Research on Hot Decomposition and Burn Function of a Double Base Propellant

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/).

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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  -