Numerical Simulation of Pintle Thrust Adjustable Solid Rocket Motor
- 10.2991/iccia-17.2017.7How to use a DOI?
- Thrust adjustable, solid rocket motor, Nozzle efficiency.
Numerical simulation of the flow field inside pintle controlled solid rocket motor was performed. The effects to nozzle performance with different pintle contour shapes and pintle position were investigated. The results showed that the influence of these factors to pintle nozzle efficiency was evident. The conclusion would be helpful for design experiment and application of pintle controlled solid rocket motor.
- © 2017, the Authors. Published by Atlantis Press.
- Open Access
- This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).
Cite this article
TY - CONF AU - Guancheng Pan AU - Xiong Chen AU - Xiaobing Ye PY - 2016/07 DA - 2016/07 TI - Numerical Simulation of Pintle Thrust Adjustable Solid Rocket Motor BT - Proceedings of the 2nd International Conference on Computer Engineering, Information Science & Application Technology (ICCIA 2017) PB - Atlantis Press SP - 43 EP - 49 SN - 2352-538X UR - https://doi.org/10.2991/iccia-17.2017.7 DO - 10.2991/iccia-17.2017.7 ID - Pan2016/07 ER -