An investigation into a non-axisymmetric tension shell decelerator concept via a computational design procedure

Keyphrases

• Computational Design 100%
• Decelerator 100%
• Design Procedure 100%
• Non-axisymmetric 100%
• Angle of Attack 66%
• Design Space 33%
• Fluid-structure Interaction 33%
• Flow Solver 33%
• Simple Modification 33%
• Structural Performance 33%
• Initial Shape 33%
• Aerodynamic Performance 33%
• Interaction Capabilities 33%
• Inflatable Decelerator 33%
• Pure Tension 33%
• Non-symmetry 33%

Engineering

• Design Procedure 100%
• Axisymmetric 100%
• Angle-of-Attack 50%
• Design Space 25%
• Flow Solver 25%
• Inflatables 25%
• Pure Tension 25%
• Aerodynamic Performance 25%
• Structural Performance 25%
• Fluid-Structure Interaction 25%