Conceptual Modeling of Drag-Augmented Supersonic Retropropulsion for Mars Entry, Descent, and Landing
Author:
Affiliation:
1. Department of Aerospace Engineering Sciences, University of Colorado at Boulder, Boulder, Colorado 80309
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.A32920
Reference32 articles.
1. Mars Exploration Entry, Descent, and Landing Challenges
2. Entry, Descent and Landing Systems Analysis: Exploration Class Simulation Overview and Results
3. Survey of Supersonic Retropropulsion Technology for Mars Entry, Descent, and Landing
4. Performance Characterization of Supersonic Retropropulsion for High-Mass Mars Entry Systems
5. Fully-propulsive Mars atmospheric transit strategies for high-mass payload missions
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