One lamellar eutectic sample and one fiber-like eutectic sample were solidified directionally during the TEXUS-6 rocket flight. The microstructures and the results of the thermal analysis, obtained from the temperatures recorded on the cartridge skin, are compared. No appreciable modifications of the regularity of the eutectic structures were observed by passing from 1 g to 0.0001 g in these experiments. No steady state growth conditions were achieved in these experiments.
Directional Solidification of Al2-Cu-Al and Al3-Ni-Al Eutectics During Texus Rocket Flight
1984
61 pages
Report
Keine Angabe
Englisch
Space Technology , Manufacturing Processes & Materials Handling , Manufacturing, Planning, Processing & Control , Optics & Lasers , Nonferrous Metals & Alloys , Aluminum alloys , Copper alloys , Directional solidification (Crystals) , Eutectics , Nickel alloys , Space processing , Laser applications , Low gravity manufacturing , Metal crystals , Metallography , Microstructure , Thermal analysis , Foreign technology , Translations
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