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ALUMINUM ALLOY

Aluminum 2024-T3

UNS A92024, AMS 4037
Aluminum AlloyLow Cost
DENSITY
3 kg/m³
MELTING POINT
502°C
TENSILE STRENGTH
483 MPa
MAX SERVICE TEMP
175°C

Aluminum 2024-T3 is a aluminum alloy used in aerospace applications. Melting point: 502 °C. Tensile strength: 483 MPa.

ABOUT ALUMINUM 2024-T3

Aluminum 2024-T3 is a high-strength aluminum-copper alloy that has been the workhorse of aerospace structures since the 1930s. It offers an excellent strength-to-weight ratio and good fatigue resistance, making it ideal for aircraft fuselage skins and wing structures. It is commonly clad with pure aluminum (Alclad) for corrosion protection.

CHEMICAL COMPOSITION

Al 90.7-94.7%, Cu 3.8-4.9%, Mg 1.2-1.8%, Mn 0.3-0.9%

ROCKET & SPACECRAFT APPLICATIONS
Aircraft fuselage skins
Wing structures
Payload fairings
Interstage adapters
Launch vehicle secondary structures
MANUFACTURING PROPERTIES
CORROSION RESISTANCE
Fair
WELDABILITY
Poor
MACHINABILITY
Good
COST RATING
Low
MECHANICAL PROPERTIES
DENSITY3 kg/m³
TENSILE STRENGTH483 MPa
YIELD STRENGTH345 MPa
STRENGTH-TO-WEIGHT173741 kN·m/kg
THERMAL PROPERTIES
MELTING POINT502 °C
MAX SERVICE TEMPERATURE175 °C
THERMAL CONDUCTIVITY121 W/m·K
THERMAL EXPANSION23.2 µm/m·K
COMPLETE SPECIFICATIONS
CATEGORYAluminum Alloy
DESIGNATIONSUNS A92024, AMS 4037
MANUFACTURERAlcoa / Arconic
DENSITY3 kg/m³
TENSILE STRENGTH483 MPa
YIELD STRENGTH345 MPa
MELTING POINT502 °C
MAX SERVICE TEMP175 °C
THERMAL CONDUCTIVITY121 W/m·K
THERMAL EXPANSION23.2 µm/m·K
CORROSION RESISTANCEFair
WELDABILITYPoor
MACHINABILITYGood
COST RATINGLow

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