Fabrication of TBC-armored rocket combustion chambers by EB-PVD methods and TLP assembling-Reference-Cited by-同舟云学术

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Fabrication of TBC-armored rocket combustion chambers by EB-PVD methods and TLP assembling

Published:2005-01 Issue:2 Volume:6 Page:103-110
ISSN:1468-6996
Container-title:Science and Technology of Advanced Materials
language:en
Short-container-title:Science and Technology of Advanced Materials

Author:

Schulz Uwe,Fritscher Klaus,Peters Manfred,Greuel Dirk,Haidn Oskar

Publisher

Informa UK Limited

Subject

General Materials Science

Link

http://www.tandfonline.com/doi/pdf/10.1016/j.stam.2004.10.001

Reference9 articles.

1. Structurally compliant rocket engine combustion chamber - Experimental and analytical validation

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1. Microstructural Stability of a Metallic Thermal Barrier Coatings for Rocket Engine;Materials Science Forum;2023-12-05

2. Thermo-structural behavior of thermal barrier coatings for thrust chamber applications;International Communications in Heat and Mass Transfer;2022-01

3. The mechanisms of controlling FCT life and failure mode of Ni-based EBPVD YSZ thermal barrier coatings via the effects of both substrate elements and reactive element doping;SN Applied Sciences;2020-12

4. Mechanical Integrity of Thermal Barrier Coatings: Coating Development and Micromechanics;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2020-10-27

5. A new Metallic Thermal Barrier Coating System for Rocket Engines: Failure Mechanisms and Design Guidelines;Journal of Thermal Spray Technology;2019-08-05

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