Aerodynamic Performances of Lifting-Body Configurations for a Reentry Vehicle
Author:
Affiliation:
1. National Aerospace Laboratory, 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/10.2514/1.2418
Reference12 articles.
1. Overview of the HYFLEX Project
2. Concepts of Reentry Technology Experimental Vehicles
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1. Fully Structured Aerodynamic Model for Parameter Identification of a Reentry Experimental Vehicle;Journal of Spacecraft and Rockets;2010-01
2. Research Activities to Realize Advanced Space Transportation System;16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference;2009-06-14
3. Optimization of Nonlinear Lateral Characteristic of Lifting-Body Type Reentry Vehicle;Journal of Aerospace Computing, Information, and Communication;2009-03
4. Improvement of Nonlinear Lateral Characteristics of Lifting-Body Type Reentry Vehicle Using Optimization Algorithm;AIAA Infotech@Aerospace 2007 Conference and Exhibit;2007-05-07
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