A Front Tracking Model of the MAXUS-8 Microgravity Solidification Experiment on a Ti-45.5at.%Al-8at.%Nb Alloy

Document Type



Available under a Creative Commons Attribution Non-Commercial Share Alike 4.0 International Licence


Thermodynamics, Materials engineering

Publication Details

IOP Conference Series: Materials Science and Engineering

Made available with the kind permission of the publisher IOP Science (Institute of Physics) home page http://iopscience.iop.org/


On 26th March 2010 the MAXUS-8 sounding rocket was launched from the Esrange Space Center launching facility in Sweden. As part of the Intermetallic Materials Processing in Relation to Earth and Space Solidification (IMPRESS) project, a solidification experiment was conducted on a Ti-45.5at.%Al-8at.%Nb intermetallic alloy in a module on this rocket. The experiment was designed to investigate columnar and equiaxed microstructures in the alloy. A furnace model of the MAXUS 8 experiment with a Front Tracking Model of solidification has been developed to determine the macrosturcture and thermal history of the samples in the experiment. This paper gives details of results of the front tracking model applied to the MAXUS 8 microgravity experiment. A model for columnar growth is presented and compared to experimental results for furnace A of the experiment module.




European Space Agency, PRODEX Programme (via Enterprise Ireland)