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  • Home
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    • Stainless Steel
      • 430 / 1.4016
      • 420 / 1.4021
      • 420 / 1.4034
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      • 420F / 1.4197
      • 304 / 1.4301
      • 305 / 1.4303
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      • 301LN / 1.4318 / UNSS30153
      • 316l-14404/
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      • 316L / 1.4435WCQ
      • 1.4435/1.4441WCQ+
      • 316LVM / 1.4441
      • 444 / 1.43521N
      • 321-14541
      • 13-8-ph-14534
      • XM-12 / 1.4545 / 15-5 PH
      • 17-4 PH / 1.4542
      • 316Ti / 1.4571
      • 309 / 1.4828
      • 314 / 1.4841
    • Special Stainless Steel
      • P2000 / 1.4452
      • 318LN / 1.4462
      • SUPER DUPLEX S32760 / F55 / 1.4501
      • 6Mo / 1.4529
      • Alloy 904L / 1.4539
      • Alloy 254 SMO / 1.4547 / UNS S31254
      • Alloy 31 / 1.4562
      • Alloy 24 / 1.4565
      • Alloy 800H / 1.4876
    • Nickel Alloys
      • Alloy 201 / 2.4068
      • Alloy 400 / 2.4360
      • Alloy C22 / 2.4602
      • Alloy 59 / 2.4605
      • Alloy C4 / 2.4610
      • Alloy 602CA / 2.4633
      • Alloy X / 2.4656 / UNS N06002
      • Alloy 617 / 2.4663
      • Alloy 718 / 2.4668
      • Nivaflex / 2.4782
      • Alloy C276 / 2.4819
      • Alloy 601 / 2.4851
      • Alloy 625 / 2.4856
      • Alloy 825 / 2.4858
    • Titanium Alloys
      • Ti Gr 1 / 3.7025
      • Ti Gr 2 / 3.7035
      • Ti Gr 4 / 3.7065
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      • Ti Gr 9 / 3.7194
      • Titan Grade 12 / 3.7105 / UNS N53400
      • 367 / Ti6AL7Nb
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    • Exotic Metals
      • P900 / 1.3816
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      • Invar 36 (FeNi36) / 1.3912
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XM-12 / 1.4545 / 15-5 PH

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  • Application
  • Composition
  • Application
  • Composition

XM-12 / 1.4545 / 15-5 PH

15-5PH is a variant of the older 17-4PH chromium-nickel-copper precipitation hardening stainless steel. Both alloys exhibit high strength and moderate corrosion resistance. High strength is maintained to approximately 600 degrees F. The 15-5 alloy was designed to have greater toughness than 17-4. This improved toughness is achieved by reduced delta ferrite content and control of inclusion size and shape. The fabrication characteristics of 15 – 5 PH are similar to those of other precipitation hardening grades; they can be age hardened by a single step, low temperature treatment.

Material Data Sheet

UNS S15500

AMS5658

AMS5659

ASTM 564

DFARS Compliant

AMS5862

AMS5562

Main fields of application of 1.4545

valve parts,

fittings and fasteners,

shafts,

gears,

chemical process equipment,

paper mill equipment,

aircraft components, 

nuclear reactor components.

Chemical composition of 1.4545

Cr14,0 - 15,5Si1,0
Ni3,5-5,5Mn1,0
Cu2,5-4,5P0,04
Cmax 0,07S0,03
Nb + Ta0,15 - 0,45

Heat treatment

The key to the properties of precipitation hardening stainless steels lies in heat treatment.

Heat treatments are used to strengthen 15-5 alloys. There are eight standard conditions for 15-5 stainless steel after treatment – H 900, H 925, H 1025, H 1075, H 1100, H 1150, H 1150+1150 and H 1150-M. Heat treating 15-5 PH follows the following steps:

Conditioning using austenite.

Air cooling, which turns the austenite into martensite.

Precipitation hardening until the desired condition is reached.

15-5 PH can be further heat-treated when in precipitation-hardened condition to provide improved resistance to stress corrosion cracking for high temperature applications. Fabrication is recommended after the metal has been heat treated to minimize distortion and stress

 

Mechanical Properties

ConditionUTSYield StrenghtElongationReduction of areaHardness BrinellHardness Rockwell
H900190.000170.000615388C40
H1025155.000125.000827331C35
H1075145.000125.000928311C32
H1150135.000105.0001130277C28
H1150m115.00075.0001435255

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