Emission Properties and Stability of Internal Air Launch System

DOI

10.2991/icmeit-17.2017.34How to use a DOI?

Keywords

internal air launch system, emission performance index, generalized stability, stability domain.

Abstract

Aiming at the characteristics of complex structure, changeable movement and the difference in emission and stability, put forward the emission performance index based on the study of internal air launch system; study the influence of the initial pitch angle of the carrier, characteristic diameter of stabilization parachute and some other characteristic parameters on emission properties; study the system's stability and put forward the concept of generalized stability through the research of kinetic equation, moreover, calculate stability domain through Monte Carlo calculation method.

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  - Jie Shu
AU  - Dengcheng Zhang
AU  - Lin Li
AU  - Ang Qin
AU  - Binlin Ma
AU  - Shuguang Li
PY  - 2017/05
DA  - 2017/05
TI  - Emission Properties and Stability of Internal Air Launch System
BT  - Proceedings of the 2nd International Conference on Mechatronics Engineering and Information Technology (ICMEIT 2017)
PB  - Atlantis Press
SP  - 187
EP  - 192
SN  - 2352-538X
UR  - https://doi.org/10.2991/icmeit-17.2017.34
DO  - 10.2991/icmeit-17.2017.34
ID  - Shu2017/05
ER  -