Products
Contact Us
15 5 Stainless Suppliers
Keywords:
Category:
Product Details
15-5 PH stainless steel is an aerospace-oriented precipitation-hardening grade where material condition, heat treatment, and traceability can matter as much as the nominal chemistry. Also identified as UNS S15500, this martensitic PH stainless steel was developed as a modification of 17-4 PH to improve transverse toughness, ductility, and property uniformity, particularly in larger sections. For procurement teams, the key question is not simply whether a supplier stocks 15-5 PH, but whether the material can be supplied in the required condition with the documentation and traceability expected for aerospace applications.
Specification clarification: The designation should be written as 15-5 PH or 15-5PH, not simply “15 5.” For purchasing documents, use the full designation together with UNS S15500 and the applicable material specification to reduce the risk of grade confusion.
15-5 PH: The Aerospace Variant of the 17-4 PH Family
15-5 PH is a martensitic precipitation-hardening stainless steel containing approximately 15% chromium, 5% nickel, and copper as a major precipitation-hardening element. Its composition and refined processing route give it a useful combination of high strength, corrosion resistance, toughness, and dimensional stability after aging.
The major procurement distinction from 17-4 PH is not simply a higher strength level. 15-5 PH was developed to provide improved transverse toughness and ductility, together with better property uniformity in larger cross-sections. This makes it attractive when a component must combine high strength with resistance to cracking or notch-related failure.
| Property | 15-5 PH | Procurement Meaning |
|---|---|---|
| UNS designation | S15500 | Use with the specification on the purchase order |
| Material family | Martensitic precipitation-hardening stainless | Strength is developed through aging |
| Relation to 17-4 PH | Modified 17-4 PH grade | Selected when transverse toughness and uniformity are important |
| Typical sectors | Aerospace, valves, pumps, structural components | High-strength applications with controlled material requirements |
Why 15-5 PH Is Used for Aerospace Structural Parts
Aerospace components often require a combination that is difficult to achieve with conventional stainless grades: high yield strength, useful corrosion resistance, controlled heat-treatment response, and adequate toughness through the section. 15-5 PH addresses this combination more directly than ordinary austenitic or martensitic stainless grades.
Typical applications include structural aircraft components, shafts, gears, fasteners, hydraulic components, pump parts, and valves. In valve and actuator applications, the precipitation-hardening response allows engineers to select a condition according to the required balance between strength, hardness, ductility, and toughness.
Procurement rule: Do not approve a material only from the words “15-5 PH stainless.” The purchase specification should identify the UNS number, product form, applicable AMS or ASTM specification, supply condition, aging condition when required, heat number, test requirements, and certification level.
Condition A vs H900-H1150: What Should the Supplier Deliver?
The normal starting condition for many 15-5 PH products is Condition A, meaning solution heat treated. Subsequent precipitation aging develops the final strength and hardness. Common aging conditions include H900, H925, H1025, H1075, H1100, and H1150.
The condition is not a minor labeling detail. Lower-temperature aging such as H900 produces very high strength and hardness, while higher-temperature aging progressively reduces strength and hardness and generally provides greater ductility and toughness. Therefore, the correct condition should be specified according to the component design rather than selected solely because it provides the highest hardness.
| Condition | Approx. Aging Temperature | Typical Strength Trend | Typical Hardness Trend |
|---|---|---|---|
| Condition A | Solution treated | Lower than aged conditions | Relatively low |
| H900 | 900°F / 482°C | Very high | About 40–47 HRC depending on product form/specification |
| H1025 | 1025°F / 552°C | High | Approximately mid-30s HRC |
| H1075 | 1075°F / 579°C | Moderately high | Approximately low-30s HRC |
| H1150 | 1150°F / 621°C | Lower than H900 | Approximately high-20s to mid-30s HRC |
For H900, a practical purchasing reference is around 44 HRC, but the actual acceptance range depends on the product form and governing specification. For example, published data for sheet and plate can show a broader H900 range than bar. The supplier should therefore report the hardness against the applicable specification rather than treating one nominal HRC number as universal.
AMS 5659: The Certification Gate for Aerospace Supply
For aerospace procurement, AMS 5659 is an important specification to verify when purchasing applicable 15-5 PH long-product forms such as bars, forgings, rings, and related products. Sheet, strip, and plate may instead fall under AMS 5862. The correct AMS document therefore depends on the product form and purchasing requirement.
A supplier claiming aerospace capability should be able to identify exactly which specification covers the quoted product. A generic “15-5 PH certificate” is not equivalent to certification against the required aerospace specification.
| Procurement Item | What to Verify |
|---|---|
| Grade identity | 15-5 PH / UNS S15500 |
| Product form | Bar, forging, ring, sheet, strip, plate, or other specified form |
| Aerospace specification | Applicable AMS specification, such as AMS 5659 or AMS 5862 |
| Heat treatment | Condition A or specified H condition |
| Material test certificate | Chemistry, mechanical properties, hardness, heat-treatment condition, and heat number |
| Traceability | Mill heat and lot identification maintained through shipment and certification |
What Aerospace Buyers Should Request from 15-5 PH Suppliers
The supplier qualification process should begin before the purchase order is released. Ask for a sample MTC or certification package showing how the material identity, heat number, specification, heat treatment, and mechanical test results are recorded.
For aerospace-related applications, traceability should remain intact from the supplied material back to the original heat or melt. This is particularly important where customer specifications require controlled melt practice, remelting, testing, or additional quality documentation.
Supplier qualification checklist
✓ Confirm UNS S15500 against the purchase specification.
✓ Confirm the exact AMS specification for the product form.
✓ Specify Condition A or the required H900–H1150 condition.
✓ Request chemistry and mechanical-property results on the MTC.
✓ Verify heat/lot traceability and identification marking.
✓ Confirm whether additional aerospace quality or inspection documents are required.
15-5 PH Supply Forms and Practical Sourcing
15-5 PH can be supplied in several forms, including bar, plate, sheet, strip, forgings, rings, and other product forms depending on the applicable specification and mill capability. For aerospace machining, bar and forging products are particularly important, while sheet and plate requirements should be checked against the corresponding aerospace material specification.
When the finished component requires machining followed by aging, Condition A material can provide a useful starting point. When the customer requires a finished mechanical-property condition, the purchase order should explicitly state the required H condition rather than leaving the heat treatment to supplier interpretation.
For procurement teams comparing specialty stainless steel products, Teda Ganghua can support material sourcing with specification-based requirements, dimensional processing, inspection coordination, and documentation review. For aerospace-oriented grades, the inquiry should include the UNS designation, product form, dimensions, condition, applicable standard, quantity, and certification requirements so the supply route can be evaluated correctly.
15-5 PH vs 17-4 PH: A Procurement-Level Distinction
Both grades belong to the precipitation-hardening stainless family and can achieve high strength through aging. The reason to specify 15-5 PH is often related to toughness, transverse properties, and property uniformity rather than simply maximum strength.
| Factor | 15-5 PH | 17-4 PH |
|---|---|---|
| Family | Martensitic precipitation-hardening stainless | Martensitic precipitation-hardening stainless |
| Primary distinction | Modified composition and refined structure for improved transverse properties | Widely used general PH stainless grade |
| Aerospace relevance | Strong, especially where toughness and traceability are specified | Very broad aerospace and industrial use |
| Selection priority | Strength plus transverse toughness and uniformity | Application-dependent strength, corrosion resistance, and availability |
FAQ: 15-5 PH Stainless Steel Suppliers
Is 15-5 PH the same as UNS S15500?
Yes. 15-5 PH is commonly identified by UNS S15500. Procurement documents should preferably state both the alloy designation and UNS number, together with the governing product specification.
What condition is 15-5 PH normally supplied in?
Condition A is a common starting condition for precipitation-hardening products. Aging conditions such as H900, H925, H1025, H1075, H1100, and H1150 are then selected to obtain the required mechanical-property balance.
Is H900 approximately 44 HRC?
Approximately, yes, as a practical reference. Published values vary with product form and specification, with H900 commonly falling around 40–47 HRC for sheet/plate and around 40 HRC in some bar specifications. The applicable specification should control the acceptance value.
What is AMS 5659 used for?
AMS 5659 covers applicable 15-5 PH long-product forms such as bars, forgings, rings, and related products. Sheet, strip, and plate may instead be covered by AMS 5862, so the product form must be confirmed before selecting the standard.
Why is 15-5 PH attractive for aerospace components?
It combines high precipitation-hardened strength with corrosion resistance and improved transverse toughness and ductility compared with the conventional 17-4 PH reference grade. For aerospace procurement, these material properties must be paired with the correct specification, heat treatment, testing, and traceability documentation.


Product Inquiry
Relevant Products