Abstract
To guarantee the missile leaves launch unit smoothly, launch interior ballistic computation model based on gas and steam launch power is improved. One missile is taken for example to compute its interior ballistic. And changing laws of interior ballistic parameters are obtained. Results indicate that the modified model can decrease gas pressure in the unit effectively when missile leaves the launch unit. This is of some reference value for the design of gas and steam launch power system.
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References
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Qinggui, C., Qiang, Q., Yuan, Z., Ruyan, Z., Bin, W. (2013). Interior Ballistic Research on Gas and Steam Launch Power System. In: Yang, G. (eds) Proceedings of the 2012 International Conference on Communication, Electronics and Automation Engineering. Advances in Intelligent Systems and Computing, vol 181. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-31698-2_12
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DOI: https://doi.org/10.1007/978-3-642-31698-2_12
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-31697-5
Online ISBN: 978-3-642-31698-2
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