Titanium Ti-13V-11Cr-3Al; (Ti-13-11-3) Annealed 800°C, 30 min.

Login to see your most recently viewed materials here. Or if you don't have an account with us yet, then click here to register.

(Viewing data as-entered. Click here to return)

Titanium Ti-13V-11Cr-3Al; (Ti-13-11-3) Annealed 800°C, 30 min.
Categories:	Metal; Nonferrous Metal; Titanium Alloy; Beta Titanium Alloy
Material Notes:	Good ductility and fabrication properties, aging yields extremely high strengths, low density. Applications: Areospace and missile applications, springs 5 other heat treatments of this alloy are in MatWeb.
Key Words:	Ti-13-11-3; B120VCA; UNS R58010
Vendors:	Visit metalmen for your metals needs. Products include special chemistry, tight tolerances, custom tempers, odd dimensions/forms, and small quantities. Phone 1-800-767-9494. Click here to view all available suppliers for this material. Please click here if you are a supplier and would like information on how to add your listing to this material.
Printer friendly version Download as PDF Download to Excel (requires Excel and Windows) Export data to your CAD/FEA program Add to Folder:

Physical Properties	Original Value	Comments

Density	4.82 g/cc

Mechanical Properties	Original Value	Comments
Hardness, Brinell	318	Estimated from Rockwell C.
Hardness, Knoop	346	Estimated from Rockwell C.
Hardness, Rockwell C	34
Hardness, Vickers	333	Estimated from Rockwell C.
Tensile Strength	792 MPa @Temperature 316 °C
Tensile Strength, Ultimate	950 MPa
Tensile Strength, Yield	860 MPa
Elongation at Break	18 %
Tensile Modulus	99.0 GPa
Modulus of Rigidity	42.7 GPa
Compressive Yield Strength	900 MPa
Compressive Modulus	105 GPa
Notched Tensile Strength	1170 MPa	K_t (stress concentration factor) = 3.0
Ultimate Bearing Strength	1860 MPa	e/D = 2
Bearing Yield Strength	1380 MPa	e/D = 2
Poissons Ratio	0.30
Fatigue Strength	140 MPa @# of Cycles 1.00e+7	K_t (stress concentration factor) = 3.0
	200 MPa @# of Cycles 1.00e+7	stress ratio = -1.0
	340 MPa @# of Cycles 1.00e+7	Unnotched
	375 MPa @# of Cycles 30000	stress ratio = -1.0
Fracture Toughness	88.0 MPa-m½	K_IC
Shear Modulus	43.0 GPa
Shear Strength	660 MPa	Ultimate shear strength
Charpy Impact	20.0 J	V-notch

Electrical Properties	Original Value	Comments
Electrical Resistivity	0.000140 ohm-cm

Thermal Properties	Original Value	Comments
CTE, linear	9.70 µm/m-°C @Temperature 20.0 - 95.0 °C
Specific Heat Capacity	0.545 J/g-°C @Temperature 20.0 °C
	0.833 J/g-°C @Temperature 425 °C
Thermal Conductivity	6.90 W/m-K
Beta Transus	700 °C	Commercial grade; lower for grades with lower oxygen content

Component Elements Properties	Original Value	Comments
Aluminum, Al	3.0 %
Carbon, C	<= 0.10 %
Chromium, Cr	11 %
Hydrogen, H	<= 0.015 %
Iron, Fe	<= 0.35 %
Nitrogen, N	<= 0.080 %
Oxygen, O	<= 0.20 %
Titanium, Ti	73 %
Vanadium, V	13 %

References for this datasheet.

Some of the values displayed above may have been converted from their original units and/or rounded in order to display the information in a consistent format. Users requiring more precise data for scientific or engineering calculations can click on the property value to see the original value as well as raw conversions to equivalent units. We advise that you only use the original value or one of its raw conversions in your calculations to minimize rounding error. We also ask that you refer to MatWeb's terms of use regarding this information. Click here to go back to viewing the property data in MatWeb's normal format.

Users viewing this material also viewed the following:
Titanium Ti-13V-11Cr-3Al; (Ti-13-11-3) Annealed 850°C (1560°F) + Aged 510°C 8 hr
Titanium Ti-13V-11Cr-3Al (Ti-13-11-3) Aged 490°C
Titanium Ti-13V-11Cr-3Al (Ti-13-11-3) SolnTreat; Age 450°C
Titanium Ti-13V-11Cr-3Al (Ti-13-11-3) Solution Treated
Titanium Ti-13V-11Cr-3Al (Ti-13-11-3) Aged 400°C

MTB314 / 14186

	Advertise with MatWeb!
	Data sheets for over 180,000 metals, plastics, ceramics, and composites.
	HOME • SEARCH • TOOLS • SUPPLIERS • FOLDERS • ABOUT US • FAQ • LOG IN

System Message