Development and Testing of a Fluid Film Bearing LH2 Turbopump Demonstrator-Reference-Cited by-同舟云学术

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Development and Testing of a Fluid Film Bearing LH2 Turbopump Demonstrator

Published:2004-06-26 Issue: Volume: Page:
ISSN:
Container-title:40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
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Author:

Edeline Emmanuel¹,Fonteyn Patrice¹,Frocot Manuel¹,Dehouve Jérôme²,Fayolle Patrice¹

Affiliation:

1. Snecma Moteurs

2. Centre National d'Etudes Spatiales

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-3688

Reference3 articles.

Cited by 4 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. Stability of Hydrogen Turbopump Rotor Shaft Axially Self-Balanced;Journal of Fluids Engineering;2022-04-05

2. An Overview of Bearing Candidates for the Next Generation of Reusable Liquid Rocket Turbopumps;Chinese Journal of Mechanical Engineering;2020-03-17

3. Manufacturing and Testing of TPX LH2-Turbopump Prototype;46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2010-07-25

4. Progress Status of TPX LH2-Turbopump Demonstration Program;44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2008-07-21

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