Safety Simulation Analyses for Shot Solid Rocket Motor
Hong-bo Liu, Xin-long Chang, Kuan Hu, Chun-guo Yue
Available Online January 2017.
- https://doi.org/10.2991/icmmita-16.2016.150How to use a DOI?
- solid rocket motor; solid propellant; shot; numerical simulation
- In order to study the safety of a shot SRM, a simulation model was established. Ignition and growth reactive flow equation was applied to describe the ignition process of the impacted propellant. The process of SRM being shot was simulated numerically by use of nonlinear finite element method of fluid dynamics. It was demonstrated that the critical velocity of the shot SRM exploding is 850~855m/s, and the max pressure was in the wave front during the initiation caused by impact.
- Open Access
- This is an open access article distributed under the CC BY-NC license.
Cite this article
TY - CONF AU - Hong-bo Liu AU - Xin-long Chang AU - Kuan Hu AU - Chun-guo Yue PY - 2017/01 DA - 2017/01 TI - Safety Simulation Analyses for Shot Solid Rocket Motor BT - Proceedings of the 2016 4th International Conference on Machinery, Materials and Information Technology Applications PB - Atlantis Press SP - 806 EP - 812 SN - 2352-538X UR - https://doi.org/10.2991/icmmita-16.2016.150 DO - https://doi.org/10.2991/icmmita-16.2016.150 ID - Liu2017/01 ER -