Predicting the Perforation Response of Honeycomb Sandwich Panels Using Ballistic Limit Equations
Protecting spacecraft against orbital debris impact damage using composite materials
Onset of petalling in a thin spacecraft wall perforated by an orbital debris particle
Some Further Comments on the New W-S Habitable Module Wall Damage Prediction Equations
Cracking Characteristics of Dual-Wall Structures Following Simulated Orbital Debris Particle Impact
Space Situational Awareness: It's Not Just About the Algorithms
Bonded Composite Patch Design for Aircraft Structures Exhibiting Cracking and Corrosion
Characterizing Debris Clouds Created in Oblique Orbital Debris Particle Impact
FULL-LENGTH PAPERS - New Failure Criterion for Space Shuttle Main Engine Turbine Blades