Experimental Investigation on Transpiration Cooling Effectiveness for Spacecraft Entering Martian Atmosphere
Author:
Affiliation:
1. Indian Institute of Science, Bangalore 560 012, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J054757
Reference22 articles.
1. Mars environmental survey probe aerobrake preliminary design study
2. High-speed aerodynamics of several blunt-cone configurations
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