Experimental validation of stability assessment methods for segmented solid propellant motors

Author:

VUILLOT F.1,TRAINEAU J.1,PREVOST M.1,LUPOGLAZOFF N.1

Affiliation:

1. ONERA, Chatillon, France

Publisher

American Institute of Aeronautics and Astronautics

Reference29 articles.

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

2. ALDEN R.J. "Improvedperformance 3.05m(120in.) boosters for the air force Titan 34D space launch vehicle" The 1983 JANNAF PROPULSION MEETING, VOL.l,pp. 15-27;83N-35012.

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1. Thrust oscillations in reduced Scale Solid Rocket Motors, A new configurations for the MPS of Ariane 5;42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2006-07-09

2. Continuum Modeling of the Dispersed Phase in Solid Rocket Motors;17th AIAA Computational Fluid Dynamics Conference;2005-06-06

3. Computational Study of Turbulence in a Subscale Solid Rocket Motor;40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2004-06-26

4. Linear Analysis of Vortex-Shedding Induced Longitudinal Oscillations in Segmented Solid Rocket Motors;39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2003-06-26

5. Influence of adaptive control on vortex-driven instabilities in a scaled model of solid propellant motors;Journal of Sound and Vibration;2003-05

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