Scaling and Similitude in Single Nozzle Supersonic Retropropulsion Aerodynamics Interference
Author:
Affiliation:
1. NASA Langley Research Center
2. LZ Technology, Inc.
Publisher
American Institute of Aeronautics and Astronautics
Reference15 articles.
1. Survey of Supersonic Retropropulsion Technology for Mars Entry, Descent, and Landing
2. Human Mars Entry, Descent, and Landing Architecture Study: Phase 3 Summary
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4. Supersonic Retropropulsion Experimental Results from NASA Ames 9×7 Foot Supersonic Wind Tunnel
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