Ablation of solid-fuel booster nozzle materials-Reference-Cited by-同舟云学术

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Ablation of solid-fuel booster nozzle materials

Published:1997-06 Issue:4 Volume:1 Page:277-289
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Maisonneuve Y

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference19 articles.

1. Ablation des matériaux de tuyères de propulseurs à propergol solide;Borie,1990

2. Ablation des matériaux composites carbone-carbone: résultats expérimentaux et prise en compte dans la modélisation;Maisonneuve;RT interne ONERA no 16/4305 EN,1989

3. Burning Carbon and Particles in the Presence of Water Vapor;Libby;Combustion and Flame,1981

4. Recession Behavior of Graphitic Nozzles in Simulated Rocket Motors;Keswani,1983

5. A Comprehensive Theoretical Model for Carbon-Carbon Composite Nozzle Recession;Kuo;Combust. Sci. and Tech.,1986

Cited by 14 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. Understanding mechanical failure of graphite rocket nozzle throats under thermal stresses;Aerospace Science and Technology;2021-12

2. SiC-Based Composites Through Liquid Infiltration Routes;Handbook of Advanced Ceramics and Composites;2020

3. SiC-Based Composites Through Liquid Infiltration Routes;Handbook of Advanced Ceramics and Composites;2019-12-25

4. SiC-Based Composites Through Liquid Infiltration Routes;Handbook of Advanced Ceramics and Composites;2019

5. Thermodynamic properties of carbon–phenolic gas mixtures;Aerospace Science and Technology;2017-07

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