 x 1	630.0
						75.00	2 x 1	675.0
			250	12 x 4	176.04	76.20	2 x 1	685.8	3	12 x 4	3380.0
						80.00	2 x 1	720.0
						88.90	2 x 1	800.1	3.5	12 x 4	3943.3
						90.00	2 x 1	810.0
						100.00	2 x 1	900.0
						101.60	2 x 1	914.4	4	12 x 4	4506.6
						125.00	2 x 1	1125.0
						127.00	2 x 1	1143.0	5	12 x 4	5633.3
						150.00	2 x 1	1350.0
						152.40	2 x 1	1371.6	6	12 x 4	6759.9

Density based on 4.50 g/cm3
(0.163 lbs/in3)

How to calculate the weight

The weight of bars is just as easily calculated. Simply multiply the appropriate alloy density (see chart below) by π, the squared radius (equals half the diameter) and length of the required part (see worked example below).

Metric	density (g/cm³)	x π	x L	x (0.5 x d)²	= weight
Example	4.50 g/cm³	x π	x 2.5m	x (0.5 x 0.4m)²	= 1413.72 kg

Imperial	density (lbs/in³)	x π	x L	x (0.5 x d)²	= weight
Example	0.163 lbs/in³	x π	x 144in	x (0.5 x 15in)²	= 4147.85lbs

How to calculate the weight

The weight of tubes is just as easily calculated. Simply multiply the appropriate alloy density (see chart below) by π, the length of the required part, and the variable q. q is herein defined as outer diameter of the tube, multiplied by the thickness and minus the squared thickness (see worked example below).

Metric	density (g/cm³)	x π	x L	x q (= d x t - t²)	= weight
Example	4.50 g/cm³	x π	x 2.5m	x (0.4m x 3mm - (3mm)²)	= 42.09 kg

Imperial	density (lbs/in³)	x π	x L	x q (= d x t - t²)	= weight
Example	0.163 lbs/in³	x π	x 144in	x (15in x 0.2in - (0.2in)²)	= 218.27lbs

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Titanium: commercially pure and alloyed forms kept in stock

Discover our titanium stock of commercially pure and alloyed forms.

How to calculate the weight

Density of titanium

How to calculate the weight

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