Universal servo control small rocket system

Abstract

The invention discloses a universal servo control small rocket system. The universal servo control small rocket system specifically comprises a small rocket fuel inlet, a combustion chamber, a spray pipe, a control system track, a universal servo control system rudder wing and a universal servo control system; the small rocket fuel inlet is used for receiving fuel; the combustion chamber is connected to the small rocket fuel inlet and used for igniting combustible gas after fuel enters the combustion chamber, and high-temperature and high-pressure gas is formed in the combustion chamber; the spray pipe is connected to the combustion chamber, and high-temperature and high-pressure gas generated by the combustion chamber generates huge thrust after passing through the spray pipe; the control system track is connected with the universal servo control system, and the universal servo control system changes the position in the control system track so as to control the direction of the spray pipe; and the universal servo control system rudder wing is connected with the universal servo control system, and the universal servo control system controls the angle change of the universal servo control system rudder wing. In the manufacturing and installing processes, the operation time is effectively shortened, the assembling difficulty is reduced, and the connecting efficiency and reliability are improved.

Description

technical field [0001] The application relates to the field of rockets, in particular to a method for constructing and positioning a radio map in a wireless communication network and a system thereof. Background technique [0002] At present, the small rockets used in the industry or the attitude and orbit control small rockets are small rockets with fixed thrust and fixed direction. Different types of small rockets are designed according to different structural designs and shapes. The design process is cumbersome, there are many project models, and the versatility is not strong. waste. Design cycle time is long. [0003] The currently used fixed thrust and fixed direction small rocket system has three major disadvantages: 1. In terms of small rocket thrust and direction: because the small rocket system is locked in the direction of the nozzle design, such as Figure 1a and Figure 2a , the nozzle can only be at a straight angle or at a certain angle, but only one high-spe...

AI Technical Summary

Problems solved by technology

[0003] The currently used fixed thrust and fixed direction small rocket system has three major disadvantages: 1. In terms of small rocket thrust and direction: because the small rocket system is locked in the direction of the nozzle design, such as Figure 1a and Figure 2a , the nozzle can only be at a right angle or at a certain angle, but only one high-speed fluid flows out, and the direction is fixed

2. In terms of installation quantity and complexity: Since the direction of thrust remains unchanged, several small rocket systems need to be installed on the surface of the rocket body, and the layout directions are also different, such as vertical layout, horizontal layout, and other multi-directional layouts, such as Figure 1b and Figure 2b , generally install 4 small rocket systems on the surface of the rocket body, which affects the structural layout space and the coordination of electromagnetic valves, increases equipment and weight, and adds unsafe factors

3. In terms of process requirements: the number of installations is large, the pipeline layout, and the installation process is complex

The efficiency of small rockets is low, and it will affect the follow-up installation process

And structural failures are highly random, and it is difficult to guarantee safety reasons

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