Testing the First Fuel Turbopump of the Vinci Engine-Reference-Cited by-同舟云学术

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Testing the First Fuel Turbopump of the Vinci Engine

Published:2003-06-26 Issue: Volume: Page:
ISSN:
Container-title:39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
language:
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Author:

Goirand Bruno¹,Alliot P.¹,Barthoulot J.¹,Bonhomme C.²

Affiliation:

1. Snecma

2. Centre National d'Etudes Spatiales

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-5069

Reference7 articles.

1. AIAA2000-3786 Development status of the VINCI engine for Ariane 5 upper stage F.Jean-E. Dalbies

2. AIAA2000-3156 VINCI hydrogen turbopump : a new step in safe, fasterandcheaperdevelopments B. Goirand-J.F. Gallardo-R. Bosson

3. AIAA2000-3831 Development of powder metallurgy impellers for Vincihydrogenturbopump D. Guichard-F. Laithier-J.P. Fournier

4. AIAA99-2346 High Performance Cryogenic Ball Bearing Demonstration R. Bosson-E. Edeline-L. Collongeat

Cited by 1 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. Vinci Engine Development Testing, a Summary of Turbine Testing Results;41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2005-07-10

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