Preliminary Design of a Fully Axisymmetric Airbreathing Micro Space Launcher-Reference-Cited by-同舟云学术

Preliminary Design of a Fully Axisymmetric Airbreathing Micro Space Launcher

Published:2008-04-28 Issue: Volume: Page:
ISSN:
Container-title:15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
language:
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Author:

Falempin Francois¹,Bouchez Marc¹,Calabro Max²

Affiliation:

1. MBDA Missile Systems

2. Inner Arch

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-2641

Reference45 articles.

1. F.FALEMPIN,Ph. NOVELLI,P.HENDRICK,A.SOUCHIER,Air breathing/rocket combined cycle propulsion efforts in Europe, AAAF - 2002 -268 -Versailles

2. FALEMPIN, D. SCHERRER, G. LARUELLE, Ph.ROSTAND, G. FRATACCI, French Hypersonic Propulsion programme PREPHA -Results, LessonsandPerspectives, AIAA -98 - 1565 -Norfolk

3. J. HUTT, SpaceLaunch Roadmap,AIAA-2003-6941

4. A. BOUDREAU, Status of the Air Force HyTechProgram, AIAA-2003-6947

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