Study of the Afterbody Radiation during Mars Entry in an Expansion Tube
Author:
Affiliation:
1. University of Queensland
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2017-0212
Reference21 articles.
1. Prediction of Forebody and Aftbody Heat Transfer Rate for Mars Aerocapture Demonstrator
2. Radiative Heating on the After-Body of Martian Entry Vehicles
3. Computation of radiative and convective contributions to Viking afterbody heating
4. Measurement and Characterization of Mid-wave Infrared Radiation in CO2 Shocks
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