The most commonly used alloys for rocket engine modules are those that can withstand extreme temperatures, high pressure, and aggressive chemical environments. Based on NewayAero's material offerings, the following alloys are typically favored in rocket engine applications:
Inconel 718: Known for its excellent high-temperature strength and corrosion resistance, Inconel 718 is commonly used for combustion chambers, turbine blades, and other components in rocket engines.
Inconel 625: This alloy offers excellent resistance to high-temperature oxidation, making it suitable for nozzle liners, exhaust ducts, and high-stress components.
Inconel X-750: Often used in gas turbines, this alloy can also be found in rocket engine components, mainly where thermal fatigue resistance is critical.
Inconel 939: Used in high-performance engine components, Inconel 939 provides good oxidation resistance at high temperatures and is often used in the combustion zone.
CMSX-10, CMSX-486, CMSX-4: Advanced single-crystal superalloys highly resistant to thermal creep and oxidation. Single-crystal components, such as turbine blades in rocket engines, benefit from these alloys' enhanced mechanical properties at elevated temperatures.
Rene 104 and Rene 108: Due to their exceptional thermal and mechanical properties, these high-performance alloys are often used in the most demanding parts of a rocket engine, such as nozzle extensions and turbine components.
Hastelloy X: Renowned for its high-temperature stability and resistance to oxidation, Hastelloy X is a common choice for high-stress, high-temperature applications, such as rocket nozzles and engine combustion zones.
Hastelloy C-276: While primarily used in chemical processing, this alloy is also suitable for rocket engine components that resist high-temperature corrosion and oxidation.
Ti-6Al-4V: Although not as heat-resistant as nickel-based alloys, titanium alloys such as Ti-6Al-4V are used in certain components of rocket engines due to their excellent strength-to-weight ratio. These are typically used for less extreme temperature zones like the engine's structure.
Monel K500: Monel alloys, such as Monel K500, are used in certain parts of the engine that require excellent corrosion resistance and moderate high-temperature performance.
Stellite 6B: Known for its wear resistance, Stellite alloys are sometimes used in components like valve seats or other parts that require wear and corrosion resistance at high temperatures. However, they are less common in rocket engines than other alloys.
Thermal Fatigue Resistance: Rocket engine modules experience extreme thermal cycling, which makes alloys like Inconel 718 and CMSX series highly desirable due to their excellent resistance to thermal fatigue.
Oxidation and Corrosion Resistance: High-temperature alloys like Inconel and Hastelloy are chosen for their superior ability to resist oxidation and corrosion in the harsh rocket engine environment.
Strength-to-Weight Ratio: For structural components, titanium alloys are favored due to their lightweight yet strong properties, helping to reduce the overall mass of the engine.
These alloys' specific properties—such as high-temperature strength, oxidation resistance, and fatigue resistance—make them critical for the demanding performance requirements of rocket engine modules.