An aerothermochemical analysis of carbon-carbon nozzle regression insolid-propellant rocket motors-Reference-Cited by-同舟云学术

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An aerothermochemical analysis of carbon-carbon nozzle regression insolid-propellant rocket motors

Published:1988-07-11 Issue: Volume: Page:
ISSN:
Container-title:24th Joint Propulsion Conference
language:
Short-container-title:

Author:

BORIE V.¹,BRULARD J.¹,LENGELLE G.¹

Affiliation:

1. ONERA, Chatillon-sous-Bagneux, France

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1988-3346

Reference26 articles.

1. Accordinl a comprehensive model of carbon-carbon reeressiun of iaree advanced solid-rockc:t norlz11 throats similar in Spirit to the approach of Keswani and KUO (8-10) has been put into place.

2. I. Swopo. I. W. and IICrxrd, M.V. "Ktfectsof Soiid-KOCkPt i'ropcllant orniiiialiOTis and Kxhnusl.(;as Cnemistrics on I he Hrnsion of Graphite Nozzics". AlAA SoIId I'roIinl. Rocket ConTerence. Paio Alto, ('A,Ian. 1964.

Cited by 3 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. Modelling of carbon–carbon composite ablation in rocket nozzles;Composites Science and Technology;2010-09

2. Analytical modeling of the steady state ablation of a 3D C/C composite;International Journal of Heat and Mass Transfer;2008-05

3. Identification of Microscale Ablative Properties of C/C Composites Using Inverse Simulation;9th AIAA/ASME Joint Thermophysics and Heat Transfer Conference;2006-06-05

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