Metals & alloys · Titanium & zirconium alloys

Ti–5Al–5Mo–5V–3Cr / Ti-5553

A high-strength metastable-beta titanium alloy used for large aerospace forgings and landing-gear structures requiring thick-section hardenability and fracture performance.

Family
Metastable Beta Titanium Alloy
Record
Standard
Conditions
1
Sources
3
Browse this family
More

01

Overview

Material class
Metals & alloys
Category
Titanium & zirconium alloys
Family
Metastable Beta Titanium Alloy
Product forms
Sheet/plate, Bar/rod

Composition

ConstituentMinMaxTypicalNote
Al4.45.75
Mo45.55
V45.55
Cr2.53.53
Fe0.50.3
TiBalance

02

Properties and conditions

Engineering properties

PropertyValueUnitCondition
Density~4.65g/cm³Representative; verify product form and condition
Elastic modulus~110GPaRepresentative; verify product form and condition
Yield strength~1050–1250MPaaged
Tensile strength~1150–1350MPaRepresentative; verify product form and condition
Fracture toughnesshighheat-treatment dependent
Hardenabilityhighthick sections

Conditions

reference

Representative supplied condition

Condition not fully specified in the source record.

03

Processing and use

Processing

  • Product form, thermal history and manufacturing route materially affect performance.

Applications

  • Landing-gear components
  • Large forgings
  • High-strength airframe fittings

Selection considerations

  • Use the current governing standard and supplier certification for design or procurement.

04

Standards and related materials

Standards and designations

SystemDesignationNote
AMS7025 / 7026product dependent
IndustryTi-5553

05

Sources and context

Sources

Confirm the applicable specification, product form and condition before using values for design or procurement.

Supply and sustainability

Availability and lead time depend on grade, product form, certification and regional supply chain.

Segregated recovery and closed-loop recycling improve material efficiency where practical.