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At least 397 records · Page 22

Identification of Risks to Eva Created By Ambient Lighting Conditions at the Lunar South Pole

In the coming years, NASA’s Artemis Campaign intends to return humans to the Moon, both to explore and to establish a permanent human presence. The targeted landing and habitation sites are near the Lunar South Pole (LSP). Compared to the middle latitudes where the Apollo landings occurred, the sun at the LSP is consistently low in the sky, creating a much more challenging visual experience. The NASA Engineering & Safety Center (NESC) is working to characterize the extremes in ambient illumination that astronauts will encounter at the LSP, and to help programs characterize the lighting systems and glare protection that will be required to conduct safe surface operations. This paper will describe the LSP natural environments, and efforts to simulate that visual experience. It will also explain the risks derived from the lighting environment for the mission goals currently planned, and the kinds of new capabilities both in simulation techniques and in surface equipment that will be required to support those mission goals.

Identification of Risks↗

Synergistic Effects of Nano-zinc Oxide on Improving the Flame Retardancy of EVA Composites with an Efficient Triazine-Based Charring Agent

The synergistic effect of nano-zinc oxide (nano-ZnO) on the flame retardancy and thermal stability of intumescent flame retardant ethylene–vinyl acetate (EVA/IFR) consisting of novel hyperbranched triazine-based charring agent (HTCFA) and APP was evaluated by limiting oxygen index (LOI), UL-94 measurement, cone calorimeter test (CCT) and thermogravimetric analysis (TGA), and the residue analysis was also carried out through scanning electron microscopy (SEM), fourier transform infrared (FTIR), laser raman spectroscopy (LRS), and X-ray photoelectron spectroscopy (XPS). The results showed that introducing a certain amount of nano-ZnO could obviously enhance LOI value and UL-94 rating, and effectively restrain the combustion performance of EVA/IFR composites, leading to the decrease of heat and smoke release. The addition of 0.5 wt% nano-ZnO into EVA/IFR composite obtained the highest catalytic effectivity (CAT-EFF). TGA results uncovered a distinct synergistic carbonization effect existed between nano-ZnO and IFR, and nano-ZnO could obviously improve the high-temperature thermal stability and promote the char formation of IFR and EVA/IFR. Analysis of final char residues proved that the incorporation of appropriate amount of nano-ZnO contributed to remaining more P and forming more high-quality graphitization char layers with richer P–O–C and P–N cross-linking structures in condensed phase owing to the catalytic carbonization effect of nano-ZnO on IFR system, which played a critical role in remarkable improvement of flame retardancy and smoke suppression properties of composites.

77 NANOSCIENCE AND NANOTECHNOLOGY↗

Fusible heat sink for EVA thermal control

The preliminary design and analysis of a heat sink system utilizing a phase change slurry material to be used eventually for astronaut cooling during manned space missions is described. During normal use, excess heat in the liquid cooling garment coolant is transferred to a reusable/regenerable fusible heat sink. Recharge is accomplished by disconnecting the heat sink from the liquid cooling garment and placing it in an on board freezer for simultaneous slurry refreeze and power supply electrical rechange.

Roebelen, G. J., Jr.↗

EVA space suit Evaporative Cooling/Heating Glove System (ECHGS)

A new astronaut glove, the Evaporative Cooling/Heating Glove System (ECHGS), was designed and developed to allow the handling of objects between -200 F and +200 F. Active heating elements, positioned at each finger pad, provide additional heat to the finger pads from the rest of the finger. A water evaporative cooling system provides cooling by the injection of water to the finger areas and the subsequent direct evaporation to space. Thin, flexible insulation has been developed for the finger areas to limit thermal conductivity. Component and full glove tests have shown that the glove meets and exceeds the requirements to hold a 11/2 inch diameter bar at + or - 200 F for three minutes within comfort limits. The ECHGS is flexible, lightweight and comfortable. Tactility is reasonable and small objects can be identified especially by the fingertips beyond the one half width active elements.

Coss, F. A.↗