MATERIALS RESEARCH & DESIGN INC — Department of Defense SBIR Phase I: MDA20-002

Description

Recent developments with the maturation and characterization of MAX phase materials indicate that a handful of these materials would be suitable for the heat produced by third stage rocket motors (TSRM). The majority of investigations have focused on alumina forming ‘211’ MAX phase systems that form an adherent oxide scale. However, tantalum carbide forming MAX phase materials offer an alternative approach to high performance rocket motor throat materials. As opposed to the expensive/difficult route of fabricating and machining bulk tantalum carbide, tantalum carbide forming MAX phase materials are readily machinable and thermally decompose into tantalum carbide at elevated temperatures. MR&D plans to team up with the Greenleaf Corporation in order to investigate a tantalum carbide forming MAX phase composition for TSRM throats. This proposed MAX phase material evaluation work will be accomplished with a three-pronged approach including computational thermomechanical analyses of the rocket motor throat supported by first-principle property prediction techniques, fabrication optimization techniques to produce a phase pure MAX phase composition, and material characterization via thermomechanical testing and oxyacetylene torch test evaluation. Approved for Public Release | 20-MDA-10643 (3 Dec 20)