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Fluid Dynamic Mass Gauging (FDMG) is a microgravity-compatible system that applies principles of fluid dynamics, the ideal gas law, and thermodynamics to determine the volume of an incompressible fluid within a tank by measuring the compressible volume in the same tank. In a simplified embodiment, the determination of the remaining volume of the fluid within a given storage tank can be calculated from a time measurement of a pressure change during a filling or venting process applied to the storage tank. The process may be automated and features low mass and volume requirements, enabling its use in any gravitational or inertial environment with minimal hardware modifications. The novel system can determine the volume of a non-condensing, incompressible fluid within a rigid tank of known or unknown volume without requiring the use of bulky equipment in microgravity locations with fixed or limited free space.

Dispersion Enhanced Aluminum Alloys improve the additive manufacturing performance of high-strength aluminum alloys by modifying the alloy powder with uniformly dispersed nano-sized ceramic particles. Building on the dispersion and acoustic mixing methods developed during the creation of NASA Glenn's GRX-810 technology, researchers use an acoustic field to attach nanoscale alumina dispersoids to the surface of each aluminum alloy powder particle. During mixing, acoustic energy creates rapid micro-vibrations that cause the alumina particles to collide with the metal powder, embed against its surface, and distribute into a uniform shell that surrounds each particle. This produces a composite powder in which every aluminum particle carries its own evenly spaced ceramic nucleation sites. When the composite powder is delivered into an additive manufacturing process such as laser powder bed fusion or directed energy deposition, the aluminum alloy melts while the alumina dispersoids remain solid due to their significantly higher melting temperature. As the molten pool flows and mixes, the dispersoids remain suspended throughout the liquid region. During solidification, these solid particles interrupt grain growth and serve as nucleation points that promote the formation of fine equiaxed grains. This refined microstructure distributes thermal stresses more uniformly and disrupts the crack initiation mechanisms that typically occur in high-strength alloys like AA 2050. By stabilizing the alloy during solidification, the technology enables these advanced materials to be printed with greater reliability, improved geometric control, and more consistent mechanical behavior across the final product. The enhanced alloy technology is available for patent licensing.

NASA's ODS-MEA maintains properties up to 1100°C and is not susceptible to deleterious phase changes when exposed to extreme temperatures, an issue ubiquitous to Ni- based superalloys such as Inconel-625 and Inconel-718. Yttria particles are dispersed throughout the alloy to maximize strength and creep resistance at high temperatures using a novel fabrication technique. This technique employs an acoustic mixer to stir nano-scale Yttria oxide powder within a metallic matrix powder, creating a film of Yttria surrounding the larger metallic powder particles. Solid components are then produced from this mixture via SLM, during which the laser disperses the Yttria particles throughout the microstructure. Ultimately, the process eliminates the many expensive and time-consuming steps in the production of ODS alloys via traditional mechanical alloying. NASA's process has been shown to fabricate components with 10x improvement in creep rupture life at 1100°C and provides a 30% increase in strength over what is currently possible with 3D printed parts. The new ODS-MEA composition may find applications where ODS alloys are currently used (e.g., those involving extreme thermal environments). Applications may also include areas where such properties are desirable but the resource-intensive nature and/or inability to produce highly complex geometries via conventional processes ultimately renders their use uneconomical or infeasible. Such uses include gas turbine components (for which increasing inlet temperature enables improved efficiency) for power generation, propulsion (rockets, jet engines, etc.), industrial processes, nuclear energy applications, and sample preparation equipment in the mining and cement production industries, among many others.