Research on Hot Decomposition and Burn Function of a Double Base Propellant
- https://doi.org/10.2991/mmme-16.2016.93How to use a DOI?
- Double base propellant, DSC, Closed bomb test, Kinetics of thermal analysis method
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
- © 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 - https://doi.org/10.2991/mmme-16.2016.93 ID - Wang2016/10 ER -