17th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar 2003 Help me understand this report
Development of an Improved Performance Parachute System for Mars Missions
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“…aeroshell (heatshield and backshell) [10]. The parachute which is deployed nearly at Mach 2.2 and adynamic pressure of 650P a is fixed to the backshell.…”
Section: Dof Mathematical Modelmentioning
confidence: 99%
“…aeroshell (heatshield and backshell) [10]. The parachute which is deployed nearly at Mach 2.2 and adynamic pressure of 650P a is fixed to the backshell.…”
Section: Dof Mathematical Modelmentioning
confidence: 99%
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