Launch vehicle line type bundling separation device
A separation device and carrier rocket technology, which is applied to the docking device of space navigation aircraft, the propulsion system device of space navigation aircraft, etc., can solve problems such as stress concentration, and achieve the effects of increasing carrying capacity, reducing self-weight and low impact
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[0027] The present invention will be described in detail below in conjunction with the accompanying drawings.
[0028] See attached figure 1 , the present invention binds and connects the inter-box section of the core stage with the oblique cone of the booster, forming a plate structure that is placed along the axis of the rocket with an overall approximate "I" cross-section. The present invention includes four groups of structures, and each group of structures is composed of four "I"-shaped square plates. Among them, each group of structures connects the inter-box section 1 of the rocket core stage and the oblique cone section of the booster, and the four groups of structures closely connect the four boosters with the core stage.
[0029] See attached figure 2 And attached Figure 4 , each "I"-shaped square plate includes a first connecting plate 3-1, a second connecting plate 3-2, two separating plates 3-3, a metal flat tube 3-4, a filler 3-5 and a guide Blast 3-6.
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