Coaxial Hydrogen/Oxygen Gas-Dynamic Resonance Ignition Technology for Rocket Repetitive Starting-Reference-Cited by-同舟云学术

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Coaxial Hydrogen/Oxygen Gas-Dynamic Resonance Ignition Technology for Rocket Repetitive Starting

Published:2007-06-18 Issue: Volume: Page:
ISSN:
Container-title:AIAA SPACE 2007 Conference & Exposition
language:
Short-container-title:

Author:

Guozhou Zhang¹,Yana Song¹,Nanjia Yu¹,Xiaoyan Tong¹,Bin Ma¹

Affiliation:

1. Beijing University of Aeronautics and Astronautics

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-6157

Reference15 articles.

1. 2Pavli, A. J. and Conrad, E. W. "Resonance-Tube Igniter for Hydrogen-Oxygen RocketEngines,"NASATMX-1460,1967.

2. A resonance igniter for hydrogen-oxygen combustors

3. 4Phillips, B. R., and Pavli, A. J. "Resonance Tube Ignition of Hydrogen-Oxygen Mixtures,"NASATN D-6354,1971.

4. 5Rocketdyne Engineering, "Advanced Ignition Systems Final Report," N71-35152,1971.

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