Two-Dimensional Aerodynamic Loads of Space Shuttle Thermal Protection System Considering Steady Internal Flow
Author:
Publisher
Springer Singapore
Link
http://link.springer.com/content/pdf/10.1007/978-981-13-3305-7_13
Reference15 articles.
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3. Rodriguez AC, Snapp CG (2011) Orbiter thermal protection system lessons learned. AIAA AIAA-2011-7308
4. Wu D, Wang Y, Gao Z, Yang J (2015) Insulation performance of heat-resistant material for high-speed aircraft under thermal environments. J Mater Eng Perform 24(9):3373–3385
5. Yamada T, Matsuda S, Okuyama K et al (2008) Lessons learned from the recovered heatshield of the USERS REV capsule. Acta Astronaut 62:192–202
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