Uncertainty Analysis of Fluid-Structure Interaction of a Deformable Hypersonic Inflatable Aerodynamic Decelerator
Author:
Affiliation:
1. Missouri University of Science and Technology, Rolla, MO 65409
2. NASA Langley Research Center, Hampton, VA 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A33532
Reference35 articles.
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3. DrakeB. G. “Human Exploration of Mars Design Reference Architecture 5.0,” NASA SP-2009-566, 2009.
4. TannerC. L. “Aeroelastic Analysis and Testing of Supersonic Inflatable Aerodyamics Decelerators,” Ph.D. Dissertation, Georgia Inst. of Technology, Atlanta, GA, May 2012.
5. SwansonG.CassellA. M.JohnsonR. K.HughesS. J.CalominoA. M.CheatwoodF. M. “Structural Strap Tension Measurements of a 6-Meter Hypersonic Inflatable Aerodynamic Decelerator Under Static and Dynamic Loading,” AIAA Paper 2013-1287, March 2013.
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