LOX / Methane Main Engine Igniter Tests and Modeling-Reference-Cited by-同舟云学术

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LOX / Methane Main Engine Igniter Tests and Modeling

Published:2008-07-21 Issue: Volume: Page:
ISSN:
Container-title:44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Breisacher Kevin,Ajmani Kumud

Publisher

American Institute of Aeronautics and Astronautics

Reference2 articles.

1. LOX/EthanolIgniter", JANNAF Propulsion Meeting, May 2007. 2.Liu, Nan-Suey, "Overview of the NCC", NASA CP-2001-211141,proceeding of the Tenth

2. Flow field measurements of stable and locally extinguishing hydrocarbon-fuelled jet flames

Cited by 8 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. Modes of Laser Spark Ignition of a Model Rocket Combustor;AIAA SCITECH 2023 Forum;2023-01-19

2. Laser ignition of a multi-injector LOX/methane combustor;CEAS Space Journal;2018-02-10

3. Development of Augmented Spark Impinging Igniter System for Methane Engines;53rd AIAA/SAE/ASEE Joint Propulsion Conference;2017-07-07

4. Study on atomization and combustion characteristics of LOX/methane pintle injectors;Acta Astronautica;2017-07

5. Experimental Study of Low Frequency Plasma for Liquid Oxygen and Methane Ignition;48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2012-07-30

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