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X5CrNiCu15-5 | FE-PM1802 Material Datasheet

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Material Description

Material Number Material Number (single) Standard Standard Status Country VDA 231-106 classification
FE-PM1802 (DIN EN 2815 : 2009-11) FE-PM1802 DIN EN 2815 : 2009-11 Valid Germany 1.1 1)
1) Remark: Stainless, precipitation hardened high strength steel FE-PM1802 (X5CrNiCu15-5) with a minimum tensile strength of 965 MPa in the form of bars up to 200mm for general aerospace applications.

Chemical Composition

C [%] Cr [%] Cu [%] Mn [%] Mo [%] Ni [%] P [%] S [%] Si [%] Nb+Ta [%]
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Mechanical Properties

Semi-finished Product Condition Nominal Size [mm] Temperature [°C] Specimen Direction Tensile Strength [MPa] Yield Strength (0.2% offset) [MPa] Elongation A [%] Reduction of Area [%] Hardness HB | HBW
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Physical Properties

Temperature [°C] Density [g/cm³] Young's Modulus [GPa] Mean Coefficient of Thermal Expansion [10^-6*K^-1] Thermal Conductivity [W/(m*K)] Specific Electrical Resistance [µΩm] Mean Specific Heat Capacity [kJ/(kg*K)] Magnetizeability
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Welding and Joining

Procedure Welding and Joining - Evaluation Added Materials
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Toughness Data (Impact)

Semi-finished Product Condition Nominal Size [mm] Temperature [°C] Specimen Shape Specimen Direction Notch Impact Energy [J]
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Heat Treatment

Heat Treatment Step Temperature [°C] Holding Time [h] Medium
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Cross Reference

Material Name Country Standard
1.4545 Germany WL 1.4545
X5CrNiCu15-5 Europe EN 2815
S15500 USA UNS 1)
XM-12 USA AISI 2)
A564 Type XM-12 USA ASTM A564 2)
15Cr-4.5Ni-0.30Cb USA AMS 5659 2)
15Cr-4.5Ni-0.30Nb USA AMS 5659 2)
EN 2815 W 3)
EN 2815 U 3)
ASNA 3294 Europe Airbus 4)
ASNA 3297 Europe Airbus 4)
ASNA 6116 Europe Airbus 4)
ABS5750 Europe Airbus 4)
ABS5455 Europe Airbus 4)
IPS01-04-003-02 Europe Airbus 4)
HMDM0022 Europe Safran Nacelles (Aircelle) 4)
D1 4426 (PC660) USA Boeing 4)
EMCM-001-1013 Canada Bombardier 4)
LAT1-9037 Germany Liebherr-Aerospace 4)
1) Source: Stahlschlüssel 2019, Verlag Stahlschlüssel Wegst GmbH, Marbach
2) Source: Metals & Alloys in the Unified Numbering System, SAE/ASTM, 11th Edition, 2008
3) Source: EN 2815
4) Source: Aerospace Materials, voestalpine BÖHLER Aerospace GmbH & Co KG, Kapfenberg/Austria, 2022

Producer/Supplier/Trade names

Tradename Supplier
15-5PH Aircraftmaterialsuk.com Ltd, Stokenchurch
15-5 PH AK Steel International B.V., Köln 1)
ATI 15-5 ATI Europe, Düsseldorf 1)
X 15 U 5 W AUBERT & DUVAL Deutschland GmbH, München 1)
BGH 4545 BGH Edelstahl Siegen GmbH 1)
Aerodur 4545 Deutsche Edelstahlwerke Specialty Steel GmbH & Co. KG, Siegen 1)
15-5 PH Enpar Sonderwerkstoffe GmbH, Gummersbach 1)
Puro 1.4545 Remystahl GmbH & Co. KG, Hagen 1)
Irrubigo 4545 ESU Schmidt + Clemens GmbH + Co. KG, Edelstahlwerk Kaiserau, Lindlar 1)
X5CrNiCu15-5 Schmiedewerke Gröditz GmbH, Gröditz 1)
N701 voestalpine High Perfomance Metals Deutschland GmbH, Düsseldorf 1)
N701 voestalpine High Perfomance Metals Deutschland GmbH, Düsseldorf 1)
1) Source: Stahlschlüssel 2019, Verlag Stahlschlüssel Wegst GmbH, Marbach

Material Compliance

REACh RoHS
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Linear-elastic

Temperature [°C] Young's modulus [GPa] Bulk modulus [GPa] Shear modulus [GPa] Poisson's ratio
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Alternating stress

Temperature [°C] Stress ratio Mean stress [MPa] Alternating stress [MPa] Cycles
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Yield strength

Temperature [°C] 0.1% Proof strength [MPa] 0.2% Proof strength [MPa] Yield strength [MPa]
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Electrical resistivity

Temperature [°C] Specific electrical resistance [µΩm]
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Specific heat

Temperature [°C] Specific heat [kJ/(kg*K)]
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Density

Temperature [°C] Density [g/cm³]
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Tensile strength

Temperature [°C] Tensile strength [MPa]
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Thermal conductivity

Temperature [°C] Thermal conductivity [W/(m*K)]
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Classification

WIAM Material Treatment Semi-finished product Dimension [mm] Load type Failure criteria Rolling direction Maximum stress [MPa] Strain at maximum stress [%] Source description
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Designation

Designation Material number Source
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Yield strength

Temperature [°C] 0.1% Proof strength [MPa] 0.2% Proof strength [MPa] Yield strength [MPa]
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Tensile strength

Temperature [°C] Tensile strength [MPa]
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Classification

WIAM Material Treatment Semi-finished product Dimension [mm] Load type Failure criteria Rolling direction Maximum stress [MPa] Strain at maximum stress [%] Source description
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Yield strength

Temperature [°C] 0.1% Proof strength [MPa] 0.2% Proof strength [MPa] Yield strength [MPa]
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Tensile strength

Temperature [°C] Tensile strength [MPa]
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Classification

WIAM Material Treatment Semi-finished product Dimension [mm] Load type Failure criteria Rolling direction Maximum stress [MPa] Strain at maximum stress [%] Source description
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