Overview of the Mars Science Laboratory Parachute Decelerator System
Stardust Parachute Trajectory Performance Reconstruction
Mars Scout Phoenix Canopy Stress Analyses
Mars Phoenix Scout Parachute Canopy Structural Test Peak Load Prediction Technique
Mars Science Laboratory Technora Age Study
Inflation Characteristics of the MSL Disk Gap Band Parachute
Inflation Characteristics of the MSL Disk Gap Band Parachute
Design of Subscale Parachute Models for MSL Supersonic Wind Tunnel Testing
Design of Subscale Parachute Models for MSL Supersonic Wind Tunnel Testing
Mars Scout Phoenix Parachute System Performance
Mars Scout Phoenix Parachute System Performance
Findings from the Supersonic Qualification Program of the Mars Science Laboratory Parachute System
Findings from the Supersonic Qualification Program of the Mars Science Laboratory Parachute System
Comparison of Subscale Versus Full-Scale Wind Tunnel Tests of MSL Disk Gap Band Parachutes
Comparison of Subscale Versus Full-Scale Wind Tunnel Tests of MSL Disk Gap Band Parachutes
Parachute Models Used in the Mars Science Laboratory Entry, Descent, and Landing Simulation
Mars Science Laboratory Technora® Age Study Results
Mars Science Laboratory Parachute System Performance
Aerodynamic Characterization of New Parachute Configurations for Low-Density Deceleration
Energy Modulators for Recovery of High Altitude Balloon Payloads
Low Density Supersonic Decelerator Parachute Decelerator System
AIAA-2001-2017 Parafoil Recovery Subsystem for the Genesis Space Return Capsule