Hydrocarbon-fuel/copper combustion chamber liner compatibility, corrosion prevention, and refurbishment-Reference-Cited by-同舟云学术

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Hydrocarbon-fuel/copper combustion chamber liner compatibility, corrosion prevention, and refurbishment

Published:1991-06-24 Issue: Volume: Page:
ISSN:
Container-title:27th Joint Propulsion Conference
language:
Short-container-title:

Author:

ROSENBERG S.¹,GAGE M.¹,HOMER G.¹,FRANKLIN J.¹

Affiliation:

1. Aerojet, Propulsion Div., Sacramento, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1991-2213

Reference7 articles.

1. I. Roback, R.,Szetela, E.J.,and Spadaccini, L.J. "Deposit Formation in Hydrocerhon Fuels," NASA CR-165405,August 19x1.

2. Giovnnetti. A.J.,Spadxcini, L.J.,and Szetela,E.J. "Deposit Formation andHeatTransfer in llydrocarbon Rocket Fuels," NASA CR-168277, Octobcr 19x3.

3. Morinoshi, R.,and Cook, R.T. "Methane Heat Transfer Investigation." Contract NAS 8-34977.

Cited by 1 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. Compatibility of Methane Fuel with LOX/Methane Engine Combustion Chamber Cooling Channels;44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2008-07-21

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