Thermal Shock Resistance of Ultra-High-Temperature Ceramic Thermal Protection System-Reference-Cited by-同舟云学术

Thermal Shock Resistance of Ultra-High-Temperature Ceramic Thermal Protection System

Published:2014-05 Issue:3 Volume:51 Page:986-990
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Cheng Tianbao¹,Li Weiguo¹,Lu Wei¹,Shi Yushan¹,Fang Daining²

Affiliation:

1. Department of Engineering Mechanics, Chongqing University, 400030 Chongqing, People’s Republic of China

2. State Key Laboratory for Turbulence and Complex Systems, Peking University, 100871 Beijing, People’s Republic of China

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.A32580

Reference12 articles.

1. LoehmanR.CorralE.DummH. P.KotulaP.TandonR. “Ultra High Temperature Ceramics for Hypersonic Vehicle Applications,” Sandia National Lab., Rept. SAND-2006-2925, Albuquerque, NM, June 2006.

2. Refractory Diborides of Zirconium and Hafnium

3. Mechanical behavior of two-step hot-pressed ZrB2-based composites with ZrSi2

4. Compressive strength degradation in ZrB2-based ultra-high temperature ceramic composites

5. Aerothermodynamic study of UHTC-based thermal protection systems

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