C/SiC Based Rigid External TPS for Future RLV: Generic Shingle, Pre-X / FLPP Anticipated Development Test Studies-Reference-Cited by-同舟云学术

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C/SiC Based Rigid External TPS for Future RLV: Generic Shingle, Pre-X / FLPP Anticipated Development Test Studies

Published:2005-05-16 Issue: Volume: Page:
ISSN:
Container-title:AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference
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Author:

Soyris Philippe¹,Foucault A.¹,Parenteau JM¹,Pichon T¹,Prel Y.¹,Guedron S.¹

Affiliation:

1. Snecma Propulsion Solide

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-3375

Reference4 articles.

Cited by 5 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Development and flight qualification of the C–SiC thermal protection systems for the IXV;Acta Astronautica;2016-07

2. Dynamical and thermal qualification of the C–SiC nose for the IXV;Acta Astronautica;2016-07

3. Preparation and properties of C/SiC bolts via precursor infiltration and pyrolysis process;Rare Metals;2011-03

4. CMC thermal protection system for future reusable launch vehicles: Generic shingle technological maturation and tests;Acta Astronautica;2009-07

5. Compressive Properties and Fracture Behavior of Two-and-a-Half-Dimensional C/SiC Composites;International Journal of Applied Ceramic Technology;2007-03

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