Load Carrying Capabilities Of Refractory Alloys For Space Reactor Power Applications
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Load-carrying Capabilities of Refractory Alloys for Space Reactor Power Applications
To achieve sufficient thermodynamic efficiency, space nuclear power systems must operate above 1000°C. A quantitative evaluation of the existing mechanical properties data for the refractory alloys relevant to space nuclear power systems design lifetimes up to seven years at temperatures up to 1400°C is being conducted. The most important properties for space nuclear power systems are long-term high-temperature (>1000°C) creep strength and ductility, low-temperature (