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  • Home
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    • Stainless Steel
      • 430 / 1.4016
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      • 316l-14404/
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      • 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
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      • 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
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      • Alloy 59 / 2.4605
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      • Alloy 602CA / 2.4633
      • Alloy X / 2.4656 / UNS N06002
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      • Nivaflex / 2.4782
      • Alloy C276 / 2.4819
      • Alloy 601 / 2.4851
      • Alloy 625 / 2.4856
      • Alloy 825 / 2.4858
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17-4 PH / 1.4542

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17-4 PH / 1.4542

17-4PH is a well-established precipitation hardening martensitic stainless steel capable of achieving very high strength and hardness after a relatively simple heat treatment. It offers excellent corrosion resistance combined with a structured range of mechanical property levels depending on the precise heat treatment applied.

The materials can be readily machined and fabricated in the softer tempers and can then be heat-treated to exceptional strength and dimensional stability. 17-4PH is widely used in the chemical, petrochemical, offshore, paper, and aerospace industries making best use of its outstanding corrosion resistance, wear resistance, strength and hardness.

  • Material
  • Application
  • Composition
  • Properties
  • Material
  • Application
  • Composition
  • Properties

Specifications

UNS S17400

AMS 5643, AMS 5604, ASTM A564

Main fields of application of 1.4542

Surgical and dental instrument, screwdriver.

17- 4 retains a high strength of precipitation hardening stainless steels a majority of applications are within the aerospace sector and OAG applications

Valves and engine components

Turbine blades

Gears

Shafts

Aircraft structures

Chemical composition of 1.4545

Cr15,0 - 17,0
Ni3,0-5,0
Cu3,0-5,0
Cmax 0,070

Characteristics of 1.4542

annealedspecification values
tensile strength Rm1000-1100 MPa
elongation A5-8
Aged at 480 ⁰Cspecification values
tensile strength Rm1150 – 1350 MPa
elongation A7 - 15

Heat treatment

Alloy 17-4PH is provided in the solution-annealed condition (Condition A). Mechanical properties may be improved by subsequent age hardening treatments. These aging treatments are commonly described as conditions H900, H1025, H1075, H1150, H1150M and H1150D.

Mechanical Properties

ConditionUTS0.2% YieldElongationReduction of areaHardness Brinel
H900190.000170.0001040388
H1025155.000145.0001245331
H1075145.000125.0001345311
H1150135.000105.0001650277
H1150m115.00075.0001855255
H1150-D125.000105.0001650255

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