Numerical Simulation of Pintle Thrust Adjustable Solid Rocket Motor

DOI

10.2991/iccia-17.2017.7How to use a DOI?

Keywords

Thrust adjustable, solid rocket motor, Nozzle efficiency.

Abstract

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.

Copyright

© 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/).

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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  -