Structural Design and Dynamics Simulation Analysis of A Certain Type of Co-frame Launcher
2021 ◽
Vol 2125
(1)
◽
pp. 012037
Keyword(s):
Abstract To study the dynamic response of a certain type of co-frame launcher during launch, this article uses the 3D modeling software Pro/E to import the model into Adams from the perspective of launch dynamics. the launch dynamics model of the shared-frame launcher is established. We apply the ejection thrust of the two types of missiles to the corresponding ejection devices and measure and collect the dynamic parameters of the cartridge system. The simulation results show that the dynamic parameters of the A and B missiles are in line with the available overload design requirements. The B-type missiles are superior to the A-type missiles in terms of ballistic orbit contact force and ejection attitude.
2016 ◽
Vol 842
◽
pp. 251-258
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Keyword(s):
2014 ◽
Vol 940
◽
pp. 132-135
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2020 ◽
Vol 12
(9)
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pp. 168781402095780
2014 ◽
Vol 543-547
◽
pp. 1305-1308
2012 ◽
Vol 268-270
◽
pp. 856-859
Keyword(s):
2013 ◽
Vol 364
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pp. 365-369