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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.

Pending Publication Date: 2017-08-18
丁乃祥
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Too many stages will not only increase the cost, but also reduce the reliability, and the performance of the rocket will also deteriorate due to the increase in structural mass
Because on the premise that the take-off mass remains the same, increasing the structural mass will inevitably reduce the propellant. From the principle of energy conservation, it can be known that its carrying capacity will inevitably decrease.

Method used

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  • Multistage irregular flight interception preventing guided missile and working method thereof
  • Multistage irregular flight interception preventing guided missile and working method thereof
  • Multistage irregular flight interception preventing guided missile and working method thereof

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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...

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PUM

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Abstract

The invention relates to a multi-stage irregular flight anti-intercept missile and its working method, belonging to the field of aircraft, including a primary booster, a secondary booster and a missile head, a primary booster, a secondary booster and a missile head. The size of the warhead is the same, its transition is smooth, it has multi-stage boosters, the cruising distance is long, and the flight trajectory is irregular, the flight trajectory is difficult to predict, and the attack speed is fast, which greatly increases the difficulty of being intercepted. At the same time, the structure is simple and firm, and the cost is low. It is cheap, and at the same time, it can improve our country's national defense strength, prevent invaders, and protect national sovereignty.

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...

Claims

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Application Information

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IPC IPC(8): F42B10/64F42B15/00F42B15/01
CPCF42B10/64F42B15/00F42B15/01
Inventor 丁乃祥丁磊
Owner 丁乃祥
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