Supersonic Retropropulsion Validation Experiment in the NASA Langley Unitary Plan Wind Tunnel
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681
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.A32649
Reference22 articles.
1. Mars Exploration Entry, Descent, and Landing Challenges
2. High Mass Mars Entry, Descent, and Landing Architecture Assessment
3. Dwyer CiancioloA. M.et al. “Entry, Descent and Landing Systems Analysis Study: Phase 1 Report,” NASA TM-2010-216720, July 2010.
4. Development of Supersonic Retro-Propulsion for Future Mars Entry, Descent, and Landing Systems
5. Performance Characterization of Supersonic Retropropulsion for High-Mass Mars Entry Systems
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