학술논문

Experimental study on the temperature compensation effect of plasma in a 300 ml closed bomb
Document Type
Conference
Source
2014 17th International Symposium on Electromagnetic Launch Technology Electromagnetic Launch Technology (EML), 2014 17th International Symposium on. :1-3 Jul, 2014
Subject
Components, Circuits, Devices and Systems
Engineered Materials, Dielectrics and Plasmas
Fields, Waves and Electromagnetics
Power, Energy and Industry Applications
Propulsion
Plasma temperature
Ignition
Combustion
Temperature sensors
Weapons
Language
Abstract
The interior ballistic performance of conventional gun is influenced by ambient temperature greatly. In the case of low ambient temperature, the chamber pressure and muzzle velocity are relatively low; and in the case of high ambient temperature, chamber pressure and velocity are higher. The reason is that the propellant combustion performance is affected by ambient temperature. The burning rate is low at low ambient temperatures, and high at high ambient temperature. The interaction of plasma and propellant can change the combustion performance of propellant, reducing or eliminating the temperature sensitivity of propellant, and this is the temperature compensation effect of plasma. In this paper, plasma ignition experiment has been carried on in a 300 ml closed bomb, and the temperatures of propellant were at −40°C, 20°C, and 50°C. Experimental results show that by regulating the electrical energy of discharge, maximum pressure, propellant burning end time and pressure-time curves are roughly the same as the propellant temperatures is −40°C and 20°C. Compared with the high temperature, the maximum pressure increase by 21 Mpa and burning end time shortened by 4.2 ms, which means that the temperature compensation effect of plasma is very significant.