High-Energy Atmospheric Reentry Test Aerothermodynamic Analysis
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 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.A32407
Reference17 articles.
1. Hypersonic Inflatable Aerodynamic Decelerator (HIAD)Technology Development Overview
2. Aerocapture Inflatable Decelerator (AID) for Planetary Entry
3. Inflatable Re-entry Vehicle Experiment (IRVE) Design Overview
4. MazaheriA. R.GnoffoP. A.JohnstonC. O.KlebB. “LAURA 5 Users Manual,” NASA TM-217092-2011, 2011.
5. HashD.OlejniczakJ.WrightM.PrabhuD.PulsonettiM.HollisB.GnoffoP.BarnhardtM.NompelisI.CandlerG. “Fire II Calculations for Hypersonic Nonequilibrium Aerothermodynamics Code Verifcation: DPLR, LAURA and US3D,” AIAA Paper 2007-0605, 2007.
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