Design of Thermal Protection System for Reusable Hypersonic Vehicle Using Inverse Approach
Author:
Affiliation:
1. Indian Institute of Technology, Mandi 175 001, India
2. Indian Institute of Technology Bombay, Mumbai 400 076, India
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.A33688
Reference37 articles.
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4. TranH. K.JohnsonC.RaskyD.HuiF.HsuM.T.ChenT.ChenY.ParagasD.KobayashiL. “Phenolic Impregnated Carbon Ablators (PICA) as Thermal Protection System for Discovery Missions,” NASA TM-110440, Washington, D.C. 1997.
5. Selection of Materials and Design of Multilayer Lightweight Passive Thermal Protection System
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