: Data confirms that high-pressure hydrogen has minimal influence on the alloy’s fracture elongation (34–36%), demonstrating superior resistance to embrittlement compared to standard alloys.
: NASA HR-2 is a specialized superalloy developed to withstand the extreme conditions of liquid rocket engines (LREs). This paper explores its mechanical properties, including high yield stress (~95 ksi) and exceptional ductility in high-pressure hydrogen environments. hr2.zip
: Detailing the laser parameters used to achieve high densification levels. : Data confirms that high-pressure hydrogen has minimal
: NASA HR-2 is a mature and viable candidate for critical aerospace hardware, successfully combining printability with robust mechanical performance in hydrogen-rich atmospheres. : Detailing the laser parameters used to achieve
: Tensile testing conducted in pressurized gaseous hydrogen (GH2) at up to 5 ksi. Results & Discussion :
: Components in hydrogen-sensitive LREs are prone to hydrogen environment embrittlement. HR-2 was formulated as a promising solution for hardware produced via Laser Powder Bed Fusion (L-PBF) , a type of 3D printing that allows for complex geometries. Methodology :
: The alloy maintains an ultimate tensile stress of approximately 165 ksi.