Computational Aerodynamic Analysis of Capsule Configurations Toward the Development of Reusable Rockets
Author:
Affiliation:
1. University of Tokyo, Tokyo 133-8656, Japan
2. Japan Aerospace Exploration Agency, Kanagawa 229-8510, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.13377
Reference17 articles.
1. X-33 Hypersonic Aerodynamic Characteristics
2. Concept and Preliminary Flight Testing of a Fully Reusable Rocket Vehicle
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