Hot fire ignition test with densified liquid hydrogen using a RL10B-2 cryogenic H2/O2 rocket engine-Reference-Cited by-同舟云学术

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Hot fire ignition test with densified liquid hydrogen using a RL10B-2 cryogenic H2/O2 rocket engine

Published:1997-07-06 Issue: Volume: Page:
ISSN:
Container-title:33rd Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

McNelis Nancy¹,Haberbusch Mark²,McNelis Nancy¹,Haberbusch Mark²

Affiliation:

1. NASA, Lewis Research Center, Cleveland, OH

2. Ohio Aerospace Inst., Cleveland

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-2688

Reference4 articles.

1. Santiago,J.R."EvolutionoftheRLlOLiquidRocket Enginefor aNew UpperstageApplication,"AIAA Paper 96-3013,July, 1996.

Cited by 6 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. Performance evaluation on ground loading systems of cryogenic propellants;Asia-Pacific Journal of Chemical Engineering;2017-09-19

2. Multipass Heat Exchanger Sizing for Optimum Liquid Oxygen Densification with Liquid Nitrogen;AIAA SPACE 2015 Conference and Exposition;2015-08-28

3. Subcooling Cryogenic Propellants for Long Duration Space Exploration;AIAA SPACE 2009 Conference & Exposition;2009-06-14

4. Transient Cryogenic Flow and Mixing from a Coaxial Rocket Injector;45th AIAA Aerospace Sciences Meeting and Exhibit;2007-01-08

5. A Cryogenic Lightweight Mass Gauging System for Expendable and Reusable Launch Vehicles;38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2002-07-07

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