Low Density Supersonic Decelerator Parachute Decelerator System
Author:
Affiliation:
1. Jet Propulsion Laboratory, California Institute of Technology
2. Pioneer Aerospace Corporation
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-1329
Reference11 articles.
1. Aerodynamic Characterization of New Parachute Configurations for Low-Density Deceleration
2. Lingard, J. S., and Underwood, J. "The Effect of Low Density Atmospheres on the Aerodynamic Coefficients of Parachutes," AIAA-1995-1556.
3. Cruz, J. R., Mineck, R. E., Keller, D. F., and Bobskill, M. V. "Wind Tunnel Testing of Various Disk-Gap-Band Parachutes," AIAA-2003-2129.
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