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MCS-8
Modular Container System Preserves Sample Integrity
The Astromaterials Acquisition and Curation Office (AACO) at NASA Johnson Space Center currently curates 500 milligrams of the regolith sample from the Asteroid Ryugu that was collected by the Japan Aerospace and Exploration Agency’s Hayabusa II spacecraft and returned to Earth in 2021. In September 2023, NASA’s OSIRIS-REx spacecraft returned 70 grams of regolith collected from the surface of Asteroid Bennu. These astromaterial sample collections are stored and handled in gloveboxes and desiccators that are continuously purged with ultrapure nitrogen in order to minimize contamination and alteration of extraterrestrial samples from terrestrial environments. For collaborative astromaterial sample research conducted outside of the AACO, a need emerged for a sample container system suitable for global transport, capable of maintaining the same low-oxygen envi-ronment as laboratory gloveboxes. Thus, the MCS was developed. MSC’s of different sizes (2, 4, and 8-inch sample container models) have been developed to store contact pads and bulk samples from NASA missions, including the OSIRIS-REx Asteroid Bennu mission. MCS’s are designed with seal profiles to prevent oxygen from seeping into the sample container. Additionally, the MCS uses a sample container form-factor that optimizes favorable nitrogen to oxygen gas ratios. The final prototypes were tested and verified using optochemical sensors to measure trace oxygen levels within the sealed containers. The Modular Container System (MCS) could fill a critical gap in the existing high-purity logistics and storage market in its ability to provide a passively maintained, verifiable, multi-year, glovebox-level low-oxygen environment in a portable robust form-factor. Although this technology was originally developed for astromaterial transport and storage, commercial applications may also exist in biopharmaceutical/ bio-banking, microelectronics/ semiconductor, and other industries.
materials and coatings
Diamond Maker Technology Simulates Alien Geology in Laboratories
Given the significant impact of fO2 on material properties, it is important to perform studies at fO2 values relevant to the sample of interest. However, current systems used to control fO2 in solid media assemblies (e.g., sliding sensors, graphite capsule buffering) have limited ability to produce the wide fO2 ranges necessary to simulate more extreme planetary interiors. NASA's fO2 control system implements a modified double capsule design that utilizes a wide range of solid metal-oxide buffers to control fO2 across a wide range of conditions. The approach is a modification of the previous double capsule design wherein the outer capsule itself acts as the metal component of the buffer assemblage, and the inner capsule to which the astromaterial sample of interest is placed resides within the outer capsule. To achieve higher experimental temperatures above the melting point of more traditional noble metal capsule materials, outer capsules of the control assembly are comprised of refractory (high melting point) metals such as Ni, Co, W, Fe, Mo, V, Cr, Nb and Ta. Resultant experiments have reliably achieved temperatures exceeding 1600 degrees C, and when used in conjunction with a multi-anvil press, system pressures of over 20 GPa can be obtained lending researchers the ability to simulate on or off-world geologic conditions previously difficult to obtain in a laboratory. NASA's fO2 control system was developed to enable high pressure, high temperature experimental studies of astromaterials at fO2 values relevant to the sample of interest. However, it may also be useful for the synthesis of materials where fO2 control is required (e.g., synthesis of crystal structures that might be stable under higher oxygen pressure). Further use cases may include mineral or melt syntheses, metal-silicate or mineral-melt element partitioning, phase equilibria studies, and the possible development of new chemical and mineral compounds that could not be manufactured in laboratories before. This fO2 control system technology is at a technology readiness level (TRL) 6 (system/subsystem prototype demonstration in a relevant environment). The innovation is now available for your company to license. Please note that NASA does not manufacture products itself for commercial sale.
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