Multistage irregular flight interception preventing guided missile and working method thereof
An anti-interception and missile technology, applied in the field of aircraft, can solve the problems of reduced carrying capacity, deterioration of rocket performance, and reduced reliability, and achieve the effects of long cruising distance, fast attack speed, and increased difficulty.
Patent Information
- Authority / Receiving Office
- CN · China
- Current Assignee / Owner
- Publication Date
- 2017-08-18
Smart Images

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Abstract
Description
technical field
[0001] The invention relates to a multi-stage irregular flight anti-intercept missile and a working method thereof, belonging to the field of aircraft. Background technique
[0002] As humans gradually enter deep space exploration and the functions of space vehicles increase, rockets are required to have greater carrying capacity, so multi-stage rockets appear. Simply put, a multi-stage rocket is formed by connecting several single-stage rockets together. One of the rockets works first, and then separates from the other rockets after the work is completed, and then the second rocket continues to work, and so on. A rocket composed of several rockets is called several stages, such as a secondary rocket, a three-stage rocket, and so on. It should be pointed out that if multiple rockets are working at the same time, they can only be counted as one stage. The advantage of a multi-stage rocket is that it jettisons the no longer useful structure every once in a wh...
Examples
Embodiment Construction
[0031] Embodiments of the present invention are further described below in conjunction with accompanying drawings:
[0032] Such as Figure 1-Figure 4 Shown, the multi-stage irregular flight anti-interception missile of the present invention comprises a first-level booster 1, a second-level booster 3 and a missile head, and a first-level booster 1, a second-level booster 3 and a warhead 10 The size is the same, and the transition is smooth at the junction,
[0033] The primary booster 1 is flat;
[0034] The secondary booster 3 is flat, and its width is greater than the height. The middle position of the upper and lower sides of the tail of the secondary booster 3 is fixed to the left and right adjusting wings 2, and the ends of the secondary booster 3 are fixed to the upper and lower adjusting wings 11 on both sides. , the upper surface of the secondary booster 3 is covered with an arc-shaped plate 4, the arc-shaped plate 4 is a convex shell, the size of the arc-shaped plat...