An ejection trajectory device of a launcher
A launcher and orbital technology, which is applied to rocket launchers, launch/drag transmission devices, and lifting devices, etc., can solve the problems of high system cost and complicated operation, and achieves low measurement and control costs, easy welding and construction, and high overall rigidity. Effect
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[0050] The ejection track device of the launcher of the present invention will be described in detail below with reference to the accompanying drawings.
[0051] As shown in Figure 1-14, an ejection track device for a launcher includes a base 1 and a track 2 located on the base 1. The track 2 in this embodiment consists of three sections of tracks, which are respectively a secondary track b and a main track a. Sub-track two c, the rear end of sub-track one b and the front end of main track a are connected together by hinges.
[0052] More specifically: the right rear end of the auxiliary track ab is hingedly connected with the right front end of the main track a. The above structure realizes that the auxiliary track b can be bent and folded to the right, and the folding effect is that the auxiliary track ab Parallel with the main track a to achieve the purpose of retracting. The left rear end of the main track a and the left front end of the secondary track 2 c are connected ...
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