A Fully Three Dimensional Analysis of Pre-Ignition Transient in Solid Rocket Motors

Author:

Favini Bernardo,Zaghi Stefano,Serraglia Ferruccio,Di Giacinto Maurizio

Publisher

American Institute of Aeronautics and Astronautics

Reference16 articles.

1. 1Favini, B., Zaghi, S., Serraglia, F., and Di Giacinto, M. "3D Numerical Simulation of Ignition Transient in SRM," AIAA, July 2006, 42thJoint Propulsion Conference, Sacramento, California.

2. 2Favini, B., Di Giacinto, M., and Serraglia, F. "Ignition Transient Pressure Oscillations in Solid Rocket Motors," AIAA, July 2005, 41thJoint Propulsion Conference, Tucson, Arizona.

3. 3Favini, B., Serraglia, F., Di Giacinto, M., and Neri, A. "Pressuring Gas Effects on Pressure Oscillations during the Ignition Transient of SRM," EUCASS, July 2005, 1thEuropean Conference for AeroSpace Sciences, Moscow.

4. 4Favini, B., Serraglia, F., and Di Giacinto, M. "Modeling of Flowfield Features During Ignition of Solid Rocket Motors," AIAA Paper 2002-3753, July 2002, 38thJoint Propulsion Conference, Indianapolis, Indiana.

5. 5Serraglia, F., Favini, B., Di Giacinto, M., and Neri, A. "Gas Dynamic Features in Solid Rocket Motors with Finocyl Grain during Ingnition," ESA/DLR, November 2004, Cologne.

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