Rocket-based versus solar wing-tail Martian UAVs: design, analysis, and trade studies

Abstract

In this study, a rocket-based UAV and a solar wing-tail Martian UAV were designed and assessed against a set of criteria established using a house of quality chart. For the design, analysis, trade studies, and optimization, MATLAB and XFLR5 were used. The optimized versions of the two configurations feature the same wing and tail airfoils, the same wing and tail planforms, different dimensions, weight, and performance. Therefore, distinct types of scientific missions are suitable for these aircraft. The results of the study extend our understanding of the capabilities of a Martian fixed-wing airplane in terms of payload mass, hence its scientific value, as well as in terms of its planform geometry and airfoil shapes.