Development status of the VINCI engine for Ariane 5 upper stage-Reference-Cited by-同舟云学术

Development status of the VINCI engine for Ariane 5 upper stage

Published:2000-07-24 Issue: Volume: Page:
ISSN:
Container-title:36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
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Author:

Jean F.¹,Dalbies E.¹

Affiliation:

1. SNECMA, Vernon, France

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-3786

Reference4 articles.

1. AIAA 99-2600 Development status of the VINCI engine for Ariane 5upper stage F. Jean-J.L.Barthoulot (SNECMA)

2. AIAA 99-2191 Design of a high performance low hydrogen turbopump forVINCI engine R.Bosson -B. Goirand (SNECMA) cost

3. AIAA 99-2601 Development of the thrust chamber forthe new cryogenic upper stage engine forAriane T.Mattstedt -F.Haidinger -C.Hensel (DASA)

4. AIAA 99-2474 Ignition System Concept forthe new Cryogenic Upper Stage Engine of Ariane 5 C. Hensel -T. Mattstedt -W.Oechslein (DASA) E. Vermeulen-M. DeWilde (SPE)

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