Advanced technology application for combustion chamber concepts-Reference-Cited by-同舟云学术

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Advanced technology application for combustion chamber concepts

Published:1992-07-06 Issue: Volume: Page:
ISSN:
Container-title:28th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

TYGIELSKI KATHY¹

Affiliation:

1. NASA, Marshall Space Flight Center, Huntsville,AL

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1992-3857

Reference5 articles.

1. Elam, S.K. " Subsca 1e LOX/Hydrogen Testing with a Modular Chamber and a Swirl Coaxial Injector", AIAA 91-1874.

2. Regeneratively Cooled Rocket combustion Chambers", AIAA 92-3526.

3. Janke, D . E . , and Hayes, W.A. "A New Approach to Cooled Combustion Chambers: The 40K Formed Platelet Chamber", AIAA-92-3864.

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. Additive Manufacturing and Hot-fire Testing of Liquid Rocket Channel Wall Nozzles Using Blown Powder Directed Energy Deposition Inconel 625 and JBK-75 Alloys;AIAA Propulsion and Energy 2019 Forum;2019-08-16

2. A concurrent multi-disciplinary approach for the analysis of liquid rocket engine combustors;30th Joint Propulsion Conference and Exhibit;1994-06-27

3. Numerical analysis of the hot-gas-side and coolant-side heat transfer in liquid rocket engine combustors;28th Joint Propulsion Conference and Exhibit;1992-07-06

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