Research on Hot Decomposition and Burn Function of a Double Base Propellant
Authors
H.C. Wang, M.H. Chen, S. Yuan, Y.W. Fan
Corresponding Author
H.C. Wang
Available Online October 2016.
- DOI
- 10.2991/mmme-16.2016.93How to use a DOI?
- Keywords
- Double base propellant, DSC, Closed bomb test, Kinetics of thermal analysis method
- Abstract
DSC method and closed bomb test were adopted to an aging different time of the double base propellant forward to carry on a research, activate energy was computed with dynamics method, and computing syn-thesize combustion characteristic parameter of the double base propellant. Conclusion: with aging time longer, activate energy of double base propellant was decrease, the burn function descends
- Copyright
- © 2016, 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 - H.C. Wang AU - M.H. Chen AU - S. Yuan AU - Y.W. Fan PY - 2016/10 DA - 2016/10 TI - Research on Hot Decomposition and Burn Function of a Double Base Propellant BT - Proceedings of the 2016 4th International Conference on Mechanical Materials and Manufacturing Engineering PB - Atlantis Press SP - 405 EP - 407 SN - 2352-5401 UR - https://doi.org/10.2991/mmme-16.2016.93 DO - 10.2991/mmme-16.2016.93 ID - Wang2016/10 ER -