Advanced refractory alloy corrosion loop program Quarterly progress report, 15 Jan. 1970 - 15 Apr. 1970
Operation and evaluation of Rankine system corrosion test loop based on refractory alloys
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Operation and evaluation of Rankine system corrosion test loop based on refractory alloys
Creep test data on refractory metal alloys for use in spacecraft power supply systems
Emerging operational environments, such as the lunar surface, present novel challenges for NASA and drive the need for advanced materials in applications like fission surface power systems. To address these demands, computational materials science is rapidly evolving to augment or replace costly and hazardous empirical testing. Although materials selection at NASA remains predominantly experimentally driven, advanced simulation methodologies are being steadily integrated into the engineering lifecycle. This work details the application of multiscale simulation techniques—including first-principles calculations, CALPHAD, dislocation dynamics, and molecular dynamics—at NASA's Ames Research Center to evaluate advanced materials for extreme environments. First, we present contributions to the Space Nuclear Propulsion Project. Be-cause propellant channel coatings in nuclear thermal rockets must withstand high-pressure, high-temperature hydro-gen, optimizing these materials is critical. First-principles calculations were employed to establish a rigorous quantitative and qualitative understanding of the behavior of the refractory carbides ZrC, NbC, and their mixtures in high-enthalpy hydrogen environments. This necessitated the generation of high-fidelity thermodynamic models for both stoichiometric and carbon-depleted carbides, both with and without the presence of hydrogen. Furthermore, we highlight efforts under the Refractory Alloy Additive Manufacturing Build Optimization (RAAMBO) project, where existing and novel alloy compositions were assessed for additive manufacturing printability and subsequent performance in applications such as heat pipes and rocket nozzle extensions. This was accomplished through a comprehensive multiscale simulation framework that bridged the gap from the nanometer to the millimeter scale. Across both initiatives, rigorous validation against empirical data was prioritized. By systematically employing a verified and validated computational frame-work, we demonstrate how simulation effectively supports multidisciplinary engineering efforts, builds project-wide confidence, and drives critical materials development.
Long-time creep data on refractory metal alloys for advanced space power systems
Fatigue data for refractory molybdenum-base alloys subjected to elevated temperatures in ultrahigh vacuum environment
Creep analysis of refractory metal alloys at high temperatures under ultrahigh vacuum conditions
Evaluation of refractory tantalum-, tungsten-, niobium-, and molybdenum based alloys for space power systems applications
Creep tests of arc-cast and vapor deposited tungsten, molybdenum alloys, niobium, and tantalum base alloys for use in advanced power systems
Creep testing data and machine reliability for high-temperature long-time tests on niobium, tungsten, and rhenium alloys
Corrosion resistance of niobium and tantalum base alloys to refluxing potassium
Long time creep test data on molybdenum base alloys, tantalum base alloys, and vapor deposited tungsten
Molybdenum base alloys and tantalum base alloys creep tested in vacuum environment at elevated temperatures
Development engineering for Rankine system corrosion test loop, and specimens preparation for tantalum alloy capsule tests
Creep tests of molybdenum base TZC, TZM alloys tantalum base T-111 and Astar 811C in vacuum environments
Fabrication of T-111 Rankine system corrosion test loop using tantalum alloy capsules filled with alkali metals
Creep tests of molybdenum alloys, and tantalum alloys
Instrumentation and performance of Rankine cycle corrosion test loop with alkali metal
Purification of alkali metals, and progress in developing Rankine system corrosion loop