Optimal Conceptual Design of Two-Stage Reusable Rocket Vehicles Including Trajectory Optimization
Author:
Affiliation:
1. University of Tokyo, Tokyo 113-8656, Japan
2. Japan Aerospace Exploration Agency, Tokyo 182-8522, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.1082
Reference23 articles.
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