Determining The Ratio Of Pressure And Compressor Air Mass Flow Rate To Generate Thrust

Missiles are strategic defense equipment that have a high deterrent effect in the national system because they destructive power, precision, and can be launched remotely. With above characteristics, missile is high-tech product, it still needs lot of engineering effort to master technology, especially propulsion / technology which mostly form turbojet engines. background, this study designs analyzes one main components system, namely compressor impeller. This pressure ratio mass flow rate air whose values used obtain impeller design small engine on surface-to-surface cruise system. The method analytical method. conclusion combination 4 an 2.5 kg/s produce target thrust 1,300 N, diameter smaller than maximum allowable space 270 mm.