Surface Heating and Boundary-Layer Transition on a Hypersonic Inflatable Aerodynamic Decelerator
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.A34046
Reference22 articles.
1. HollisB. R.HollingsworthK. E. “Experimental Study of Hypersonic Inflatable Aerodynamic Decelerator (HIAD) Aeroshell with Axisymmetric Surface Deflection Patterns,” NASA TM-2017-219585, March 2017.
2. Survey of Ballute Technology for Aerocapture
3. Hypersonic Inflatable Aerodynamic Decelerator (HIAD)Technology Development Overview
4. Inflatable Re-entry Vehicle Experiment (IRVE) Design Overview
5. IRVE-II Post-Flight Trajectory Reconstruction
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