Alloy Geek Mar M 002 Standard
Mar M 002, a distinguished member of the Mar M family, represents the pinnacle of high-temperature alloy engineering. Engineered to perform exceptionally well in extreme environments, this alloy boasts a unique chemical composition and a remarkable set of properties that set it apart in the world of high-performance materials.
Chemical Composition of Mar M 002:
- Nickel (Ni): 39.0% - 45.0%
- Cobalt (Co): 10.0% - 12.5%
- Chromium (Cr): 7.0% - 9.0%
- Iron (Fe): 5.0% max
- Molybdenum (Mo): 4.0% - 6.0%
- Titanium (Ti): 0.5% - 1.0%
- Aluminum (Al): 0.1% - 0.5%
- Zirconium (Zr): 0.1% - 0.5%
- Carbon (C): 0.05% max
- Boron (B): 0.01% max
- Yttrium (Y): 0.1% - 0.5%
Exceptional High-Temperature Strength: Mar M 002 retains exceptional mechanical properties even in applications reaching extreme temperatures, making it a top choice for aerospace and industrial applications, especially those operating in temperatures of up to 2200°F (1200°C).
Superior Oxidation and Corrosion Resistance: With its high chromium and nickel content, this alloy demonstrates superior resistance to oxidation and corrosion, ensuring longevity in harsh, high-stress environments.
Excellent Fatigue Resistance: Mar M 002 exhibits exceptional fatigue resistance, making it suitable for components exposed to cyclic loading conditions.
Precipitation-Hardening Capability: The alloy is amenable to precipitation hardening, enabling the tailoring of mechanical properties to specific application needs.
Other Names for Mar M 002:
- Alloy M 002: A recognized reference in aerospace and engineering industries.
Unique Qualities of Mar M 002: What sets Mar M 002 apart from its counterparts is its extraordinary balance between high-temperature strength, resistance to oxidation and corrosion, and excellent fatigue resistance. This combination of properties makes it an invaluable material for the most demanding environments, where precision, reliability, and longevity are non-negotiable.
In applications spanning aerospace, industrial furnaces, and beyond, Mar M 002 plays a pivotal role in the construction of critical components that must endure extreme temperatures and oxidative conditions. Its ability to maintain structural integrity under these demanding circumstances makes it a material of choice for those seeking uncompromised performance in challenging applications.
XRF Samples are thinner samples approximately 1/4 inch thick. OES Standards are thicker in nature and are approximately 1 inch thick. Please Contact Us if you would like to know the specific dimensions of a sample.
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In summary, the main difference between a reference material and a certified reference material lies in the level of characterization, validation, and certification. CRMs have undergone a more comprehensive and rigorous testing process, resulting in certified values and uncertainties that can be confidently used for instrument calibration, quality control, and research. Reference materials, on the other hand, can provide a point of comparison but might not have the same level of certification and traceability as CRMs. When accuracy and traceability are critical, certified reference materials are preferred.