Airbreathing space launcher interest of a fully variable geometry propulsion system and corresponding French-Russian partnership-Reference-Cited by-同舟云学术

Airbreathing space launcher interest of a fully variable geometry propulsion system and corresponding French-Russian partnership

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:

Bouchez Marc¹,Genevieve Pascal¹,Levine Vadim²,Davidenko Dmitri²,Avrashkov Valery²

Affiliation:

1. Aerospatiale Matra Missiles, Bourges, France

2. Moscow Aviation Inst., Russia

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-3340

Reference48 articles.

1. PREPHA program (1992-1999) was devoted to research in supersonic combustion and hydrogen fueled scramjet technology. AEROSPATIALEMATRA, ONERA and DASSAULT-AVIATION had designed several vehicles, several engines, several air intakes, and select a final assumptions for each. In PREPHA, several propulsion concepts refered as Bl, B2, DCT (and others, not considered in the current study) had been designed.

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