Proceedings of the 2nd International Conference on Computer Engineering, Information Science & Application Technology (ICCIA 2017)

Numerical Simulation of Pintle Thrust Adjustable Solid Rocket Motor

Authors
Guancheng Pan, Xiong Chen, Xiaobing Ye
Corresponding Author
Guancheng Pan
Available Online July 2016.
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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Volume Title
Proceedings of the 2nd International Conference on Computer Engineering, Information Science & Application Technology (ICCIA 2017)
Series
Advances in Computer Science Research
Publication Date
July 2016
ISBN
10.2991/iccia-17.2017.7
ISSN
2352-538X
DOI
10.2991/iccia-17.2017.7How to use a DOI?
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/).

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  -