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Rocket-borne monitoring system of solid-liquid dynamic sounding rocket

A technology of sounding rockets and monitoring systems, applied to projectiles, self-propelled missiles, offensive equipment, etc., can solve the problems of regulation, monitoring, and lack of flow regulation monitoring and collection records, and achieve low cost, simple structure, and security Effect

Active Publication Date: 2014-11-26
BEIHANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, the research on the adjustment and monitoring of the actual thrust of solid-liquid powered sounding rockets, as well as flow adjustment monitoring and collection records is very scarce

Method used

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  • Rocket-borne monitoring system of solid-liquid dynamic sounding rocket
  • Rocket-borne monitoring system of solid-liquid dynamic sounding rocket
  • Rocket-borne monitoring system of solid-liquid dynamic sounding rocket

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Embodiment Construction

[0057] The present invention will be further described in detail with reference to the accompanying drawings and embodiments.

[0058] A rocket-borne monitoring system of a solid-liquid power sounding rocket proposed by the present invention, such as figure 1 As shown, it includes arrow thrust adjustment controller 1, arrow power supply system 2, arrow data monitor 3, arrow x-axis accelerometer 4, arrow y-axis accelerometer 5, arrow z-axis accelerometer 6, storage Tank pressure sensor 7, cylinder pressure sensor 8, boost valve 9, auxiliary road blow off valve 10, main road blow off valve 11.

[0059] The arrow-borne thrust adjustment controller 1 includes a power supply conversion module 101 , a single-chip microcomputer control valve action module 102 , a feedback module 103 for controlling valve voltage, and a single-chip microcomputer reset and storage module 104 . Among them, the arrow-borne thrust adjustment controller 1 adopts the single-chip microcomputer 89C51.

[00...

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Abstract

The invention discloses a rocket-borne monitoring system of a solid-liquid dynamic sounding rocket. The rocket-borne monitoring system is composed of a rocket-borne thrust adjustment controller and a rocket-borne data monitor. The controller and the monitor are both composed of a plurality of monitoring and testing modules. The rocket-borne monitoring system is mainly used for realizing the following four tasks: converting power supply of the rocket-borne monitoring system from ground power supply to rocket-borne power supply, completing control to actions of relative valves according to thrust adjustment control, carrying out monitoring recording on working conditions of a rocket-borne device, and realizing reset control to the rocket-borne device. By utilizing the rocket-borne monitoring system of the solid-liquid dynamic sounding rocket, control to liquid propellant booster valves, main road and side road channel valves is realized in the flight process of the rocket according to control requirements, the function of thrust adjustment is completed, and safety of a conveying system is ensured. The real-time working conditions of a solid-liquid rocket engine can be effectively reflected by data monitoring results.

Description

technical field [0001] The invention belongs to the field of control systems, and in particular relates to an rocket-borne monitoring system of a solid-liquid powered sounding rocket. Background technique [0002] The solid-liquid powered sounding rocket is a new type of aircraft that uses a solid-liquid rocket engine as a power device, has adjustable thrust, and can be started repeatedly. Compared with solid and liquid rocket engines, the entire combustion process of solid-liquid rocket engines is easier to control, but it also has the difficulty of stabilizing the ratio of oxidant and fuel. The ratio has an important influence on the working performance of the solid-liquid rocket engine such as the combustion efficiency and specific impulse of the solid-liquid rocket engine. At present, the research on the adjustment and monitoring of the actual thrust of solid-liquid powered sounding rockets, as well as flow adjustment monitoring and collection records is very scarce. I...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F42B15/01
Inventor 宋佳蔡国飙辛洁陈辰王鹏
Owner BEIHANG UNIV
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