Simulating Stardust Earth Reentry with Radiation Heat Transfer
Author:
Affiliation:
1. Wright State University, Dayton, Ohio 45435
2. Russian Academy of Sciences, 119526, Moscow, Russia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.52029
Reference35 articles.
1. Aerothermodynamics of the Stardust Sample Return Capsule
2. Calculation of Stagnation-Point Heating Rates Associated with Stardust Vehicle
3. Zel'dovich, Ya. B., and Raizer, Yu. P., Physics of Shock Waves and High-Temperature Hydrodynamic Phenomena, Dover, Mineola, NY, 2002, pp.107-348.
4. Influence of Ablation Products on the Radiation at the Surface of a Blunt Hypersonic Vehicle at 10 km/s
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