Technical Papers

Technical Papers

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Development of a Low Cost 10,000 lb Capacity Ram Air Parachute, DRAGONFLY Program Presented at the AIAA Aerodynamic Decelerator Systems Technology Conference and Published by AIAA, May 2005, Munich, Germany

AIAA ATPS Simulation The use of LS-DYNA to Assess the Performance of Airborne Systems North Americas Candidate ATPS Main Parachutes, May 2005, Munich, Germany

AIAA Inflation Simulation The use of LS-DYNA to Simulate the Inflation of a Parachute Canopy, May 2005, Munich, Germany

DCLDYN Paper The DCLDYN Parachute Inflation and Trajectory Analysis Tool, May 2005, Munich, Germany

FLOATSTAB Floatstab A Tool for the Rapid Analysis of Flotation Stability, May 2005, Munich, Germany

Design and Testing of an Airbag Landing Attenuator System for a Generic Crew Return Vehicle Presented at the AIAA Aerodynamic Decelerator Systems Technology Conference and Published by AIAA, May 2005, Munich, Germany

The System Approach to Spin Stall Parachute Recovery Systems A Five Year Update Presented at the Society of Experimental Test Pilots Symposium, September 2004, Los Angeles, California

The use of LS-DYNA to Simulate the Water Landing Characteristics of Space Vehicles Presented at the 8th International LS-DYNA Users Conference, May 2004, Detroit, Michigan

An Investigation of the Apparent Mass of Parachutes under Post Inflation Dynamic Loading using FSI Simulation Presented at the AIAA Aerodynamic Decelerator Systems Technology Conference and Published by AIAA, May 2003, Monterey, California

Application of Optimization Software to Aid the Design of an Airbag Decelerator System Presented at the AIAA Aerodynamic Decelerator Systems Technology Conference and Published by AIAA, May 2003, Monterey, California

The Application of Explicit Finite Element Analysis and Fluid Structure Interaction Simulations for Recovery Systems Presented at the 41st SAFE Symposium, September 2003, Jacksonville, Florida

Design and Development of the Main Parachute for the Beagle 2 Mars Lander Presented at the AIAA Aerodynamic Decelerator Systems Technology Conference and Published by AIAA, May 2003, Monterey, California

Design and Testing of the HOPE-X HSFD-II Landing System Presented at the AIAA Aerodynamic Decelerator Systems Technology Conference and Published by AIAA, May 2001, Boston, Massachusetts

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