21st AIAA Aerodynamic Decelerator Systems Technology Conference


CIMSA ramair parachutes succeed in PACD 2008


ESA IXV Space Vehicle


RESEARCH & DEVELOPMENT / UHARAW

Ultra High Aspect Ratio Ram-Air Wing is an internal research and development program addressing the feasibility of designing a very high aspect ratio ram-air textile wing able to be deployed at high wing loadings.

The project involved the design of extreme wing plan form shapes, critical airfoil sections and sophisticated internal wing structures with special emphasis on internal pressure control through standard flight envelope maneuvers.