Aerodecelerator Performance of Flare-Type Membrane Inflatable Vehicle in Suborbital Reentry
Author:
Affiliation:
1. University of Tokyo, Kashiwa 277-8561, Japan
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.A33682
Reference26 articles.
1. Inflatable Re-entry Vehicle Experiment (IRVE) Design Overview
2. Survey of Ballute Technology for Aerocapture
3. Postflight Analysis of Inflatable Reentry and Descent Technology Blackout During Earth Reentry
4. Hypersonic Inflatable Aerodynamic Decelerator (HIAD)Technology Development Overview
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