Carbon/carbon nozzle exit cones - SEP's experience and new developments-Reference-Cited by-同舟云学术

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Carbon/carbon nozzle exit cones - SEP's experience and new developments

Published:1997-07-06 Issue: Volume: Page:
ISSN:
Container-title:33rd Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Broquere Bernard¹,Broquere Bernard¹

Affiliation:

1. SEP, St.-Medard-en-Jalles, France

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-2674

Reference15 articles.

1. Carbon-carbonmaterials for nozzles of Solid Propellant rocketmotors.AIAA paper 76-609 , J.J. Choury. SocieteEuropeenne de Propulsion, Saint MedardenJalles,France

2. DeployableExit Cones AIAA 78-1566Y.Coron , Societe Europeennede Propulsion, SaintMedard en Jalles,France

3. AdvancedSpaceMotor DemonstrationAIAA 80-1270R.AEllisand R.N. Hammond,ChemicalSystem Div - United Technologies Sunnyvale, Ca. , P. Donguy, SocieteEuropeennede Propulsion,Saint MedardenJalles,France

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. The Behavior of Pyro-Carbon Matrix Synthesized Through Isothermal Chemical Vapor Infiltration (I-CVI) Process;Lecture Notes in Mechanical Engineering;2023

2. A Global Approach to Fiber nD Architectures and Self-Sealing Matrices: From Research to Production;International Journal of Applied Ceramic Technology;2005-03

3. Carbon/Carbon extendible Nozzles;Acta Astronautica;2002-03

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