Design method for launching cylinder preventing guide missile from rolling in loading process
A design method and launch tube technology, applied in launch devices, calculations, special data processing applications, etc., can solve the problems of excessive roll volume, limited capacity, and inability to meet the requirements of engineering use, and achieve the goal of improving installation efficiency and preventing The effect of rolling, improving safety and reliability
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[0043] Exemplary embodiments of the present invention will be described in detail below with reference to the accompanying drawings. The description of the exemplary embodiments is for the purpose of illustration only, and in no way limits the invention and its application or usage.
[0044] Such as figure 1 As shown, the missile 10 , the adapter 20 arranged on the body of the missile 10 and the launch tube 30 for accommodating the missile 10 are shown in the missile loading process. A plurality of annular adapters 20 may be provided on the circumference of the body of each missile 10 . The ring adapter 20 is usually made of a material with a certain degree of elasticity, so as to be able to support the missile 10 in the launch tube 30 . In order to prevent or reduce as far as possible the rolling of the missile 10 relative to the launching tube 30 during its loading process, that is to prevent the relatively fixedly rolling of the adapter 20 relatively fixedly arranged on t...
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