Particle size distribution measurements in a subscale motor for the Ariane 5 solid rocket booster-Reference-Cited by-同舟云学术

Particle size distribution measurements in a subscale motor for the Ariane 5 solid rocket booster

Published:1992-07-06 Issue: Volume: Page:
ISSN:
Container-title:28th Joint Propulsion Conference and Exhibit
language:
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Author:

TRAINEAU J.¹,KUENTZMANN P.¹,PREVOST M.¹,TARRIN P.¹,DELFOUR A.²

Affiliation:

1. ONERA, Chatillon, France

2. ONERA, Centre d'Etudes et de Recherches de Toulouse, France

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1992-3049

Reference16 articles.

1. Segmented solid rocket motor for Ariane 5

2. Assessment of chamber pressure oscillations in the Shuttle SRB

3. Vortex Shedding as a Source of Acoustic Energy in Segmented Solid Rockets

4. Numerical simulation of vortex shedding phenomenon in 2D test case solid rocket motors

5. Tien, J.S. "Theoretical Analysis of Combustion Instability",Fundamentalsof Solid-PropellantCombustion, Progressin Astronauticsand Aeronautics,Vol.90,1984.

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