Slow baking and burning test system of solid rocket engine

Abstract

The invention relates to a slow baking and burning test system of a solid rocket engine. The system comprises a test box, a heating system, a control system, a data acquisition system, a video monitoring system, a shock wave overpressure sensor and a result judging system, wherein the test box is connected with the two half cylinders through fasteners, a sample support is arranged in the test box,a thermocouple is inserted into the top of the test box, the thermocouple is connected with the data acquisition system, the heating system winds the outer side of the test box, the heating system isconnected with the control system, and the outer side of the heating system is sequentially wrapped with heat preservation cotton and a protection shell; and PID is adopted to adjust by the control system, the data acquisition system records the temperature inside the test box through a high-speed acquisition card, the video monitoring system records the damage degree of the test box, the shock wave overpressure sensor is used for recording the magnitude of the overpressure of the shock wave, and the result judging system is used for judging according to the damage degree of the test box andthe overpressure of the shock wave. The system provides data for evaluating and identifying the low-vulnerability and passive characteristics of the solid rocket engine.

Description

technical field [0001] The invention relates to a solid rocket motor slow cook-off test system, which can provide data for the design, development, evaluation and identification of parameters such as low vulnerability and insensitivity characteristics of the solid rocket motor. Background technique [0002] In modern warfare, fighter planes, ships, aircraft carriers and other combat platforms are equipped with various types of weapons. In order to improve combat capabilities, the energy and power of weapon models are getting higher and higher, followed by the deterioration of safety performance, especially in transportation Combustion or explosion accidents caused by external stimuli such as accidental falls, fires, etc. in the process of lifting, hoisting and combat will not only cause damage to one's own weapons and equipment, but also cause a large number of casualties and huge economic losses. For example, in April 1967, the USS Forrestal aircraft carrier caught fire and...

AI Technical Summary

Problems solved by technology

[0003] With the continuous enhancement of China's national defense strength and the increase of unstable factors in the surrounding environment, design units and the military urgently need to establish test systems and methods for the low vulnerability and insensitivity of solid rocket motors. There is no test system for solid rocket motors. For this reason, this method has established a test system suitable for slow cook-off of solid rocket motors. After many tests and verifications, the results show that the device is stable in use, easy to operate, and the test results are consistent with The results of foreign countries are more consistent

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