Compatibility of Niobium Alloys and Superalloys in a Flowing He-Xe Power Conversion System

Proposed concepts for an ambitious mission to explore Jupiter’s three icy moons place significant demands on the various spacecraft systems. There are many challenges re lated to the high output power conversion systems being considered, and one example is the need to ensure system compatibility at all levels. The utilization of appropriate materials for component structures is important to ensuring long mission life. Re fractory metal alloys have attractive high -temperature properties in inert environments, but these alloys are sometimes susceptible to contamination. Potential material compatibility issues exist between refractory metal candidates and more conventional a lloys. Nb -1Zr has long been considered one of the most well characterized refractory alloys that is well suited for elevated -temperature use and liquid -metal compatibility. However, previous studies have suggested that niobium alloys can not co -exist in a closed system with traditional stainless steels or superalloys due to transport of contaminants. The relevance of this information to a proposed power conversion system is discussed. Also, experiments and fundamental calculations are being performed to determine contamination transport from candidate superalloys to Nb -1Zr in a closed system with an inert carrier gas. Potential protective schemes are explored to ensure system level compatibility between the refractory alloy Nb -1Zr and a nickel -based sup eralloy.