Performance and stability of a booster class LOX/hydrogen swirl coaxial-element injector-Reference-Cited by-同舟云学术

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Performance and stability of a booster class LOX/hydrogen swirl coaxial-element injector

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

Author:

HULKA J.¹,SCHNEIDER J.¹,DEXTER C.²

Affiliation:

1. Aerojet, Propulsion Div., Sacramento, CA

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

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1991-1877

Reference9 articles.

1. TechsystemsCompany,presented at the 1986JANNAF

2. Reardon,F.H. "GuidelinesforCombustionStability Suecifications and Verification Procedures forLiauid

3. Muss,J.A., C. W. Johnson,and T.V. Nguyen,"Users Manualforthe RocketCombustorInteractiveDesign (ROCCID)Methodology,"NASA CR-185187,Contract NAS 3-25556,February,1991.

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 design and main performance of a hydrogen peroxide/kerosene coaxial-swirl injector in a lab-scale rocket engine;Aerospace Science and Technology;2017-11

2. Large Eddy Simulation of Supercritical Combustion of Liquid Oxygen and Kerosene of a Bi-Swirl Coaxial Injector;51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2013-01-05

3. Near-field Film Thickness Measurements of an LPRE Swirl Injector Spray;47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2011-07-31

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