UNMANNED AERIAL SYSTEM (UAS) SAFETY ANALYSIS MODEL (AIAA 2014-2285)
Probabilistic Optimization of Integrated Thermal Protection System
Overview of NASA Langley's Systems Analysis Capabilities
Experimental Investigation of a Vortex Type Pilot Seat Stabilizer Parachute System
Drag Reduction Study of a 2D Metal Projectile Series Using SU2 Code (AIAA 2018-4128)
Design Evaluation of an Flexible Decelerator System for 125 kg Class Weapon at Sonic Velocity
Design Development and Testing of Stabilising Parachute for Bomblet