Parametric Study of an Ablative TPS and Hot Structure Heatshield for a Mars Entry Capsule Vehicle

  • Sarah L. Langston, Christapher G. Lang, Jamshid A. Samareh
  • September 2017, American Institute of Aeronautics and Astronautics (AIAA)
  • DOI: 10.2514/6.2017-5290

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http://dx.doi.org/10.2514/6.2017-5290

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