Gas phase ignition of solid rocket motors
Author:
Affiliation:
1. Turkish Research Council, Defence Industries Research and Development Inst., Ankara, Turkey
2. Middle East Technical Univ., Ankara, Turkey
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1999-2495
Reference20 articles.
1. Peretz,A., Kuo, K-K., Caveny,L.H., andSummerfield, M. "Starting Transient of Solid Propellant Rocket Motors with High Internal Gas Velocities0022, AIAA J., vo1.11,1719,1973
2. Pardue,B.A., Han, S.S. "Ignition Transient Analysis of a Solid Rocket Motor Using a One Dimensional Two Fluid Model0022, AIAA paper 93-3277. 3s' Joint PropulsionConferenceand Exhibit, Nashville. TN. July 6-8, 1992.
3. Chang, S.T., Han, S.S, and Chai. J.C. "Radiation Effects on 1-D Ignition Transient Analysis of SRM0022. AIAA paper93-3035, 1996
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