Liquid Rocket Motor

Numerical Simulation and Experimental Validation of Chemical Reaction Viscous Turbulent Flow Field in the Nozzle of Liquid Rocket Motor

液体火箭发动机喷管化学反应黏性流场数值模拟和实验验证

Bipropellant liquid rocket motor

双元液体推进剂火箭发动机

A transient burning model of solid propellants and its application to liquid quench of rocket motor

固体推进剂瞬态燃烧模型及其在液体喷射熄火研究中的应用

It is found from this theoretical study that there is a critical value of injection pressure drop required , for the liquid quench of rocket motor .

理论研究发现液体喷射瞬变燃烧存在着临界喷射压降。

Determination of liquid quantity required for liquid quench of solid rocket motor

固体火箭发动机液体喷射熄火液量的确定