High Angle-of-Attack Pitching Moment Characteristics of Slender-Bodied Reusable Rocket
Author:
Affiliation:
1. Yokohama National University, Yokohama, Kanagawa 240-8501, Japan
2. Institute of Space and Astronautical Science, Kanagawa 252-5210, 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.A34211
Reference28 articles.
1. Concept and Preliminary Flight Testing of a Fully Reusable Rocket Vehicle
2. Simulation and Analyses of Stage Separation of Two-Stage Reusable Launch Vehicles
3. Optimal Longitudinal Trajectories for Reusable Space Vehicles in the Terminal Area
4. Weight Growth Study of Reusable Launch Vehicle Systems
5. Wing Planform Design Optimization for Reusable Launch Vehicle
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