Determining the ballistic characteristics of space penetrator
To model the movement of an aviation penetrator, it is necessary to know the coefficient of the drag and the coefficient of the lift force. The article presents a method of calculating them using the geometric dimensions of the penetrator. The obtained values of the coefficients are compared with those obtained when blowing a penetrator in the aerodynamic tube. By the sustainability criterion is determines the degree of damping of the penetrator. The results of modeling the movement of the penetrator show, that the mathematical model of motion can be used to solve the task of targeting.
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2001 ◽
Vol 6
(1)
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pp. 9-19
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2011 ◽
Vol 2
(1)
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pp. 1-12
2004 ◽
Vol 62
(1-6)
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pp. 113-120
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