Gas phase ignition of solid rocket motors

Author:

Ak Mehmet1,Vural Huseyin2

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

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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