UNS N07001 Specifications | |
Material | Standard |
Sheet, Plate, & Strip | AMS 5544 |
Billet, Rod, & Bar | AMS 5704, AMS 5706, AMS 5707, SB 647, B 637 |
Bare Welding Rods & Wire | AMS 5828 |
Forgings | AMS 5704, AMS 5706, AMS 5707, Sb 637, B637 |
Waspaloy® is a nickel-based superalloy renowned for its exceptional strength and oxidation resistance at high temperatures, typically up to 980°C (1800°F). Its superior performance makes it a critical material in aerospace and power generation industries. In aerospace, Waspaloy® is commonly used in jet engine components, turbine disks, and combustion chambers. For fasteners, Waspaloy® is favored in environments requiring high tensile strength, corrosion resistance, and heat tolerance—such as in gas turbines, space systems, and high-performance aircraft. Its machinability and resistance to creep deformation under stress also make it ideal for critical structural and fastening applications in extreme conditions.
Contact Nickel Systems today to request a quote on Waspaloy® fasteners for your next aerospace project.
Get our technical data and specifications for Waspaloy® below.
Download the Haynes® Waspaloy® Technical Data Sheet. This technical data is specifically related to Haynes® Waspaloy® material. If you require this specific material, you must request it at the time of quotation. Haynes® is a trademark of Haynes International. Waspaloy® is a trademark of United Technologies Corporation. For more information on this mill, please visit the website of Haynes International.
UNS N07001 Specifications | |
Material | Standard |
Sheet, Plate, & Strip | AMS 5544 |
Billet, Rod, & Bar | AMS 5704, AMS 5706, AMS 5707, SB 647, B 637 |
Bare Welding Rods & Wire | AMS 5828 |
Forgings | AMS 5704, AMS 5706, AMS 5707, Sb 637, B637 |
UNS N07001 Chemical Composition | ||
Element | % Composition | Description |
Nickel | ~54% | Remainder |
Chromium | 18-21% | Range |
Cobalt | 12-15% | Range |
Molybdenum | 3.5-5% | Range |
Titanium | 2.75-3.25% | Range |
Iron | 2% | Max |
Aluminum | 1.2-1.6% | Range |
Manganese | 1% | Max |
Silicon | 0.75% | Max |
Copper | 0.5% | Max |
Carbon | 0.03-0.10% | Range |
Phosphorus | 0.03% | Max |
Sulfur | 0.03% | Max |
Zirconium | 0.02-0.12% | Range |
Boron | 0.003-0.01% | Range |
These values are based on the ASTM standard. Specific trademarked materials will fall somewhere within this standard. If you need a specific trademarked material or chemical composition, you must request this at the time of quotation | ||
Waspaloy®'s Physical Properties | |||
Density | |||
RT | 0.296 lb/in³ | RT | 8.20/g/cm³ |
Melting Range | |||
2,425 - 2,475℉ | 1,330 - 1,360℃ | ||
Thermal Conductivity | |||
Temperature, ℉ | Btu-in/ft²-hr-℉ | Temperature, ℃ | W/m-℃ |
400 | 88 | 200 | 12.6 |
800 | 112 | 400 | 15.7 |
1,000 | 125 | 600 | 19.1 |
1,200 | 139 | 700 | 20.9 |
1,400 | 152 | 800 | 22.7 |
1,600 | 167 | 900 | 24.5 |
Mean Coefficient of Thermal Expansion | |||
Temperature, ℉ | μin/in-℉ | Temperature, ℃ | x10^-6 m/m-℃ |
70 - 800 | 7.6 | 20 - 500 | 13.9 |
70 - 1,000 | 7.8 | 20 - 600 | 14.3 |
70 - 1,400 | 8.4 | 20 - 800 | 15.4 |
70 - 1,600 | 8.9 | 20 - 900 | 16.4 |
70 - 1,800 | 9.7 | 20 - 1,000 | 17.8 |
Dynamic Modulus of Elasticity | |||
Temperature, ℉ | x10^6 psi | Temperature, ℃ | GPa |
70 | 30.9 | 20 | 213 |
400 | 29.5 | 200 | 204 |
800 | 27.7 | 400 | 192 |
1,000 | 26.7 | 600 | 180 |
1,200 | 25.6 | 700 | 172 |
1,400 | 24.3 | 800 | 164 |
1,800 | 21.1 | 1,000 | 146 |
UNS 07001 Mechanical Properties | |
Tensile Strength | 160ksi / 1,100MPa |
Yield Strength | 110ksi / 760MPa |
Elongation in 2 in. Min, | 15% |
Reduction of Area, Min | 18% |
Brinell Hardness Min. | 310 |
These are the minimum required values for the ASTM B637 standard for rod and bar in UNS 07001 material. | |
Waspaloy® is a nickel-based, precipitation-hardened, austenitic, superalloy. Its primary chemical elements are nickel, chromium, molybdenum and cobalt. It maintains excellent performances at elevated temperatures. It is designed to be used in aerospace, power generation, and other high-temperature, high-stress environments.
Check out our Waspaloy® Chemical Composition Breakdown.
Beyond the typical elements connected with high nickel alloys, Waspaloy® has several unique elements that increase its performance in extreme environments.
Waspaloy’s® Key Elements and Their Effects | ||
Element | Primary Role | Key Effect on Performance |
Nickel (Ni) | Matrix base | High-temp strength, ductility, oxidation resistance |
Chromium (Cr) | Oxidation resistance | Forms protective Chromium-oxygen layer |
Cobalt (Co) | Solid solution & γ’ stabilizer | Boosts high-temp strength & phase stability |
Molybdenum (Mo) | Strengthener | Improves creep resistance & grain stability |
Aluminum (Al) & Titanium (Ti) | Precipitation hardeners | Form γ’ phase which is the core of Waspaloy’s strength |
Boron (B) & Zirconium (Zr) | Grain boundary modifiers | Enhance ductility, toughness, and creep resistance |
Waspaloy® is designed for use in extreme environments. Check out a description of its performance below.
Waspaloy® fasteners exhibits excellent oxidation resistance at elevated temperatures, up to 980℃ (1,800℉). It forms a stable, protective oxide layer that prevents degradation in hot gas environments.
Waspaloy® offers good resistance to mildly to moderately corrosive environments, especially under aerospace and turbine service conditions. However, it is not primarily designed for aqueous or marine corrosion, unlike stainless steels or corrosion-resistant nickel alloys.
Waspaloy® is engineered specifically for severe and mechanical environments, such as those found in gas turbines and high-performance aircraft. It maintains high strength and structural stability even under creep, thermal fatigue, and oxidizing hot gases.
